FIELD OF THE DISCLOSED TECHNIQUE

The disclosed technique relates to vehicles in general, and to suspension and steering systems in particular.

BACKGROUND OF THE DISCLOSED TECHNIQUE

Suspension systems for vehicles are in known the art. In wheeled vehicles, such systems connect a vehicle chassis with a wheel or wheels, but also enable relative motion between the wheel and the chassis at least in the vertical axis of the vehicle. A suspension system aims to maintain contact with the road and to reduce shocks and impacts transferred to the chassis from the wheel. Known in the art suspension systems includes springs (e.g., leaf springs, coil springs, torsion bars) and shock absorbers, which are coupled with linkages between the wheel and the chassis of the vehicle.

Transverse suspension systems are widely used in vehicles. Some current transverse suspension systems may provide independent suspension for each of the wheels of the vehicle. One example of a known in the art transverse suspension system is a double wishbone suspension system. The double wishbone suspension system includes two wishbone arms, each pivotally coupled at one end thereof to a reference frame of a vehicle, employing two pivoting connections. The other end of each wishbone arm is coupled with wheel interface using one pivoting connection. Another example of known in the art transverse suspension system is a MacPherson strut suspension system. The MacPherson strut suspension system includes a single wishbone arm and a telescopic shock absorber which is also used as a steering pivot.

SUMMARY OF THE PRESENT DISCLOSED TECHNIQUE

It is an object of the disclosed technique to provide a novel suspension system. In accordance with the disclosed technique, there is thus provided a suspension system including a Chebyshev-Lambda mechanism, at least one linear motion mechanism and a spring-damper assembly. The Chebyshev-Lambda mechanism includes suspension-arm, a support-arm and a first rotating-arm. A rotating-arm-anchoring-end of the rotating-arm is configured to be rotatably coupled with a reference frame at a rotating-arm-anchoring-node. An operational-end of the suspension-arm is configured to be rotatably coupled with a surface-contact-element-suspended-mount at an operational-node. A support-arm-anchoring-end of the support-arm is configured to be rotatably coupled with the reference frame at a support-anchoring-node. The at least one linear motion mechanism is configured to be coupled with the reference frame via at least one anchoring node. An operational end of the at least one linear motion mechanism is configured to be rotatably coupled with the surface contact element suspended mount at a second operational node. The spring-damper assembly includes at least one spring and at least one damper. The ends of each of the at least one spring and at least one damper are coupled between two points, where the distance between the two points changes during the motion action of the surface contact element.

In accordance with another aspect of the disclosed technique, there is thus provided a suspension system including a first Chebyshev-Lambda mechanism a second Chebyshev-Lambda mechanism and a spring-damper assembly. Each of the first Chebyshev-Lambda mechanism and the second Chebyshev-Lambda mechanism includes a respective suspension-arm, a respective support-arm and a respective rotating-arm. A rotating-arm-anchoring-end of each of the respective rotating-arm is configured to be rotatably coupled with a reference frame at a respective rotating-arm-anchoring-node. An operational-end of each the respective suspensionarm is configured to be rotatably coupled with a surface-contact-element-suspended-mount at a respective operational-node. A support-arm-anchoring-end of each the respective support-arm is configured to be rotatably coupled with the reference frame at a respective support-anchoring-node. The spring-damper assembly includes at least one spring and at least one damper. The ends of each of the at least one spring and at least one damper are coupled between two points, where the distance between the two points changes during the motion action of the surface contact element.

BRIEF DESCRIPTION OF THE DRAWINGS

The disclosed technique will be understood and appreciated more fully from the following detailed description taken in conjunction with the drawings in which:

Figures 1A, 1 B, 1 C, and 1 D are schematic illustrations of

Chebyshev-Lambda mechanism;

Figures 2A, 2B, 2C, and 2D are schematic illustrations of a suspension system constructed and operative in accordance with an embodiment of the disclosed technique;

Figure 3A, 3B, 3C, 3D and 3E are schematic illustrations of a suspension system, constructed and operative in accordance with another embodiment of the disclosed technique;

Figure 4A, 4B, 4C and 4D, are schematic illustrations of a suspension system, constructed and operative in accordance with a further embodiment of the disclosed technique;

Figures 5A and 5B are schematic illustration of a suspension system, constructed and operative in accordance with another embodiment of the disclosed technique;

Figures 6A and 6B are schematic illustrations of a suspension system, constructed and operative in accordance with a further embodiment of the disclosed technique;

Figures 7A, 7B, 7C and 7D are schematic illustrations of a suspension system, constructed and operative in accordance with another embodiment of the disclosed technique; and

Figure 8, which is a schematic illustration of a suspension system, constructed and operative in accordance with a further embodiment of the disclosed technique;

Figure 9 is a schematic illustration of a suspension system, constructed and operative in accordance with another embodiment of the disclosed technique;

Figure 10 is a schematic illustration of a suspension system constructed and operative in accordance with a further embodiment of the disclosed technique;

Figure 11 is a schematic illustration of a suspension system constructed and operative in accordance with another embodiment of the disclosed technique; and

Figure 12 is a schematic illustration of a suspension system constructed and operative in accordance with a further embodiment of the disclosed technique. DETAILED DESCRIPTION OF THE EMBODIMENTS

The disclosed technique overcomes the disadvantages of the prior art by providing a suspension system for a vehicle, which employs one or more Chebyshev-Lambda mechanisms (also known as Hoekens mechanism). The one or more Chebyshev-Lambda mechanisms are arranged to operate in the respective linear ranges thereof. When two or more Chebyshev-Lambda mechanisms are employed, these mechanisms are arranged vertically one with respect to the other (i.e., along a vertical axis) and can each be transverse with respect to a wheel hub rotation axis as well as non-transverse to such a rotation axis. The operational end of each Chebyshev-Lambda mechanism is configured to be coupled with a suspended mount (i.e., a frame on which the wheel is mounted). In a suspension system according to the disclosed technique, the suspension system operates independently of any suspension systems in the vehicle. Chebyshev-Lambda mechanisms are typically employed in the constructions of biomimetic mechanical machines (e.g., machines which mimic a walking creature). Unlike biomimetic machines, where the operational end is typically the output of the Chebyshev-Lambda mechanism, in a suspension system according to the disclosed technique the operational end of each of the Chebyshev-Lambda mechanisms may be regarded as “the motion input” to the suspension system. According to the disclosed technique, a steering mechanism is optionally employed in conjunction with the suspension system as further elaborated below. In the explanations which follow, the plane over which a vehicle maneuvers, is referred to herein as a “horizontal plane” and an axis perpendicular to such a horizontal plane, is referred to herein as a “vertical axis”. When the vehicle is a wheeled vehicle, the “horizontal plan” may be the plane (e.g., terrain) over which a wheel rolls. The terms “vertical motion” and “motion in the vertical direction”, relate herein to motion along a vertical axis as per the definition thereof above. Also, the term “in-motion axis” relates to an axis pointing in a direction along which the wheel rolls (i.e., the in-motion direction, e.g. longitudinal direction of the vehicle). Typically, the in-motion axis is parallel (or substantially parallel, for example, when wheel has a camber angle) to the horizontal plane. The term “lateral axis” relates to an axis perpendicular (or substantially perpendicular) to both the vertical axis and the in-motion axis, pointing in a direction perpendicular to the direction toward which the wheel rolls (i.e., lateral direction). Also, the terms ’’coupled at pivot point”, ’’pivotally coupled”, ’’coupled at rotation point” and ’’rotatably coupled” are all employed herein interchangeably and relate to two elements coupled such that these two elements may rotate one with respect to the other. Reference is now made to Figures 1A, 1 B, 1 C, and 1 D which are schematic illustrations of Chebyshev-Lambda mechanism, generally referenced 100. Chebyshev-Lambda mechanism 100 includes a rotating arm 102, a suspension arm 103 and a support arm 104. In the above example of biomimetic machines, a rotating arm such as rotating arm 102 may also be referred to as an input arm, and a suspension arm such as suspension arm 103 may also be referred to as an actuation arm or an output arm.

