FIELD OF THE INVENTION

The present invention relates to an improved propelling system for an underwater device with the self charging structural design capable of propelling in the water. The present invention specifically describes an underwater device with an additional charging arrangement that is capable of propelling inside water as well as at the surface of water bodies.

BACKGROUND AND THE PRIOR ART Various types of propulsion devices are known for propelling watercraft through water environments. Such types of propulsive devices include types that push water, push air, and that is propelled by other means, such as by rocket. This invention pertains particularly to water pushing propulsion devices.

Various types of water pushing devices have clearly been proven successful and have been utilized for decades and even centuries. Presently, the most common of such devices in use are the exposed rotating propeller and the ducted rotating propeller (the later often being referred to as "jet" propulsion). In most circumstances, the exposed type of propeller is the most efficient and practical means for powering a watercraft. However, in some situations, such as in situations involving a watercraft such as a Jet Ski© or a Wave Runner©, an exposed propeller would present a significant risk of personal injury, and therefore a ducted propeller is utilized in place thereof. Although generally less efficient, ducted propellers present significantly less risk of personal injury.

U. S. Patent No. 8038492 to John A. Tesvich disclosed underwater propulsion apparatus for enhancing propeller motion by attaching annular collar affixable in the shaft of the propeller in a longitudinal space between a propeller hub and a cut less bearing.

U. S. Patent No. 4375337 to Joseph W Verger disclosed underwater device for ruffling still water that operates a submerged propeller in a stationary location for the purpose of creating ripples on the surface of still water.+ None of the existing prior art presented an underwater device having a dual controlling mechanism, one to control the up-down and forward- backward motion by regulating the wings movement through a“twisting rod assembly“with a’’ movable wrist’’ which is arranged at the one end of the twisting rod and also further forward motion by the driver section . with this none of prior art disclose an underwater device with additional self charging mechanism capable of self charge and generate the electricity in the air, water, and land as well as at the low gravity place where is difficult to install the equipment.

The present device also discloses a mechanism to move in the air at high density places, and low gravity like places outer space planets The device can move in normal air with more propulsion rate of wings.

Therefore, it would be beneficial to provide a simple, robust, and dependable device and method of manufacture and use for substantially propelling device underwater by regulating wings movement through piston control and improved balancing arrangement.

The device is able to propel by using single wings on each side, but using the dual wings concept device performance and efficiency is increased to a good extent.

OBJECTIVES OF THE INVENTION

An objective of the present invention is to design the present device capable of performing motion under water.

Another objective of the present invention is to design the present device capable of performing motion at the surface of the water.

Still another objective of the present invention is to design an underwater propulsion device capable of performing motion by experiencing force and that force is exerting by the twisting rod assembly and movable wrist between the wings.

Still another objective of the present invention is to design a device capable of recharge itself and generate electricity without any external source by its own structural design on the air water and land.

Yet another objective of the present invention is to regulate the movement of the wings by regulating the movement of the twisting rod assembly and movable wrist, which is connected to the wings through the wing frame coupling post. Movement of the twisting rod assembly and the movable wrist providing the force on the wing thus the regulated force on the wings is providing the propulsion mechanism to the device. Further another objective of the present invention is to attach mechanical controls in an underwater device so that technology can bring in more affordable prices.

Further objective of the present invention is to attach an additional spiral road or barrel at any one position of the device for providing stability and structure to perform the operation of electricity generation or propulsion.

In addition to the above objective, the present device can arrange in the wall or with the barrel/rod in a particular position in order to generate the electricity.

A further objective of the invention is to design an underwater propulsion device capable of performing submarine operations.

In addition to previous objectives, a further objective of the invention is to design an underwater propulsion device capable of performing varying air ball or buoyancy as per requirement

A further objective of the present invention all the major parts like the upper wing system, lower wing section, tail section, and many other parts of the device are detachably fixed to the device and that parts can be replaceable for reducing cost for the repairing and servicing.

A further objective of the present invention capable of propelled by both flexible and non-flexible types of the wings section which depends on the type of propulsion system required or using jet type or conventional.