A rotating arm anchoring end of rotation arm 102 is rotatably coupled with a reference frame 101 at a rotating arm anchoring node 105, such that rotating arm 102 is operative to rotate about rotating arm anchoring node 105. The location of rotating arm anchoring node 105 is fixed in reference frame 101 (i.e., indicated by the double circle). A rotating arm motion end of rotating arm 102 is rotatably coupled with a suspension arm motion end of suspension arm 103 at rotating node 106, such that rotating arm 102 and suspension arm 103 are operative to rotate one with respect to other about rotating node 106. A support arm anchoring end of support arm 104 is rotatably coupled with reference frame 101 at a support anchoring node 107, such that support arm 104 is operative to rotate about support anchoring node 107. The location of support anchoring node 107 is fixed in reference frame 101 (i.e., indicated by the double circle). A support arm motion end of support arm 104 is rotatably coupled with suspension arm 106 at support node 108, such suspension arm 103 and support arm 104 are operative to rotate one with respect to the other about support node 108.

For a given length, L, of rotating arm 102, the length of suspension arm 103 is 5*L and the length of support arm 104 is 2.5*L. Also, the distance between pivot point 105 and pivot point 107 is 2*L, and the distance between pivot point 106 and pivot point 108 is 2.5*L (i.e., pivot point 108 is located at the middle of suspension arm 103) regardless of the angular position of rotating arm 102.

In the example brought forth in Figures 1A-1 D, the vertical axis represents the angle of 0 degrees (0°) and 180 degrees (180°), where the angles increase in a counterclockwise direction. As rotating arm 102 rotates from 0° degrees, through 90° degrees to 180° (Figure 1 B and 1 C), a second end 109 of suspension arm 103 traces a straight line as indicated by double arrowed dashed line 111. As rotating arm 102 rotates from 180° degrees, through 270° degrees to 180° (Figures 1 D and 1A), second end 109 of suspension arm 103 traces an arc as indicated by double arrowed dashed arc 110. A second end of a first arm linkage (e.g., second end 109 of suspension arm 103) of a Chebyshev-Lambda mechanism shall be referred to herein as an ‘operational end’. Also, the angular range through which a rotating arm (e.g., rotating arm 102) of a Chebyshev-Lambda mechanism rotates, and the operational end traces a straight line, is referred to herein as ‘the linear range’.

Reference is now made to Figures 2A, 2B, 2C, and 2D, which are schematic illustrations of a suspension system generally referenced 120, constructed and operative in accordance with an embodiment of the disclosed technique. The description of suspension system 120 brought herein in conjunction with Figures 2A-2D relates to aspects of the disclosed technique which apply to any of the embodiments described herein in conjunction with Figures 1A-1 D, 3A-3E, 4A-4D, 5A-5B, 6A-6B, 7, 8, 9, 10 or 11. Suspension system 120 includes two Chebyshev-Lambda mechanisms, a first Chebyshev-Lambda mechanism 122i and a second Chebyshev-Lambda mechanism 122 ₂ , each operating within the respective linear range thereof. Suspension system 120 further includes a spring-damper 136. Each one of first Chebyshev-Lambda mechanism 122i and second Chebyshev-Lambda mechanism 122 ₂ is coupled with a reference frame 124 (i.e., at the anchoring nodes indicated by double circles). Reference frame 124 is, for example, a chassis of a vehicle, or a frame of an assembly (e.g., a wheel assembly or corner assembly) attachable to a chassis.

First Chebyshev-Lambda mechanism 122i is coupled with reference frame 124 at rotating arm anchoring node 126-1 and support anchoring node 128-|. Second Chebyshev-Lambda mechanism 122 ₂ is coupled with frame 124 at rotating arm anchoring node 106 ₂ and support anchoring node 128 ₂ . Also, the operational ends of each one of first Chebyshev-Lambda mechanism 122-1 and second Chebyshev-Lambda mechanism 122 ₂ are rotatably coupled, for example with a suspended mount 130, at operational nodes 1321 and 132 ₂ respectively. Thus, suspended mount 130 is free to move in a straight line in the vertical axis, as indicated by arrow 134, and relative to reference frame 124.

Spring-damper 136 (e.g., coil over) may be rotatably coupled with one of Chebyshev-Lambda mechanisms 1221 and 122 ₂ at a selected point (i.e., either directly or mechanical energy transfer elements such as rockers or rods), which moves with motion of suspended mount 130. In the example brought forth in Figure 2A, one end of damper 136 is rotatably coupled with second Chebyshev-Lambda mechanism 122 ₂ at rotating node 127 ₂ such that spring-damper 136 is free to rotate about rotating node 127 ₂ . The other end of spring-damper 136 is rotatably coupled with reference frame 124 at pivot point 138, such that spring-damper 136 is free to rotate about pivot point 138. Thus, any vertical motion of suspended mount 130, and thus of the operational end of second Chebyshev-Lambda mechanism 122 ₂ is transferred to spring-damper 136, which reduces the shocks and impacts transferred to reference frame 124 from the wheel.

With reference to Figures 2B-2D, suspension system 120 is depicted with a wheel 140 mounted on suspended mount 130, rolling over a road 142 at three different instances. Wheel 140 rotates relative suspended mount 130 about in-motion axis. For the sake of clarity, spring-damper 136 has been omitted from Figures 2B-2D. With reference to Figure 2B road 142 is even as wheel 140 rolls there over. In Figures 2B and 2C road 142 defines a horizontal plane indicated by dashed line 144. With reference to Figure 2C, road 142 includes a protrusion (i.e., a “bump”) relative to horizontal plane 144. Consequently, wheel 140 moves “up” in the vertical axis, as indicated by arrow 146. With reference to Figure 2D, road 142 includes a depression relative to horizontal plane 144. Consequently, wheel 140 moves “down” in the vertical axis, as indicated by arrow 148.

Figure 2A above referred to an example in which spring-damper 136 is rotatably coupled to second Chebyshev-Lambda mechanism 122 ₂ at pivot point 127 ₂ . It is noted that this is one alternative for positioning a spring-damper in a suspension system according to the disclosed technique described herein above and below. Additional examples are described herein below. In general, a spring-damper may be placed between any two points that the distance therebetween changes during the motion of the wheel, as further exemplified below in conjunction with Figures 3A-3E. It is noted that the spring-damper or spring-dampers described herein above and below, included a spring and a damper, both connected to at the same points. In general, a suspension system according to the disclosed technique includes a spring-damper assembly, which includes at least one spring and at least one damper. The spring or springs and the damper or dampers are connected at respective points (i.e., either the same points or different points). Also, the number of springs and the number of dampers need not be the same. Nevertheless, the ends of each spring and damper are coupled between two points that the distance therebetween changes during the motion action of the wheel.

Reference is now made to Figures 3A, 3B, 3C, 3D and 3E, which are schematic illustration of a suspension system, generally referenced 150, constructed and operative in accordance with another embodiment of the disclosed technique. The description of suspension system 150 brought herein in conjunction with Figures 3A-3E relates to aspects of the disclosed technique which apply to any of the embodiments described herein above and below in conjunction with Figures 1A-1 D, 2A-2D, 4A-4D, 5A-5B, 6A-6B, 7, 8, 9, 10, 11 , 12. Similar to as described in Figures 2A-2D, Suspension system 150 includes two Chebyshev-Lambda mechanisms, a first Chebyshev-Lambda mechanism 152i and a second Chebyshev-Lambda mechanism 152 ₂ , each operating within the respective linear range thereof attached to a reference frame 160. Similar to as described above, reference frame 160 is, for example, a chassis of a vehicle, or a frame of an assembly attachable to a chassis. Suspension system 150 further includes at least one spring-damper 176.