In addition of the above objective, the wings section’s which may be similar or non similar in dimension, shape, and size while arranging with the barrel, rod and somewhere else that depends on the desired requirement for that particular condition of the propelling device

A further objective of the invention is to design an underwater propulsion device capable of performing a flexible wing section, non flexible wing section and semi flexible wing section arrangement to propelling the device and generate electricity with improving the performance. A further objective of the present invention each propulsion mechanism regarding recharging or movement having the same and common principle or concept which may describe in various different forms and embodiments are subjected to the present invention and further improvement of the present invention.

SUMMARY OF THE INVENTION

The present invention relates to an underwater device capable of propelling in the water. The present invention more particularly relates to an underwater device capable of propelling inside the water and as well as capable of propelling and self charging the at the surface of water bodies and the air. The device will also move in the air at high density places and low gravity like places outer space planets.

The device can move in normal air with more propulsion rate of wings .there is some improvement are employing to the device from the last some year which provides better efficiency and the advantages over prior applications 1950/MUM/2014 . the present application is the further development of the prior applications underwater device 1950/MUM/2014 and Indian application 201823029516 an improve the propelling system for the underwater device. So all the applications are in the same technical family.

BRIEF SUMMARY OF THE INVENTION

The present invention advantageously fills the aforementioned deficiencies by providing an improve propelling device with the self-charging unit which is able to recharge itself. The present invention relates to the propelling system with the self charging structural design.

In one particular embodiment of the present invention, the device comprises the pair of the wings in the upper wings section and the lower wing section wherein the pair of wing is the propelling and rotating type of wings, so due to that pairs of wings the present device is capable of propelling and the recharging itself and also able to generate the electricity due to its structure design.

In still particular embodiment of the present invention, the upper wing section comprising the“twisting rod assembly’’ and“movable wrist’’ which are excreting the force on the upper pairs of the flexible wings when the pair of the wing are propelling in the“up-down’’ direction for providing the propulsion mechanism to the present device.

In still particular embodiment of the present invention, the set of semi foldable panel with the flow directing panel unit is providing the surrounding housing to the lower wing section wherein the semi foldable panels are directing the flow of liquid and air in the desired area to the lower wings due to which all the wings can rotate simultaneously in order to generate the electricity/energy. In still particular embodiment of the present invention, set of lower wings are the flapping and rotating type of wings which are providing the both operation of propelling and electricity generation wherein the flapping wings assembly is arranging at both side of the wings, which are help to retain the horizontal position of wing when the wing shifting from the vertically to horizontally or when converting the wings position in the operation from charging to the propelling.

In still above embodiment of the present invention, the flapping wing assembly further providing the propelling mechanism to the lower wing system. Still another embodiment of the present invention, the device is able to recharge itself and other utensils in air, water, and land more particularly in outer space and on another planet wherein it is difficult to install the renewable resource. In still another embodiment of the present invention may comprise the wearable structure which may be used in various operations.

In still another embodiment of the present invention, by the increasing number of sets of varying air ball with the semi foldable panel stability of the device is also increasing.

In still another embodiment of the present invention all the major parts of the device wings, piston, internal- engine, barrel, entire tail section, front section, etc are can be detachable or replaceable.

In still another embodiment of the present invention, the front part of the device comprises the additional mechanical controls a“wing shifting structure assembly’’ for the twisting and turning the dual-plates or wings on the front part of the device.

In still another embodiment of the present invention, the hanging unit such as“wing holding hinges’’ which is holds the wings and the wing frame structure member and that“wing holding hinges’’ in conjunction with the wing shifting structure assembly is further providing the controlled movement in the left/right direction due to which the present device is able to perform twisting or shifting actions.

In addition to the above embodiment of the present invention the twisting and shifting action perform by the device using wing holding hinges concept more particularly in the case when the device comprising the non flexible wings structure with the jet engines or similar engines.

Still another embodiment of the present invention device can 8be held by the rope or cable for providing stability while charging in air or water.

The present invention now will be described more fully with reference to accompanying drawing which is intended to be read in conjunction with both this summary, detail description and any prefer and particular embodiment in many different forms and should not be construed as limited to the embodiment set forth herein; rather these embodiment are provided by way to illustration only and so that this disclosure will be through complete and will fully convey the full scope of the invention to those skilled in the art.