Chebyshev-Lambda mechanism 152-1 includes a first rotating arm 154-1, a first suspension arm 156i and a first support arm 158i . A rotating arm anchoring end of first rotating arm 154i is rotatably coupled with a reference frame 160 at a first rotating arm anchoring node 162 _{1 ;} such that first rotating arm 154-, is operative to rotate about first rotating arm anchoring node 162-|. The location of first rotating arm anchoring node 1621 is fixed in reference frame 160 (i.e. , indicated by the double circle). A rotating arm motion end of first rotating arm 154i is rotatably coupled with a suspension arm motion end of first suspension arm 156-1 at a first rotating node 164-,, such that first rotating arm 154-1 and first suspension arm 156-i are operative to rotate one with respect to other about first rotating node 164i. An operational end of first suspension arm 156i is rotatably coupled with suspended mount 170 at a first operational node 172-i such that first suspension arm 156i and suspended mount 170 are operable to rotate one with respect to the other about first operational node 172i . A support arm anchoring end of first support arm 158-1 is rotatably coupled with reference frame 160 at a first support anchoring node 166-1, such that first support arm 158-i is operative to rotate about first support anchoring node 1661. The location of first support anchoring node 1661 is fixed in reference frame 160 (i.e., indicated by the double circle). A support arm motion end of first support arm 158-i is rotatably coupled with first suspension arm 156-i at a first support node 168-1, such that first suspension arm 156-i and first support arm 158-i are operative to rotate one with respect to the other about first support node 1681.

Similar to Chebyshev-Lambda mechanism 152i, Chebyshev-Lambda mechanism 152 ₂ includes a second rotating arm 154-1, a second suspension arm 156 ₂ and a second support arm 158 ₂ . A rotating arm anchoring end of second rotating arm 154 ₂ is rotatably coupled with a reference frame 160 at a second rotating arm anchoring node 162 ₂ , such that second rotating arm 154 ₂ is operative to rotate about second rotating arm anchoring node 162 ₂ . The location of second rotating arm anchoring node 162 ₂ is fixed in reference frame 160 (i.e. , indicated by the double circle). A rotating arm motion end of second rotating arm 154 ₂ is rotatably coupled with a suspension arm motion end of second suspension arm 156 ₂ at second rotating node 164 ₂ , such that second rotating arm 154 ₂ and second suspension arm 156 ₂ are operative to rotate one with respect to other about second rotating node 164 ₂ . An operational end of second suspension arm 156 ₂ is rotatably coupled with suspended mount 170 at a second operational node 172 ₂ such that first suspension arm 156 ₂ and suspended mount 170 are operable to rotate one with respect to the other about second operational node 172 ₂ . A support arm anchoring end of second support arm 158 ₂ is rotatably coupled with reference frame 160 at a second support anchoring node 166 ₂ , such that second support arm 158 ₂ is operative to rotate about second support anchoring node 166 ₂ . The location of second support anchoring node 166 ₂ is fixed in reference frame 160 (i.e., indicated by the double circle). A support arm motion end of second support arm 158 ₂ is rotatably coupled with second suspension arm 156 ₂ at second support node 168 ₂ , such that second suspension arm 156 ₂ and second support arm 158 ₂ are operative to rotate one with respect to the other about second support node 168 ₂ .

Figure 3A relates to an example in which spring-damper 176 is coupled with first Chebyshev-Lambda mechanism 152-|. Accordingly, one end of damper 176 is rotatably coupled with first Chebyshev-Lambda mechanism 1521 at first rotating node 164-1 such that spring-damper 176 is free to rotate about first rotating node 164-,. The other end of spring-damper 176 is coupled with reference frame 160 at pivot point 178, such that spring-damper 176 is free to rotate about pivot point 178. Pivot point 178 is fixed in reference frame 160 (i.e., as indicated by the double circle). Since any vertical motion of suspended mount 170, and thus of the operational end of first Chebyshev-Lambda mechanisms 152i in the vertical direction results in motion of first rotating node 164i, such a vertical motion of suspended mount 170 is transferred to spring-damper 176, which reduces the shocks and impacts transferred to reference frame 160 from the wheel.

Figure 3B relates to an example in which two spring-dampers, a first spring-damper 166i and a second spring-damper 166 ₂ are coupled with a respective one of first Chebyshev-Lambda mechanism 152-1 and second Chebyshev-Lambda mechanism 152 ₂ . Accordingly, one end of spring-damper 176i is coupled with first Chebyshev-Lambda mechanism 152-1 at first rotating node 164-1 such that spring-damper 176-1 is free to rotate about rotating node 164-|. The other end of spring-damper 176i is coupled with reference frame 160 at pivot point 178-1, such that spring-damper 176i is free to rotate about pivot point 178i. Similarly, one end of spring-damper 176 ₂ is coupled with first Chebyshev-Lambda mechanism 152 ₂ at second rotating node 164 ₂ such that spring-damper 176 ₂ is free to rotate about second rotating node 164 ₂ . The other end of spring-damper 176 ₂ is coupled with reference frame 160 at pivot point 178 ₂ , such that spring-damper 176 ₂ is free to rotate about pivot point 178 ₂ . Since any vertical motion of suspended mount 170, and thus of the operational end of first Chebyshev-Lambda mechanisms 152-1 and 152 ₂ in the vertical direction results in motion of rotating nodes 164i and 164 ₂ , such a vertical motion of suspended mount 170 is transferred to the respective spring-dampers 176i and 176 ₂ , which reduces the shocks and impacts transferred to reference frame 160 from the wheel. Employing two spring-dampers may increase control of the shock absorption characteristics of the suspension system. For example, each spring-damper may be associated with different characteristics (e.g., motion characteristics, size, angle relative to the vertical axis, material of the spring, damping medium such as oil or air). These motion characteristics are, for example, the motion frequency range of the spring-damper and/or the motion action distance of the spring-damper. Employing spring-dampers with different motion characteristics may result, for example, in linear spring/damper rate over an extended wheel rate (i.e. , relative to a single spring-damper) and/or a uniform frequency response of the suspension system.

Figure 3C relates to an example in which spring-damper 176 is coupled between first Chebyshev-Lambda mechanism 152i and second Chebyshev-Lambda mechanism 152 ₂ . Accordingly, one end of spring-damper 176 is rotatably coupled with first Chebyshev-Lambda mechanism 152-1 at operational node 172-1 such that spring-damper 176 is free to rotate about operational node 172-,. The other end of spring-damper 176 is coupled with reference frame 160 at rotating arm anchoring node 162 ₂ , such that spring-damper 176 is free to rotate about rotating arm anchoring node 162 ₂ . Since any vertical motion of suspended mount 170, results in the vertical direction results in motion of operational node 172-1, such a vertical motion of suspended mount 170 is transferred to spring-damper 176, which reduces the shocks and impacts transferred to reference frame 160 from the wheel. Such orientation may allow a large motion action distance of spring-damper 176 (movement range of suspension arm 168 may be larger than of rotating arm 164), thus increase in shock absorption range compared to the system of Fig. 3B. Figure 3D relates to an example in which suspension mechanism 150 further includes a suspension rocker arm 180 (e.g., a lever) and a suspension pushrod 182, and in which spring-damper 176 is coupled with first Chebyshev-Lambda mechanism 152 ₂ via suspension rocker arm 180 and a suspension pushrod 182. Suspension rocker arm 180 includes three pivot points, pivot point 184 and pivot point 188, each at a respective end of suspension rocker arm 180, and a third pivot point 186 located between pivot points 184 and 188. Suspension rocker arm 180 is rotatably coupled with first Chebyshev-Lambda mechanism 152-, at the third pivot point 186 and at first support anchoring node 166i. Thus, suspension rocker arm 180 is operable to rotate about support anchoring node 166-1 (i.e., independently of first Chebyshev-Lambda mechanism 152-i). One end of damper 176 is rotatably coupled with suspension rocker arm 180 at pivot point 184, such that damper 176 and suspension rocker arm 180 are operable to rotate one with respect to the other about pivot point 184. The other end of damper 176 is rotatably coupled with reference frame 160 at pivot point 190, such that damper 176 is operable to rotate about pivot point 190. Pivot point 190 is fixed in reference frame 160 (i.e., as indicated by the double circle). Also, one end of suspension pushrod 182 is rotatably coupled suspension rocker arm 180 at pivot point 188, such that suspension pushrod 182 and suspension rocker arm 180 are operable to rotate one with respect to the other about pivot point 188. The other end of suspension pushrod 182 is rotatably coupled with suspension arm 156 ₂ of second Chebyshev-Lambda mechanism 152 ₂ at pivot point 192, such that suspension pushrod 182 and suspension arm 156 ₂ are operable to rotate one with respect to the other about pivot point 192.