BRIEF DESCRIPTION OF DRAWING

Fig.1 is a view of the perspective of a principal part of the wings mechanism of the improved propelling system for the underwater device with self charging mechanism. Fig. 2 is a view of the perspective of internal design of the improved propelling system for the underwater device with self charging mechanism.

Fig.3 is a view of the perspective of a channel slot piston of the improved propelling system for the underwater device with self charging mechanism. Fig.4 is a view of the perspective of the principal parts of the wings shifting mechanism of the improved propelling system for the underwater device with self charging mechanism.

Fig.5 is a view of perspective to explain the wings shifting concept of the improved propelling system for the underwater device with self charging mechanism.

Fig.6 is a view of perspective to explain the upward propulsion mechanism of the improved propelling system for the underwater device with self charging mechanism.

Fig.7 is a view of perspective to explain the downward propulsion mechanism of the improved propelling system for the underwater device with self charging mechanism.

Fig.8 is a view of the perspective of the internal design of the wings mechanism for forwarding and backward propulsion mechanism of the improved propelling system for the underwater device with self charging mechanism.

Fig.9 is a view of perspective explain the lower wings and semi foldable panel arrangement for the charging mechanism of the improved the propelling system for the underwater device with self charging mechanism.

Fig.10 is a view of perspective explain the lower wings and semi foldable panel arrangement for the propulsion mechanism of the improved propelling system for the underwater device with self charging mechanism.

Fig.11 is a view of perspective explain the flapping concept of the lower wings for the propulsion mechanism of the improved propelling system for the underwater device with self charging mechanism.

Fig.12 is a view of the perspective of the flapping wing assembly structure design of the improved propelling system for the underwater device with self charging mechanism.

Fig.13 is a view of perspective that explains the flapping wing assembly mechanism of the improved propelling system for the underwater device with self charging mechanism.

Fig.14 is a perspective view of the improved the propelling system for the underwater device with self charging mechanism. DETAIL DESCRIPTION

Referring to the figl, upper wings section comprising of a four wings (2, 4, 3, 5), a twisting rod assembly (7), a movable wrist (6), a wing frame coupling post (8), a spiral rod post (9) and a wing frame structure member (12), out of four wings all the four wings (2, 4, 3, 5) is supported by the twisting rod assembly(7) which is arranged immediately below or above the each of wing (2, 4, 3, 5), all the four wings (2, 4, 3, 5) is attached to the wing frame structure member (12) of the present device all the four wings (2, 4, 3, 5) form a system, such that all four wings(2,4,3,5) coincide on the same plane and superposed the upper (2,4) and lower wings (3,5) of the upper wing system are arranged in parallel to each other wherein a twisting rods assembly (7) is disposed between the wings ( 2,3) and (4,5) at the below/above of the wing.

As referring to fig 1,2 When the upper wings (2, 4, 3, 5) is starting propelling in the upward-downward direction then the twisting rod assembly (7) and the movable wrist (6 ) are simultaneously transmitted pressure on the flexible upper wings (2, 4, 3, 5), so all the four wings(2,4,3,5) is starting propelling the device at the desired direction of upward/downward forward-backward, etc. A H- stabilizing rod(22) is the basically an intermediate part between a slot piston sliding unit(34) of a channel slot-piston(31) and a horizontal propulsive rod(21) which is connecting to the wings frame structure member(12) through a balancing rod(23), the H-stabilizing rod (22) is the helpful in controlling wings movement through the balancing rod (23) and provide accuracy and also reduces the unnecessary movement of the rods that may causes damage to the piston.

The one end of the H-stabilizing rod(22) can be disposed on the slot piston sliding unit(34) of the channel slot piston (31), and the H-stabilizing rod(22) can move in unison with the channel slot piston(31) and further the other end of H-stabilizing rod(22) can engage with the horizontal propulsive rod(21) in such manner that the horizontal propulsive rod(21) move upward-downward when a channel slot piston-disc(32) rotates horizontally.

According to fig (3), the channel slot-piston(31) is placed at the center of the engine or device over the motor section wherein the channel slot-piston(31) is having a number of slots which is used to provide the up-down propulsion mechanism to the wings(2,3,4,5) and wings are superposed one over another and also use to propel the device by using the single motor assembly. Each slot section of the channel slot-piston (31) comprising the channel slot piston discs(32) that is mounted to a motor shaft assembly (35) wherein the slot piston disc (32) has molded in the half -upward direction and in the half-downward direction for moving the slot piston sliding unit(34) of the channel slot piston(31) in the up- down direction by moving a k-type propulsive shaft member(33) which is disposed between a slots(36) and the channel slot piston disc(32) which shown in fig (3), so when the motor shaft assembly(35) is rotating in its own axis then the channel slot piston disc(32 ) is also rotating and the free rotating tube part of the k-type propulsive shaft member(33) is not shown that is also rotating due to that k-type propulsive shaft member(33) which is disposed between the slots(36) that k-type propulsive shaft member(33) that can only moving in up and down direction in unison with half up-molded and half down-molded part of the channel slot piston disc(32) due to that the channel slot piston sliding unit(34) of the channel slot piston(31) is moving in the upward and downward direction for providing the propulsion mechanism to the device.

Referring to the fig (4), the wing frame structure member/ 12) is connected to the horizontal propulsive rod (21) through a wing holding hinges(44) that horizontal propulsive rod(21) providing the sustain up-down movement to the upper wing(2,4,3,5) and further more the upper part of the wing holding hinges(44) is coupled to a wing-shifting structure assembly(41) in which a open ended coupling joint(43) is arrange above the wing holding hinges (44) at the both front and rear part of the device that open ended coupling joint(43) is coupled to the all wing holding hinges(44) through the wing shifting structure assembly(41) and a wing shifting motor assembly(45) which is shifting the load to the all wings holding hinges(44) at the right or left side by the moving of a arc -type shifting rod(42) in the clockwise or anticlockwise direction due to which the device and the wing system can move in the left/right direction by moving the wings in left or right direction during the gliding mode of the device.

According to fig (1, 6, 7), In a preferred embodiment, there can be an independent twisting rod assembly (7) that is coupled to each wing(2, 3, 4, 5) of a upper wing system (l).In this embodiment, some component of the twisting rod assembly(7) such as the movable wrist (6) can be further coupled to each wing of the upper wings system (1) and that movable wrist(6) can control the flapping amplitude of all the individual upper wings. Further in this embodiment the wings are can flap/propel at the constant frequency/amplitude for the propulsion of the device by providing the constant angle by twisting the movable wrist(6) in the desired direction.

The upper wings system (1) of the device comprises a set of the twisting rod assembly (7) that causes upper wings to flap. The twisting rod assembly(7) comprising a movable wrist(6), a set of parallel rods not shown in fig is coupled to one end at spiral rod post(9) through a spiral rod sliding unit (10), and a wing frame coupling post(8) which is connected to the wings frame structure member(12). in preferred embodiment, there can be plurality of twisting rods assembly(7) that can be arranged at the above/below or both side of the flexible wings(2,4,3,5) of the upper wings system/ 1), for example, there may be four/six independent twisting rod assembly(7) arrange in the device, in this embodiment each upper wing is mechanically or electrically coupled to one of the twisting rod assembly(7), allowing each wing to flap independently each wing can, therefore, twist or flap/propel at different angle and amplitude with the unique flap pattern.

As a further, best operation obtain by the twisting rod assembly(7) that control the propelling motion of the device by twisting/shifting the movable wrist(6) in the desired direction of forward and backward by means of when the movable wrist (6) is turning to the forward direction then the device is able to propel in the forward direction by the continuous propulsion of flexible wings(2,3,4,5) with the wings frame structure member (12) and when the movable wrist(6) turn to backward direction so the device being able to propel in the backward. furthermore, the movable wrist (6) controls the flapping amplitude of each exterior end of the flexible wing (2, 3, 4, 5) individually .in addition there can be the twisting rod assembly(7) with the wings frame structure member(12) in unison that control the propulsion motion of the device by twisting the movable wrist(6) in the forward-backward and upward -downward direction, and the movable wrist (6) that is capable of for controlling the flapping amplitude of the wings in this manner that movable wrist(6) is capable of for providing the maximum and minimum up-down propulsion to the device .in some embodiment the twisting rod assembly (7) can also hold the wings straight and stationary by holding wrist straight, for allowing the device to glide and further the twisting rod system discussed in great detail below. As per above embodiment, the twisting rod assembly (7) is extending between the spiral rod sliding unit(10) of the spiral rod post(9 ) and the movable wrist(6) through the wing frame coupling post (8), the twisting rod assembly (7) is helpful for controlling the movable wrist(6) movements by moving the spiral rod sliding unit(10) of the spiral rod post (9)