In operation, any motion in the vertical direction of suspended mount 170, and thus of the operational end of first Chebyshev-Lambda mechanisms 152-1, results in motion of pivot point 192. The motion of pivot point 192 is transferred to spring-damper 176 via, suspension pushrod 182 and suspension rocker arm 180. Thus the shocks and impacts transferred from the wheel to reference frame 160 are reduced. It is noted that in Figure 3D, suspension rocker arm 180 is exemplified as a lever. However, suspension rocker arm 180 may alternatively be a triangular rocker.

In Figure 3D, third pivot point 186 and first support anchoring node 1661 are depicted to be located at the same location. However, in general, third pivot point 186 may located at other points in reference frame 160. Alternatively, third pivot point 186 may be located at first rotating node 164-,, at first support anchoring node 166-1 or other locations on first suspension arm 156-i or first support arm 158-|. Figure 3E relates to an example in which spring-damper 176 is coupled with first Chebyshev-Lambda mechanism 1521 at an extension 194 of a first suspension arm 156i. Accordingly, one end of damper 176 is rotatably coupled with first Chebyshev-Lambda mechanism 152-1 at first pivot point 196 such that spring-damper 176 is free to rotate about first pivot 196. Rotating node is at an end of extension 194 of first suspension arm 156i. The other end of spring-damper 176 is coupled with reference frame 160 at pivot point 178, such that spring-damper 176 is free to rotate about pivot point 178. Pivot point 178 is fixed in reference frame 160 (i.e., as indicated by the double circle). Since any vertical motion of suspended mount 170, and thus of the operational end of first Chebyshev-Lambda mechanisms 152-1 in the vertical direction, results in motion first suspension arm 156-, and thus of pivot point 196 (i.e., via extension 194), such a vertical motion of suspended mount 170 is transferred to spring-damper 176, which reduces the shocks and impacts transferred to reference frame 160 from the wheel. It is noted that in Figure 3E, extension 194 exhibits a curved shape. However, extension 194 may alternatively be straight. Also, spring-damper 176 is depicted as parallel to the vertical axis. However, spring-damper 176 may be at an angle relative to the vertical axis.

In general, a spring-damper may be placed between two points of the arms that the distance therebetween changes during the motion of the suspension system. The two points are selected or designed such that the spring-damper rate (i.e., force per distance of motion of the spring-damper, damping per travel range of the springdamper) shall result in a desired wheel rate (i.e., force per distance of motion of the suspension system or the wheel). As described above in conjunction with Figure 3D, a rocker, such as suspension rocker arm 172, may be employed to achieve a spring-damper rate that shall result in a desired wheel rate.

Reference is now made to Figures 4A, 4B, 4C and 4D, which are schematic illustrations of a suspension system, generally referenced 200, constructed and operative in accordance with a further embodiment of the disclosed technique. The description of suspension system 200 brought herein in conjunction with Figures 4A-4D relates to aspects of the disclosed technique which apply to any of the embodiments described herein above and below in conjunction with Figures 1A-1 D, 2A-2D, 3A-3E, 5A-5B, 6A-6B, 7, 8, 9, 10 11 or 12. Specifically, suspension system 200 depicts an implementation example of the suspension system described hereinabove in conjunction with Figure 3D Suspension. System 200 includes two Chebyshev-Lambda mechanisms, a first Chebyshev-Lambda mechanism 202! and a second Chebyshev-Lam bda mechanism 202 ₂ attached to a reference frame. Similar to as described above, the reference frame is, for example, a chassis of a vehicle, or a frame of an assembly attachable to a chassis.

First Chebyshev-Lambda mechanism 202! includes a first rotating arm 204-,, a first suspension arm 206! and a first support arm 208!. A rotation arm anchoring end of first rotating arm 204! is rotatably coupled with a reference frame (not shown) at a first rotating arm anchoring node 210!, such that first rotating arm 204! is operative to rotate about first rotating arm anchoring node 210! around a rotation axis (shown as a rotation axis 203 ₂ in Figure 4D), and the location of first rotating arm anchoring node 210! is fixed in the reference frame. A rotating arm motion end of first rotating arm 204! is rotatably coupled with a first suspension arm motion end of first suspension arm 206! at rotating node 212!, such that first rotating arm 204! and first suspension arm 206! are operative to rotate one with respect to other about first rotating node 212!. A support arm anchoring end of first support arm 208! is rotatably coupled with the reference frame at a first support arm anchoring node 214!, such that support arm 208! is operative to rotate about first support arm anchoring node 214! around a rotation axis (shown as a rotation axis 203 ₃ in Figure 4D), and the location of first support arm anchoring node 214! is fixed in the reference frame. A support arm motion end of first support arm 208! is rotatably coupled with first suspension arm 206! at first support node 216!, such suspension arm 206! and support arm 208! are operative to rotate one with respect to the other about first support node 216!.

Second Chebyshev-Lambda mechanism 202 ₂ includes a second rotating arm 204 ₂ , a second suspension arm 206 ₂ and a second support arm 208 ₂ . A rotating arm anchoring end of second rotating arm 204 ₂ is rotatably coupled with the reference frame at a second rotating arm anchoring node 210 ₂ , such that second rotating arm 204 ₂ is operative to rotate about second rotating arm anchoring node 210 ₂ around a rotation axis (shown as a rotation axis 203 ₄ in Figure 4D), and the location of second rotating arm anchoring node 210 ₂ is fixed in the reference frame. A rotating arm motion end of second rotating arm 204 ₂ is rotatably coupled with a suspension arm motion end of second suspension arm 206 ₂ at second rotating node 212 ₂ , such that second rotating arm 204 ₂ and second suspension arm 206 ₂ are operative to rotate one with respect to other about second rotating node 212 ₂ . A support arm anchoring end of second support arm 208 ₂ is rotatably coupled with the reference frame at a second support arm anchoring node 214 ₂ , such that rotating arm 208 ₂ is operative to rotate about second support arm anchoring node 214 ₂ around a rotation axis (shown as a rotation axis 203 ₅ in Figure 4D), and the location of pivot point 214 ₂ is fixed in the reference frame. A support arm motion end of second support arm 208 ₂ is rotatably coupled with second suspension arm 206 ₂ at support node 216 ₂ , such that second suspension arm 206 ₂ and second support arm 208 ₂ are operative to rotate one with respect to the other about second support node 216 ₂ .

Also, the operational end of first suspension arm 206i is rotatably coupled, for example, with a suspended mount 226, at first operational node 2181. The operational end of second suspension arm 206 ₂ is rotatable coupled with suspended mount 226 at operational node 218 ₂ . Thus, suspended mount 226 is free to move in the vertical axis, and relative to the reference frame, as indicated by arrow 228, similar to as described above in conjunction with Figure 2A-2D. In Figures 4A-4D, operational nodes 2181 and 218 ₂ are implemented, for example, as ball joints. A wheel hub rotation axis is shown in Figure 4D as a rotation axis 203-i .