REFERING to the fig (1,2), each wing frame structure member (12) comprising the wing frame coupling post (8) near the device body that wing frame coupling post(8) is connecting the wings(2,3,4,5) with the respective twisting rod assembly(7) .wherein the twisting rod assembly(7) is horizontally extending away from that wing frame coupling post(8) and device.

Moreover, the twisting rod assembly(7) is extending between the wing frame coupling post(8) and the movable wrist(6) and facilitate the coupling between the movable wrist(6) and respective wing(2,3,4,5) in such a manner that movable wrist(6) is capable to provide best the propulsion mechanism to the device by means of when the movable wrist (6) is turning to the downward direction then the device is able to propel in the upward by the continuous propulsion of flexible wings(2,3,4,5) with the wings frame structure member (12) and when the movable wrist(6) turn to upward direction so the device being able to propel in the downward.

In another embodiment of the present invention, the brushless (BLDC) motor driver may arrange at the movable wrist(6) that causes the wrist is capable of moving or rotating in the forward direction and backward direction in order to provide the forward or backward movement of the device.

In another embodiment of the present invention, the present device with the non-flexible wings arrangement further include the additional sets of the non flexible wings with the tilting edges which are arrange at the exterior end of the wings or at the movable wrist (6) section that additional set of wings is used to stabilize the device and provide the up-down movement by horizontally rotating/moving the additional wings in its own axis. Referring to the fig (9,10) in the other embodiment, device comprises a lower wing section wherein four or more sets of a lower wing(l l l,112,113,114) is pivotably coupled to a center gear arrangement(94), in this configuration by rotating the wings(l l l,112,113,114) in any clockwise or anticlockwise direction that can move the center gear arrangement (94) horizontally due to which device is able to generate electricity.

Fig (9,10), the lower wing configuration of an above embodiment of a present device in accordance with the present invention. In this embodiment, the device is constructed in a lower wing configuration which including a legs(96); a front (forward) wings(112,114) is coupled to the legs(96); a rear(aft) wings (111,113) is coupled to legs(96), and the controllable rotation means the center gear arrangement(94) is coupled to the both forward and rear wing(112,114,l l l,113) through the legs(96) and a leg gear arrangement(95), in order to, rotates all four wings simultaneously in clockwise or anticlockwise direction.

According to fig (11,12,13), In one preferred embodiment of the present invention, a flap-casing unit (121) is pivotally arrange on the all four wings(l l l,112,113,114) at a internal non-flexible wing section (115) on the both side of the wings with a force transmitting strips (124) arrangement, the force transmitting strips (124) is extend outward from the flap-casing unit(121) for providing the control propulsion mechanism to the device by flapping the wings in the up/down direction.

In addition to the above embodiment, the best control propulsion of the device in the forward-upward direction of the device through the internal non flexible lower wing section (115) of the lower wing (111,112,113,114) which includes the force transmitting strips (124) to control the propulsion and the control propulsion means comprising the force transmitting strips (124), generally, the force transmitting strips(124) and a force transmitting strips arm(126) that force transmitting strips (124) is pivotally connected to the flap casing unit (121) through a hollow tube (122) and a hollow tube slots (123) which is present at the one side of the hollow tube(122), and the force transmitting strip arm(126) enables the force transmitting strips(124) to tilt/turn in the up-down direction along with the wings(l l l,112,113,114) which are connected to the legs (96) in order to provide propelling- mechanism.

Moreover, the force transmitting strips(124) arrangement is comprising the sets of force transmitting strips(124) are arrange in the parallel to the wings(l l l,112,113,114) at the both side of the wings ,and the force transmitting strips arm(126) is perpendicularly mounted on the force transmitting strips (124) and the sets of force transmitting strips(124) are arrange inside the hollow tube(122) wherein at the one end of the hollow tube(122) is including the hollow tube slot(123) in that particular hollow tube slot(123) the force transmitting strips arm(126) is the perpendicularly mounted on the force transmitting strips(124) and at the another end of the hollow tube(122) the force transmitting strips(124) are divided into the two section or a strip twisting joint(125) is provided in which from the strip twisting joint(125) one end of the force transmitting strips(124) is open ended and able to twist in up-down direction that is responsible to provide the control propulsion of the device in the forward and upward direction when the wings is flapping or move a flexible lower wing section(116) of the lower wings (111,112,113,114) in the up-down direction that wings have the open portion that is created by the force transmitting strips(124) by twisting in the downward direction which is enables by the force transmitting strips arms(126) , and the closed upper portion wherein the force transmitting strips(124) not twisting or not permitting to the wings to move in upward direction or not enables by the force transmitting strips arms(126 ) for twisting in upward.

Fig (14) shown, a wings coupling shaft arm (141) is detachably-connecting the lower wings( 111,112,113,114) with the upper wing frame structure member(12) in order to provide the propulsion mechanism for the lower wings(l l l,112,113,114). this arrangement causes the sets of the lower wings(l l l,112,113,114) is up-down propel and move during the flight and further capable to fold in the desired manner so that the lower wing can execute both propulsion mechanism and electricity generation mechanism by the same set of lower wings (111,112,113,114).

Furthermore, lower wings(l l l,112,113,114) can connect to the upper wings frame structure member(12) or directly connected to the channel slot piston(31) arrangement through the horizontal propulsive rod (21) and h- stabilizing rod (22) arrangement in order to execute the propulsion mechanism of the lower wings. In another embodiment of the present invention referring to fig (9,10 ), device comprises the two or four sets of a semi foldable panel (91)which are situated at the each facing of device and extended outward from the device body through a resting rods arms(97) which is capable of moving and folding the semi foldable panels (91) in such an manner due to which the semi foldable panel (91) is able for providing the housing to the lower wing section when the semi foldable panel (91) is placed in the parallel to the lower wings (111,112,113,114) in order to facilitate the flow of air /water in a particular direction due to which all the four wing rotate simultaneously for generating the electricity.

In other embodiment, the semi foldable panel (91) extended outward from the device body further comprising the foldable structure, a flow directing panel gap unit(92) or gap within the panel and a varying air ball (93) arrange at both ends of the semi foldable panels(91).In this particular embodiment, the semi foldable panels (91) are configured in this manner the pair of front semi foldable panels (91) pivotally coupled the front resting rods arm (97); the rear semi foldable panels (91) pivotally coupled the rear resting rod arms (97) and the controllable propulsion motion means the semi foldable panels (91) is connecting to the varying air balls (93) at the each end of the semi foldable panels (91) in order to provide the stability to the device and further, the semi foldable panels (91) is operating in the conjunction with varying air ball (93) for facilitating the turning and tilting motion to the device by moving the semi foldable panel (91) or varying air ball(93) in a different direction due to which device is capable of propelling in several different directions. In addition of above embodiment, the semi foldable panels (91) may also arrange with the upper wings system (1) manually in such a manner that the pair of the upper wings (2, 3, 4, 5) are surrounded by the semi foldable panel(91) with the parallel coupling or having arrange in parallel wherein the semi foldable panel (91) facilitating the flow of air/water in the particular direction for the upper wings (2,3,4,5)due to which the wing(2,3,4,5) are circularly propelled or rotate in clockwise and anticlockwise direction for generating the electricity through its surrounding or the renewal sources according to the present embodiment, the semi foldable panels (91) is capable of arranged in the parallel to the lower wings (111,112,113,114) and the upper wings(2,3,4,5) in the automatically/ manually manner in order to facilitate the direction of the air/water in the particular required area for rotating the wings in clockwise or anticlockwise direction.