In general, a suspension system according to the disclosed technique incudes a damper coupled with one of the Chebyshev-Lambda mechanisms. In the example brought forth in Figure 4B, suspension system 200 further includes a spring-damper (e.g., coil over, fluid filled) 220, coupled with second Chebyshev-Lambda mechanism 202 ₂ via a suspension rocker arm 222 and a suspension pushrod 224. Suspension rocker arm 222 includes three pivot points, pivot point 230 and pivot point 232, each at a respective end of suspension rocker arm 222, and a third pivot point located between pivot points 230 and 232. Suspension rocker arm 222 is rotatably coupled with first Chebyshev-Lambda mechanism 202i at third pivot point thereof and at pivot point 214i. Thus, suspension rocker arm 222 is operable to rotate about pivot point 214-1 (i.e., independently of first Chebyshev-Lambda mechanism 202- . One end of damper 220 is rotatably coupled with suspension rocker arm 222 at pivot point 230, such that damper 220 and suspension rocker arm 222 are operable to rotate one with respect to the other about pivot point 230. The other end of spring-damper 220 is rotatably coupled with the reference frame at pivot point 234, such that spring-damper 220 is operable to rotate about pivot point 234.

Also, one end of suspension pushrod 224 is rotatably coupled with suspension rocker arm 222 at pivot point 232, such that suspension pushrod 224 and suspension rocker arm 222 are operable to rotate one with respect to the other about pivot point 232. The other end of suspension pushrod 224 is rotatably coupled with second suspension arm 206 ₂ of second Chebyshev-Lambda mechanism 202 ₂ at pivot point 236, such that suspension pushrod 224 and suspension arm 206 ₂ are operable to rotate one with respect to the other about pivot point 236.

In operation, suspension pushrod 224 and suspension rocker arm 222 transfers the motion of suspended mount 226 in the vertical axis, as indicated direction of arrow 228, to spring-damper 220, thus the shocks and impacts transferred from the wheel to the reference frame are reduced.

In some cases, the wheel may be employed for steering. To that end, a wheel attached to a suspension system such as described above, is also required to rotate about a steering axis, also referred to as ‘kingpin axis’. In typical steering systems, steering is achieved by an actuator, which pushes and pulls a steering rod which, in turn, pushes and pulls on the suspended mount such that the suspended mount rotates about a kingpin axis. When the actuator is attached to the vehicle platform, and the wheel moves in the vertical axis (e.g., over an uneven surface), the lateral distance (i.e., the distance along the lateral axis) between the vehicle platform and the connection point of the steering rod with the suspended mount changes, thereby the wheel is steered beyond desired steering angle (a phenomenon known as bump-steering). To prevent this, either the length of the steering rod should change, or the actuator should move, both according to the vertical motion of the wheel.

According to the disclosed technique, a steering actuator is mounted on a rocker which rotates according to the vertical motion of the suspended mount. Consequently, the steering actuator and steering rod also move with respect to the reference frame during the vertical motion of the wheel. Thus, the lateral distance between the reference frame and the connection point between the steering arm with the suspended mount, is maintained (i.e., remains constant or substantially constant) during the vertical motion of the wheel, for any steering angle.

As shown in Figure 4D, the rotation axes (rotation axes 203 ₂ -203 ₅ ) around which first rotation arm 204i (at first rotating arm anchoring node 210i ), first support arm 208! (at first support arm anchoring node 214-,), second rotation arm 204 ₂ (at second rotating arm anchoring node 210 ₂ ) and second support arm 208 ₂ (at second rotating arm anchoring node 214 ₂ ) rotate around are substantially parallel to one another. Thus rotation axis 203 ₂ and rotation axis 203 ₃ are substantially parallel to one another, rotation axis 203 ₄ and rotation axis 203 ₅ are substantially parallel to one another, rotation axis 203 ₂ and rotation axis 203 ₄ are substantially parallel to one another and rotation axis 203 ₃ and rotation axis 203 ₅ are substantially parallel to one another. In addition, each of rotation axes 203 ₂ , 203 ₃ , 203 ₄ and 203 ₅ are substantially perpendicular to rotation axis 203! which is the wheel hub rotation axis when a wheel (not shown) is in a neutral position and not being steered.

Also shown in Figure 4D is that both first suspension arm 206i and second suspension arm 206 ₂ are transverse to rotation axis 203!. Thus the direction of first suspension arm 206!, second suspension arm 206 ₂ or both is parallel to rotation axis 203! when a wheel (not shown) is in neutral and not being steered. Furthermore, as shown in each of Figures 4A-4D, first suspension arm 206! and second suspension arm 206 ₂ are positioned one above another and are each coupled with surface-contacts of suspended mount 226 at first operational node 218! and second operational node 218 ₂ . It is noted as well that suspension system 200 can be used in a bogie-like suspension system (not shown) wherein the rotation axes (rotation axes 203 ₂ -203 ₅ ) of a first rotation arm, a first support arm, a second rotation arm and a second support arm are parallel to rotation axis 203! (i.e., the wheel hub rotation axis) when a wheel (not shown) is in a neutral position and not being steered. In such an embodiment, the first suspension arm and the second suspension arm would be perpendicular to rotation axis 203!. Thus the direction of first suspension arm 206!, second suspension arm 206 ₂ or both would be perpendicular to rotation axis 203! when a wheel (not shown) is in a neutral position and not being steered. As mentioned above, in this embodiment, first suspension arm 206! and second suspension arm 206 ₂ would be positioned one above another and would each be coupled with surface-contacts of the suspended mount at first and second operational nodes.

Reference is now made to Figures 5A and 5B, which are schematic illustration of a suspension system, generally referenced 250, constructed and operative in accordance with another embodiment of the disclosed technique. Suspension system 250 includes a steering compensation mechanism, which during vertical motion of suspended mount maintains the lateral distance between the reference frame and steering-arm-rotating-node, located on the suspended mount. The description of suspension system 250 brought herein in conjunction with Figures 5A-5B relates to aspects of the disclosed technique which apply to any of the embodiments described herein above and below in conjunction with Figures 2A-2D, 3A-3E, 4A-4D, 6A-6B, 7 8, 9, 10 11 or 12. System 250 employs the principles described herein above in conjunction with Figures 2A-2D, 3A-3E and 4A-4D. System 250 includes a Chebyshev-Lambda mechanism 252 and a steering actuator rocker 254, which are coupled therebetween via a steering pushrod 256. It is noted that for the sake of clarity of the drawings and explanations, only a single Chebyshev-Lambda mechanism is depicted in Figures 5A and 5B. However, as further elaborated below, the steering mechanism described in conjunction with Figures 5A and 5B can be employed with a double Chebyshev-Lambda suspension system described herein above, and below.

Chebyshev-Lambda mechanism 252 is coupled with a reference frame (not shown) at rotating arm anchoring node 258 and support arm anchoring node 260, similar to as described above in conjunction with Figures 2A-2D, 3A-3E. Steering actuator rocker 254 is rotatably coupled with a reference frame at steering rocker anchoring node 262 such that steering actuator rocker 254 is operable to rotate about steering rocker anchoring node 262. Also, an actuator (not shown in Figures 5A and 5B for clarity) is coupled with steering actuator rocker 254 at actuator mounting point 264. Mounting point 264 may include a joint (e.g. ball joint), allowing motion between the actuator and actuator rocker 254, as the rocker rotates about pivot 262. A steering arm 268 extends from the actuator to suspended mount 270. Steering arm 268 is rotatably coupled with suspended mount 270 at steering arm rotating node 272 such that steering arm and suspended mount are operable to rotate one with respect to the other about steering arm rotating node 272.

One end of steering pushrod 256 is rotatably coupled with steering actuator rocker 254 at pushrod rotating node 274 such that steering pushrod 256 and steering actuator rocker 254 are operable rotate one with respect to the other about pushrod rotating node 274. The other end of steering pushrod 256 is rotatably coupled with Chebyshev-Lambda mechanism 252 via one end of a stub 276 at pivot point 278 such that steering pushrod 256 and stub 276 are operable to rotate one with respect to the other about pivot point 278. The other end of stub 276 is rigidly coupled with support arm 280 of Chebyshev-Lambda mechanism 252, at point 282. For completeness, an operational end of suspension arm 284 of Chebyshev-Lambda mechanism 252 is rotatably coupled with suspended mount 270 at operational node 286 such that suspension arm 284 and suspended mount 270 are operable to rotate one with respect to the other about operational node 286.