In addition to the above embodiment panel section may further comprise the barrel arrangement and the wall mounting arrangement due to which wings system of the device can stabilize in the particular position in order to create the electricity

Fig (14) shown, a tail(142) which is providing the turning ability to the device wherein a semi-flexible plate (143) is arranged in the tail( 142) that semi-flexible plate (143) is provides the turning movement to the device by performing in the clockwise and anticlockwise movement that clockwise/anticlockwise movement helps the device for rotation on its own axis, the semi-flexible plate (143) structure comprising a non pivot flap casing unit( 144) which is arrange at the both side of the semi flexible plates (143) wherein the non pivot flap casing unit(144) comprising similar arrangement as a flapping wing assembly(13) which is described in lower wings system(l l l,112,113,114) or ( 11) shown in fig(l 1 , 12, 13) wherein the non pivot flap casing(144) includes the hollow tube(122), force transmitting strips(124) arrangement and the force transmitting strips arm(126) wherein the hollow tube(122) and force transmitting strip(124) is extended outward from the non pivot flap casing(144)

The Force transmitting strip(124) is including the force transmitting strips arm(126) at the one side within the hollow tube slot(123) in the hollow tube(122) and the strip twisting joint (125) is arranged at another side of the hollow tube(122) wherein the strip twisting joint(125) is the point at which force transmitting strip(124) is twisting or move in the up and down direction and operates in conjunction with the force transmitting strips arm (126) by means of when the force transmitting strip arm(126) is suspending in the downward direction vertically due to the gravity that time the force transmitting strip(124) can twist and move in up-down direction and not able to push water but when the force transmitting strip arm(126) is not suspending in downward direction or positioned over the wings(l l l,112,113,114 or 11) horizontally or in a horizontal manner so the force transmitting strips(124) are not able to twist in the up-down direction from that joint and push the water this arrangement provide the ability of pushing the water and allow the device to move in it own axis without forwarding movement. A fin (146) and a driver (147) is mounting on the tail for further providing the stability and forward movement to the device. In another embodiment of the wings section, the piston can include any desired shape and size rectangular, circular semicircular triangular hexagonal or any desired shape or size due to which the device or apparatus performance becomes more efficient or better. The wing structure comprising the frame of wings can also contain any shape, size, the material according to A wing section can include any desired shape and size rectangular, circular, semicircular, triangular, hexagonal, or any desired shape or size due to which the device or apparatus performance become more efficient or better.

It is also to be noted that the present invention is susceptible to modifications, adaptations and changes by those skilled in the art. Such variant embodiments employing the concepts and features of this invention are intended to be within the scope of the present invention, which is further set forth under the following ADVANTAGES OF THE PRESENT INVENTION

The best propulsion mechanism of the device obtained by the arranging the twisting rod assembly and the movable wrist in between the pairs of the wings and further the movable wrist is capable to shifting in forward backward direction to propel the device so the present device is able to move in all direction of forward-backward and upward-downward using the single movable wrist and twisting rod assembly arrangements.

The present device can be used to perform various types of underwater operations such as navigation, security operations, and research activities in a faster way, etc. The device is operating under mechanical control so its dependence on electronics is less. The device can be used for temperature sensing and data collection. The present device uses to recharge itself and other utensils by the own structural design in air, water, and land most particularly to the planet of outer space.

In present device major parts of the device are detachable or replaceable due to which cost reduction on transportation, repairing, maintenance.

The present device comprising the panel structure with the barrel and wall mounting arrangement due to which device can be easily arranged in different places for energy electricity generation purposes.

The present device having less complexity and the most affordable prices.

MATHS

The present calculation about the propulsion mechanism of the device to in the various different direction. vindicated the movable wrist section which is positioned above /below of the wings or may at both side of the wings. Ax- Total displacement of the movable wrist in any direction wherein x indicating the positioning of the movable wrist and D indicates the displacement of the movable wrist in any required direction.

A= indicating the device

AA=Total displacement of the device in any of the following directions of the up-down forward and backward.

W=Indicating the wings system comprising the pair of wings each side of the device.

AW— Constant continuous propulsion of the wing section in the up-down direction.

1) Condition in which the device required the upward movement with the sustain continuous propulsion.

So,

DC(Q|)= Total displacement of the wrist in the downward direction

DC(Q|)= \X( 180+ \X )=Total displacement of the movable wrist in the downward direction by varying the angel Q.

DC(Q|) X A W _Anguiar p _r0 p _Uision =Total displacement of the wrist in the presence of the continuous propulsion of the wings system.

DC(Q ) X AW ngular p _r0 p _U isi _on — D4 T X AW ngular propulsion As per the above equation AW _{Anguiarpr0pUislon} is the common element function for both the movable wrist and device.

Therefore

W Angular p _r0 p _U is _l0 n can be assumed to be constant =1

Result 1 DC(Q|) = AA T

DC(Q|) oc ^-1 DA( displacement of device in upward direction)

When the movable wrist is moving in the downward direction then the device is propelling in an upward direction in the presence of constant propulsion of the wings system.

IF the movement of the movable wrist in the downward direction is zero

So DC(Q|) =1 Wherein, W Angular propulsion Propulsion in the upward and downward direction nullifying to each other of the wings system.

1 W An ular propulsion ^~ AA T X AW Angular propulsion

AA T= 1 (So the total displacement of the device in the upward direction is zero or device is in stationary condition =1)

2) Condition in which the device required to move in the downward direction with the sustain continuous propulsion of the wings system.

\X(0† )= Total displacement of the movable wrist in the upward direction \X(0† )= \X( 180- \X )=Total displacement of the movable wrist in the upward direction by varying the angel Q

DC(Q†) X AW Angular propulsion =Total displacement of the movable wrist in the presence of the continuous propulsion of the wings system.

DC(QT) X AW Angular propulsion ~ AA 1 X AW Angular propulsion

As per the above equation AW Angular propulsion is the common element function for both the movable wrist and device.

Therefore

AW Angular propulsion can be assumed to be constant =1

Result 2 DC(Q†) = DA i

When the movable wrist is moving in the upward direction then the device is propelling in the downward direction in the presence of constant propulsion of the wings system.

SO DC(qί) oc ^-1 DA (displacement of device in downward direction)

IF the movement of the wrist in the upward direction is zero

SO DC(Q†) =1

DC(Q†) X AW Angular propulsion ^~ AA i X AW Angular propulsion

Wherein, AW Angular propulsion Propulsion in the upward and downward direction nullifying to each other of the wings system. 1 X AW _An g _U]ar propulsion ^— ^A 1 X AWy^g _U]ar propulsion:

DA 1 = 1 (So the total displacement of the device in the downward direction is zero or device is in stationary condition =1)

3) Condition in which the device required the forward-upward movement with the sustain continuous propulsion of the wings system.

DC(Q1)= \X( 180+ \X )=Total displacement of the movable wrist in the downward direction varying the angel Q.

DC = movement of the movable wrist in the forward direction.

DC(Q l)=Total displacement of the movable wrist in the forward-downward direction varying the angel Q

DC(Q1) X iW _{AngUia]. pr0pU]sion} =Total displacement of the movable wrist in the presence of the continuous propulsion of the wings system.

As per the above equation AW _{Angular propulsion} is the common element function for both wrists and devices.

Therefore AW _{Angu]ar propulsion} can be assumed to be constant =1

Result 1 DC(QI) = DA T

When the movable wrist move in the forward-downward direction then the device is propelling in a forward-upward direction in the presence of constant propulsion of the wings system.

DC(Q1) oc ^-1 DA ( displacement of device in forward— upward direction) A similar mechanism for the backward direction.

. Thus, Different embodiments of the inventions are possible to achieve the best method of performance and to obtain an effective device as describes. It will be understood that the invention may be carried out into practice by skilled persons with many modifications, variations, and adaptations without departing from its spirit or exceeding the scope of the claims in describing the invention for the purpose of illustration. It is also to be noted that the present invention is susceptible to modifications, adaptations and changes by those skilled in the art. Such variant embodiments employing the concepts and features of this invention are intended to be within the scope of the present invention, which is further set forth under the following claims.

The best propulsion mechanism obtains be arranging the twisting rod assembly(7) and the movable wrist (6) in between the wings.