In operation, vertical motion of suspended mount 270 is transferred via Chebyshev-Lambda mechanism 252, stub 276, steering pushrod 256 to steering actuator rocker 254 causing steering actuator rocker to rotate about pivot point 262. Consequently, point 264 and thus the steering actuator, moves on an arc 288, thus maintaining the lateral distance between point 262 and pivot point 272, regardless of the motion of suspended mount 270. In other words, the length of the steering rod 268 remains constant or substantially constant during the vertical motion of the wheel, for any steering angle. For example, in Figure 5B, suspended mount 270 has moved down relative to the position thereof in Figure 5A. However, the steering angle and the length of steering arm 268 did not change (i.e. , beyond a determined margin of error).

In Figures 5A and 5B, stub 276 is optional. In general, the other end of steering pushrod 256 may be rotatably coupled with any point which exhibits a vertical motion with the vertical motion of suspended mount 270. Pushrod 256 shall transfer this vertical motion to rocker 254.

Reference is now made to Figures 6A and 6B, which are schematic illustrations of a suspension, generally referenced 300, constructed and operative in accordance with a further embodiment of the disclosed technique. Suspension system 300 includes a steering compensation mechanism, which during vertical motion of the suspended mount, maintains the lateral distance between the reference frame and steering arm rotating node 324, located on the suspended mount. The description of suspension system 300 brought herein in conjunction with Figures 6A-6B relates to aspects of the disclosed technique which apply to any of the embodiments described herein above and below in conjunction with Figures 1A-1 D, 2A-2D, 3A-3E, 4A-4D, 5A-5B, 7, 8, 9, 10, 11 or 12. System 300 is an implementation example of mechanism described herein above in conjunction with Figures 5A and 5B, employed in a suspension system described hereinabove in conjunction with Figures 2A-2D, 3A-3E and 4A-4D. System 300 includes two Chebyshev-Lambda mechanisms, a first Chebyshev-Lambda mechanism 302! and a second Chebyshev-Lambda mechanism 302 ₂ attached to a reference frame. Similar to as described above, the reference frame is, for example, a chassis of a vehicle, or a frame of an assembly attachable to a chassis. System 300 further includes a steering actuator 304, a rocker 306 and a pushrod 308.

Steering actuator 304 is coupled with rocker 306. Rocker 306 is coupled with a reference frame (not shown) at pivot point 310 such that rocker 306 is operable to rotate relative to the reference frame about pivot point 310. One end of pushrod 308 is coupled with rocker 306 at pivot point 312, such that pushrod 308 and rocker 306 are operable to rotate one with respect to the other about pivot point 312. The other end of pushrod 308 is coupled with support arm 314 of first Chebyshev-Lambda mechanism 302-1 , at pivot point 316, via stub 318, such that pushrod 308 and support arm 314 are operable to rotate one with respect to the other. Steering arm 320 is coupled to suspended mount 322 at steering arm rotating node 324, located on said suspended mount 322, such that steering arm 320 and suspended mount 322 are operable to rotate one with respect to the other.

Steering actuator 304 is operative to extend and retract steering arm 320. Consequently, suspended mount 322 rotates about king pin axis 326 enabling steering of a wheel at least within a steering angle range (e.g., on the order of tens of degrees to each direction). In the example brought forth in Figures 6A and 6B, vertical motion of suspended mount 322 is transferred via first Chebyshev-Lambda mechanism 302i, stub 314, steering pushrod 308 to rocker 306 causing rocker to rotate about pivot point 310. Consequently, steering actuator 304 moves on an arc, thus maintaining the lateral distance between pivot point 310 and steering arm rotating node 324 during the vertical motion of the wheel for any steering angle. Alternatively, stub 314 may be coupled with Chebyshev-Lambda mechanism 302 ₂ .

It is noted that the geometry the suspension system and steering compensation described above may be defined to allow a controlled change in the lateral distance between the wheel mount and the reference frame, within a range which provides desired dynamic behavior for the vehicle (e.g. keeping wheel in a toe-in position). For example, the geometry of rocker 306, as well as the sizes and ratios between the different linkages (e.g. ratios between linkages of arm 302! and/or 302 ₂ ) may be defined to provide desired dynamic behavior. In cars, such a change in distance may be defined to allow a limited amount of bump steer, for example between 0.8 to 1.0 degrees over the vertical motion of the suspended mount.

Reference is now made to Figures 7A, 7B, 7C and 7D, which are schematic illustrations of a suspension system, generally referenced 350, constructed and operative in accordance with another embodiment of the disclosed technique. The description of suspension system 350 brought herein in conjunction with Figures 7A-7D relates to aspects of the disclosed technique which apply to any of the embodiments described herein above and below in conjunction with Figures 1A-1 D, 2A-2D, 3A-3E, 4A-4D, 5A-5B, 6A-6B, 8, 9, 10 11 , or 12. Suspension system 350 includes two Chebyshev-Lambda mechanisms, first Chebyshev-Lambda mechanism 352! and second Chebyshev-Lambda mechanism 352 ₂ attached to a reference frame 360. Similar to as described above, reference frame 360 is, for example, a chassis of a vehicle, or a frame of an assembly attachable to a chassis. Each one of first Chebyshev-Lambda mechanism 352! and second Chebyshev-Lambda mechanism 352 ₂ includes a respective rotating arm, a respective suspension arm and a respective support arm. First Chebyshev-Lam bda mechanism 350! includes a first rotating arm 354! a first suspension arm 356! and a first support arm 358!. A rotating arm anchoring end of first rotating arm 354! is rotatably coupled with a reference frame 360 at a first rotating arm anchoring node 362!, such that rotating arm 354! is operative to rotate about first rotating arm anchoring mode 362! and the location of first rotating arm anchoring mode 362! is fixed in a reference frame 360. A rotating arm motion end of first rotating arm 354! is rotatably coupled with a suspension arm motion end of first suspension arm 356! at a first rotating node 364!, such that first rotating arm 354! and first suspension arm 356! are operative to rotate one with respect to other about first rotating node point 364!. A support arm anchoring end of first support arm 358! is rotatably coupled with reference frame 360 at a support anchoring node 366!, such that first support arm 358! is operative to rotate about support anchoring node 366! and the location of support anchoring node 366! is fixed in reference frame 360. A support arm motion end of first support arm 358! is rotatably coupled with first suspension arm 356! at a first support node 368!, such first suspension arm 356! and first support arm 358! are operative to rotate one with respect to the other about first support node 368!.

Second Chebyshev-Lambda mechanism 350 ₂ includes a second rotating arm 354 ₂ a second suspension arm 356 ₂ and a second support arm 358 ₂ . A rotating arm anchoring end of second rotating arm 354 ₂ is rotatably coupled with a reference a frame 360 at a second anchoring node 362 ₂ , such that second rotating arm 354 ₂ is operative to rotate about second anchoring node 362 ₂ and the location of second anchoring node 362 ₂ is fixed in a reference frame 360. A rotating arm motion end of second rotating arm 354 ₂ is rotatably coupled with a suspension arm motion end of second suspension arm 356 ₂ at second rotating node 364 ₂ , such that second rotating arm 354 ₂ and second suspension arm 356 ₂ are operative to rotate one with respect to other about second rotating node 364 ₂ . A support arm anchoring end of second support arm 358 ₂ is rotatably coupled with reference frame 360 at a second support are anchoring node 366 ₂ , such that support arm 358 ₂ is operative to rotate about second support are anchoring node 366 ₂ and the location of second support are anchoring node 366 ₂ is fixed in reference frame 360. A support arm motion end of second support arm 358! is rotatably coupled with second suspension arm 356 ₂ at a second support node 368 ₂ , such second suspension arm 356 ₂ and second support arm 358 ₂ are operative to rotate one with respect to the other about second support node 368 ₂ .

Also, the operational end of first suspension arm 356! is rotatably coupled, for example, with a suspended mount 370 at operational node 372!, such that the suspension arm 356! and suspended mount 370 are free to rotate one with respect to the other. The operational end of second suspension arm 356 ₂ is rotatably coupled, for example, with a suspended mount 370, at second operational node 372 ₂ , such that the second suspension arm 356 ₂ and suspended mount 370 are free to rotate one with respect to the other. Thus, suspended mount 370 is free to move in the vertical axis, and relative to the reference frame, as indicated by arrow 374, similar to as described above in conjunction with Figure 2A-2D.

In the example brought forth in Figure 7A, the dimensions of first Chebyshev-Lambda mechanism 352i are different from the dimensions of second Chebyshev-Lambda mechanism 352 ₂ . For example, if the length of first rotating arm 354! is ‘A’, the length of second rotating arm is AC (i.e., A times C), where ‘C’ is a constant. Thus, the length of second support arm 356 ₂ is 2.5AC and the length of second suspension arm 358 ₂ is 5AC. This difference in the dimensions of first Chebyshev-Lambda mechanism 352! and second Chebyshev-Lambda mechanism 352 ₂ , results in a camber angle (i.e., the wheel is at non-vertical angle relative to the horizontal plane). The camber angle can be selected by a corresponding selection of ‘C’. Figure 7A depicts negative camber. However, a positive camber may alternatively be created. It is noted that although the different dimensions of first Chebyshev-Lambda mechanism 352! and second Chebyshev-Lambda mechanism 352 ₂ , the operational ends thereof still move vertically in the direction of arrow 374. It is also noted that, alternatively or additionally, first Chebyshev-Lambda mechanism 352! and second Chebyshev-Lambda mechanism 352 ₂ are not aligned vertically, such that a line defined by the operational ends of first Chebyshev-Lambda mechanism 352! and second Chebyshev-Lambda mechanism 352 ₂ is tilted in the in-motion direction relative to the vertical axis.

Alternatively or additionally to creating camber, and with reference to Figure 7B, when the wheel is steered, the different dimensions of first Chebyshev-Lambda mechanism 352! and second Chebyshev-Lambda mechanism 352 ₂ may be employed to create a non-vertical kingpin axis 382. In Figure 7B, suspended mount 370 rotates about kingpin axis 382. Negative or positive camber and/or a non-vertical kingpin axis affect the dynamic performance of the vehicle (e.g., traction, cornering, body roll, steering force and the like). It is noted that roll axis of wheel 371 and kingpin axis 382 need not be perpendicular.

With reference to Figures 7C and 7D, Chebyshev-Lambda mechanism 352! is tilted relative to Chebyshev-Lambda mechanism 352 _2: such that the linear motion of operational node 372! is tilted with respect to the linear motion of operational node 372 ₂ . In such a configuration, the camber angle of wheel 371 changes with vertical motion of wheel 371 (i.e., the camber is dynamic) as indicated by double arrowed arc 376. A dynamic camber affects the dynamics of the vehicle. For example, during a turn, the roll of the vehicle results in vertical motion of the wheel. Thus, during a turn, the surface area of the wheel, which is in contact with the road during the turn, may be maintained or increased. According to another example for achieving a dynamic camber, one of the Chebyshev-Lambda mechanisms operates in the non-linear range thereof.

Reference is now made to Figure 8, which is a schematic illustration of a suspension system, generally referenced 400, constructed and operative in accordance with a further embodiment of the disclosed technique. The description of suspension system 350 brought herein in conjunction with Figure 8 relates to aspects of the disclosed technique which apply to any of the embodiments described herein above in conjunction with Figures 1A-1 D, 2A-2D, 3A-3E, 4A-4D, 5A-5B, 6A-6B, 7, 9, 10 11 or 12. Suspension system 400 includes two Chebyshev-Lambda mechanisms, first Chebyshev-Lambda mechanism 402i and second Chebyshev-Lambda mechanism 402 ₂ . Each one of first Chebyshev-Lambda mechanism 402! and second Chebyshev-Lambda mechanism 402 ₂ is coupled with reference frame 404 attached to a reference frame 404. Similar to as described above, reference frame 404 is, for example, a chassis of a vehicle, or a frame of an assembly attachable to a chassis. Also, the operational ends of each one of first Chebyshev-Lambda mechanism 402! and second Chebyshev-Lambda mechanism 402 ₂ is coupled with a suspended mount 406. A wheel 410 is coupled with suspended mount via a wheel interface 408 (e.g., wheel hub, a hub bearing).

The motion action distance, Dv, of suspension system 400 (i.e., the distance between the extreme positions of wheel 410 in the vertical axis) is designated by double headed arrow 412 in Figure 8. The dimension of the respective rotating arms of first Chebyshev-Lambda mechanism 402! and second Chebyshev-Lambda mechanism 402 ₂ , and consequently of the respective suspension arms and support arms are selected to provide a desired value of Dv. Furthermore, the dimension of the respective rotating arms of first Chebyshev-Lambda mechanism 402! and second Chebyshev-Lambda mechanism 402 ₂ are selected such that the lateral distance between reference frame 404 and suspended mount 406, as indicated by double headed arrow 414 is within a predetermined range during the action motion of wheel 410. Similarly, the dimension of the respective rotating arms of first Chebyshev-Lambda mechanism 402i and second Chebyshev-Lambda mechanism 402 ₂ are selected such that the lateral distance between reference frame 404 and wheel 410, as indicated by double headed arrow 416, is within a predetermined range during the action motion of wheel 410.

In the examples brought forth herein above, the Chebyshev-Lambda mechanisms employed in a suspension system according to the disclosed technique are depicted in a “down-outward orientation”. In the down-outward orientation, the suspension arm is positioned above the support arm relative to the horizontal plane, the operational end of the suspension arm is coupled with the suspended mount, and the rotating arm and the support arm are coupled with the frame, as described above. However, any one of Chebyshev-Lambda mechanisms may alternatively be in an “up-outward orientation”, a “down-inward orientation” or and “up-inward orientation”. In the up-outward orientation, the suspension arm is positioned below the support arm relative to the horizontal plane, the operational end of the suspension arm is coupled with the suspended mount, and the rotating arm and the support arm are coupled with the frame. In the down-inward orientation, the suspension arm is positioned below the support arm relative to the horizontal plane, the operational end of the suspension arm is coupled with the frame, and the rotating arm and the support arm are coupled with the suspended mount. In the up-inward orientation, the suspension arm is positioned above the support arm relative to the horizontal plane, the operational end of the suspension arm is coupled with the frame, and the rotating arm and the support arm are coupled with the suspended mount.

Reference is now made to Figures 9, which is a schematic illustration of a suspension system, generally referenced 500, constructed and operative in accordance with another embodiment of the disclosed technique. Suspension system 500 includes two Chebyshev-Lambda mechanisms, Chebyshev-Lambda mechanism 502i and Chebyshev-Lambda mechanism 502 ₂ . Each one of Chebyshev-Lambda mechanism 502! and Chebyshev-Lambda mechanism 502 ₂ is similar in operation and construction to any one of the Chebyshev-Lambda mechanisms described above in conjunction with Figures 1A-1 D, 2A-2D, 3A-3E, 4A-4D, 5A-5B, 6A-6B, 7 and 8. In Figure 9, depict suspension system 502! in the up-outward orientation. In the up-outward orientation, the suspension arm 510! is positioned below the support arm 514! relative to the horizontal plane 516. The operational end of suspension arm 510! is coupled with the suspended mount 506 and the rotating arm 512-, and support arm 514-1 are coupled with the frame 504 as described above.

Reference is now made to Figures 10, which is a schematic illustration of a suspension system, generally referenced 520, constructed and operative in accordance with a further embodiment of the disclosed technique. Suspension system 520 includes two Chebyshev-Lambda mechanisms, Chebyshev-Lambda mechanism 522i and Chebyshev-Lambda mechanism 522 ₂ . Each one of Chebyshev-Lambda mechanism 522! and Chebyshev-Lambda mechanism 522 ₂ is similar in operation and construction to any one of the Chebyshev-Lambda mechanisms described above in conjunction with Figures 1A-1 D, 2A-2D, 3A-3E, 4A-4D, 5A-5B, 6A-6B, 7 and 8. Figure 10 depicts Chebyshev-Lambda mechanism 522! in the down-inward orientation. In the down-inward orientation, the suspension arm 530! is positioned above the support arm 534! relative to the horizontal plane 536. The operational end of suspension arm 530! is coupled with the frame 524. The rotating arm 532! and support arm 534! are coupled with the suspended mount 526.

Reference is now made to Figures 11 , which is a schematic illustration of a suspension system, generally referenced 540, constructed and operative in accordance with another embodiment of the disclosed technique. Suspension system 540 includes two Chebyshev-Lambda mechanisms, Chebyshev-Lambda mechanism 542! and Chebyshev-Lambda mechanism 542 ₂ . Each one of Chebyshev-Lambda mechanism 542! and Chebyshev-Lambda mechanism 542 ₂ is similar in operation and construction to any one of the Chebyshev-Lambda mechanisms described above in conjunction with Figures 1A-1 D, 2A-2D, 3A-3E, 4A-4D, 5A-5B, 6A-6B, 7 and 8. Figure 11 depicts Chebyshev-Lambda mechanism 542! in the up-inward orientation. In the up-inward orientation, the suspension arm 550! is positioned below the support arm 554! relative to the horizontal plane 556. The operational end of suspension arm 550! is coupled with the frame 544. The rotating arm 552! and support arm 554! are coupled with the suspended mount 546.

Similar to as mentioned above, and with reference to Figures 9, 10 and 11 , any one of Chebyshev-Lambda mechanisms, 502 ₂ 522 ₂ 542 ₂ may also be in any one of the up-outward orientation, a down-inward orientation or up-inward orientation. Also, any one of Chebyshev-Lambda mechanisms, 502!, 522!, 542!, 502 ₂ , 522 ₂ and 542 ₂ may be tilted as described above in conjunction with Figures 7C and 7D. Also, any one of Chebyshev-Lambda mechanisms, 502!, 522!, 542! exhibit different dimensions with respect to Chebyshev-Lam bda mechanisms 502 ₂ , 522 ₂ and 542 ₂ , as described above in conjunction with Figures 7A.

In the description above, a suspension system according to the disclosed technique includes two Chebyshev-Lambda mechanisms. In general, a suspension system according to the disclose technique include at least one Chebyshev-Lambda mechanism and at least one linear motion mechanism. Reference is now made to Figure 12, which is a schematic illustration of a suspension system, generally referenced 600, constructed and operative in accordance with a further embodiment of the disclosed technique. The description of suspension system 600 brought herein in conjunction with Figure 12 relates to aspects of the disclosed technique which apply to any of the embodiments described herein above in conjunction with Figures 1A-1 D, 2A-2D, 3A-3E, 4A-4D, 5A-5B, 6A-6B, 7, 8, 9, 10 or 11 .

Suspension system 600 includes a Chebyshev-Lambda mechanism 602 and a linear motion mechanism 604 attached to a reference frame 606. Similar to as described above, reference frame 606 is, for example, a chassis of a vehicle, or a frame of an assembly attachable to a chassis. In Figure 12, linear motion mechanism 604 is embodied as arm mechanism which includes arm 612. Chebyshev-Lambda mechanism 602 is coupled with reference frame 606 at rotating arm anchoring node 608 and support anchoring node 610 (i.e., anchoring nodes indicated by double circles). Linear motion mechanism 604 is coupled with reference frame 606 at a first anchoring node 612 and a second anchoring node 614. An operational end of Chebyshev-Lambda mechanism 602 is rotatably coupled with a suspended mount 616, at operational node 6181. An operational end linear motion mechanism 604 is rotatably coupled with a suspended mount 616 at operational node 618 ₂ . The other end of linear motion mechanism 604 is rotatably coupled with reference frame 606. Thus, suspended mount 616 is free to move along the vertical axis, as indicated by arrow 620, and relative to reference frame 606. Suspension system 600 further includes two spring-damper assemblies, spring-damper 622 and spring-damper 624. One end of spring-damper 622 is rotatably coupled with the rotating arm motion node of Chebyshev-Lambda mechanism 602 and the other end of spring-damper mechanism 622 is rotatably coupled with reference frame 606. One end of spring-damper 624 is rotatably coupled with arm 612 at a suspension node, and the other end of spring-damper mechanism 624 is rotatably coupled with reference frame 606. Thus, any vertical motion of suspended mount 620, and thus of the operational end of Chebyshev-Lambda mechanism 602 and linear motion mechanism 604 is transferred to spring-dampers 622 and 624, which reduces the shocks and impacts transferred to reference frame 606 from the wheel. It is noted that the two spring-damper in Figure 12 (i.e., spring-damper 622 and spring-damper 624) are described as an example only. Similar to as mentioned above, suspension system 600 includes at least one spring-damper assembly connected at respective points, where the ends of each spring and damper are be coupled between two points that the distance therebetween changes during the motion action of the wheel, for example, as described above in conjunction with Figures 3A-3E.

A wheel assembly according to the disclosed technique described herein above includes a suspension system, such as any of the suspension systems described hereinabove. The wheel assembly according to the disclosed technique described herein above includes the wheel assembly frame, configured to be attached to a vehicle platform/chassis (e.g., at the wheel corner thereof).

A “corner assembly” as described herein means an assembly for supporting a wheel of a vehicle and regulating the motion of a vehicle according to any of the embodiments disclosed herein. The corner assembly can include components such as steering systems, suspension systems, braking systems (including hydraulic subsystems), gearing assemblies, drive motors, drive shafts, wheel hub assemblies, controllers, communications arrangements, electrical wiring and the like, as is known in the field.

According to the disclosed technique, the wheel assembly and/or corner assembly is motorized and includes a drivetrain assembly. The drivetrain assembly includes, for example, a motor and may further include rotatable drivetrain shaft, coupled with the motor and the wheel, and passing between the Chebyshev-Lambda mechanisms. The rotatable drivetrain shaft is coupled with the wheel, for example, with a constant-velocity (CV) joint. In operation the motor rotates rotatable drivetrain shaft which transmit rotations generated by the motor to the wheel. Optionally, drivetrain assembly may further include one or more gears (e.g., planetary gears).

The above description of the disclosed technique related to a vehicle or vehicles in which the surface contact element (i.e., the element in contact with the surface over which the vehicle moves) is a wheel. However, the surface contact element may alternatively or additionally be, for example, skis or caterpillar tracks. As such, the term “wheel” is a special case of a surface contact element and the term “suspended mount” is a special case of a “the surface contact element suspended mount”. Suspended mount for a wheeled vehicle may include a wheel interface, a wheel hub, a wheel bearing and the like. Also, a vehicle according to the disclosed technique may be a car, a motorcycle, a tricycle, an All Terrain Vehicle (ATV), a train, an aircraft, a trailer, a truck, a toy vehicle, an amphibian, a tank, a tractor, a compactor or a roller. A vehicle or vehicles may include two or more the surface contact elements and, as such, include two or more respective suspension systems, such as those described hereinabove. Also, for the sake of example only, a wheel in a car exhibits a rim diameter of 15-17 inches. The motion action of a suspension system employed with a wheel and a car shall be between 100-300 mm. It will be appreciated by persons skilled in the art that the disclosed technique is not limited to what has been particularly shown and described hereinabove. Rather the scope of the disclosed technique is defined only by the claims, which follow.