FIELD OF THE INVENTION

The present invention relates to wind turbines. More particularly, the invention relates to the wind turbine having a plurality of outer-blades and a plurality of inner-blades attached to the rotating rim. BACKGROUND OF THE INVENTION

There is a wide spectrum of the wind-to-energy conversing turbines. The main element defining the turbine's type is the rotor's shape. In US Patent No. 6,951,443 entitled "Wind turbine ring/shroud drive system" the wind turbine of three-blade rotor is disclosed. This rotor is based on ring or shroud structure for reducing blade root bending moments. The blades of this rotor is very long that brings the common turbine's problem decreasing its efficiency - big linear speed difference between root vs tip parts of the blade. The rotor is carried by the central hub and by two struts. The hub and the struts are mounted into/onto nacelle, i.e. all stresses and forces from the rotor hub and the struts are finally concentrating on/in the nacelle. Thus, the element (nacelle) carrying the rotor does not get any decreasing in stresses producing by the rotor. The central pivotal area of the rotor is being not free for the air flows, its square is taken by struts, interior blades, nacelle itself. As in each common turbines this pivotal rotor's area does not takes any significant part in the energy producing since the low rotating moments (i.e. the distance to the revolution axis). Therefore, the pivotal rotor's part brings a significant drag forces without to generate an energy.

In US Patent No. 7,323,792 entitled "Wind turbine" the wind turbine with foldable blades attached to the rim is disclosed. Here the hub also carries all stresses from the rotor, the central axial part of the rotor is not free for the air flows.

In US Patent No. 7,550,864 entitled "Wind turbine" the wind turbine with a plurality of radial blades attached to the ring-shaped aerofoil diffuser is disclosed. In this turbine the ring-diffuser is used to reduce acoustic emission. The other configuration of this turbine remained without changes - high difference in tip-root blade speeds, at a very high degree filled the pivotal rotor's area, hub carries all stresses. In US Patent No. 7,775,760 entitled "Turbine wheel" the turbine wheel comprising a peripheral rim, series of spokes, plurality of airfoil flexible blades is disclosed. In this turbine the ring- diffuser is used to reduce acoustic outer rim attached to the blades' tip is used. Here the rotor also is carries by the hub, the blades have non-defined shapes decreasing aerodynamic efficiency of the rotor. The central part of the rotor is taken by plurality of non-visible spokes being danger for the birds.

In US Patent No. 7,964,978 entitled "Wind turbine having a blade ring using magnetic levitation" the wind turbine with a ring to which blades are attached. The ring holds the blades and provides the rotor revolutions into a stator/guide track. The rotor is located and supported into said guide track either by mechanical means or electrical means (by magnetic field) for reducing friction between rotor and stator. This rotor has a very filled (by blades, hub, external from supports) central part, this prevents the free air flow at that area. The blades have a high difference between tip/root linear speeds. Both rotor and stator have ring structures, therefore such configuration will be high level weight at large enough embodiments. This will be obstacle to build high power big turbines. Two ring structures will be doubly expensive through installation. In US Patent No. 7,980,811 entitled "Turbine with mixers and ejectors" the wind turbine with an aerodynamically contoured shroud with inlet, ring of stator vanes, ring of rotating blades, mixer/ejector pump to increase the flow volume through the turbine while rapidly mixing the low energy exit flow with high energy bypass fluid flow. Here the diffuser related effects are used - the increasing the flow velocity at the output of nozzle like structure. The energy of increased speed flow is used to draw the low speed air flows occurred after the rotor's blades. But here as the air source for the ejectors (diffusers) the outer wind streams are used. The wind flows entry into turbine meet the high resistance in pivotal area of the rotor where the hub and the blades' roots are presenting. That brings to decreasing the turbine's efficiency. The aerodynamic flows' distribution is formed/forced by the significant constructive elements - the mixer/ejector's shrouds. These elements have significant drags sharply reducing aerodynamic effectiveness, take large space, have high weight and, finally, limit the possible embodiments of such type turbines by small ones. The present invention has been made with the aim of solving the noted above and additional problems, and it is an object of the present invention to provide an effective aerodynamics of the rotor increasing the wind energy captured by the turbine. Another object of the present invention is to decrease the speed differences between tip and root parts of the blades, decrease audible and infra-sound noise emission.

Still another object of the present invention is to provide the stability, reliability of turbine performance, decrease the stresses in the turbine elements, provide flexible adapting the turbine to the current wind parameters, provide optimal work parameters for the electric generation.

Yet another object of the present invention is to provide a universal configuration being applicable for all diapason of generated power - from small wind turbines 1KW till giant wind turbines 100MW.

A further object of the present invention is to provide the safety for birds.

SUMMARY OF THE INVENTION The present invention provides a wind turbine with two (or more) pluralities of the blades attached to the rim. The configuration of this turbine is applicable both for upwind and downwind turbines types. The blades configured to provide in the rotor a pivotal diffuser. The air streams passing through the diffuser indirectly enhance the aerodynamics of the rotor and, accordingly, increase efficiency of the present wind turbine.

The present turbine has a tower comprising stationary standing- and turning yaw-portions. The standing-portion is established onto land, sea bottom, floating platform, etc. The yaw-portion is jointed to the top part of the standing-portion through the turning yaw-mechanism. The yaw-portion carries the rotor. I.e. the rotor itself does not perform yaw turnings. It is placed definite onto and relative to the yaw-portion. The absence of necessary of yaw related turnings allows to not use hub, and hub related (more particular, nacelle related) yaw-gear. In the common turbines all being very hard loads and stresses are concentrating in these elements, the carrying elements have a small bases providing large bending moments, loads, etc. In the present turbine such extremely loaded points and in-one-point-concentrated forces are absent, the supporting bases are very long and reliable.

Since through the yaw turning the arms with the rotor always are being one-way oriented relative wind direction it is possible to use in the present turbine the unidirectional aerofoil shape of the arms. This drastic decreases the drag forces, enhances the aerodynamic of the rotor, and as result the efficiency of the present turbine is grown. Also aerofoil shape of the arms allows to use the present turbine with high effectiveness both as upwind and downwind mode turbine - the arms even located in-front of the rotor bring a very low vortices or other negative things to the air streams.

In the preferred embodiment the yaw-portion has two arms constituting a near to V-shape construction. The arms and the root-part of the yaw-portion are carrying four roller based components of rotor suspend set (RS-SET). The roller components are in mechanical rotatable contact with the rim of the rotor. They support the rim at four points and are defining the rim's (and accordingly the rotor's) suspension relatively yaw-portion of the wind turbine. I.e. the rotor itself does not perform any yaw turning - the yaw to wind related orientation is performing the yaw-mechanism. The rim and two lowest roller components of RS-SET constitute at single-stair gear with high enough rotation transmission ratio. That allows to build the present turbine without

conventional gear-boxes (being almost "standard" part of big wind turbines, bringing hard weight, sound noise and energy losses), but get a suitable revolution speed to spin the generator(s).

Two upper roller based components of RS-SET mounted onto top parts of the arms do not carry significant loads, their main function is to fix the rotor relative the yaw-portion.

The rotor has two blades' assembles attached to the rim. The six inner-blades are attached so to be inward radial oriented to the rim's center. The twelve upper-blades are attached so to be outward radial oriented to the rim's periphery. The number of outer-blades is two times more than number of the inner-blades. That allows to the present turbine to much more effective capture the wind flows at the periphery of the rotor (where in the common turbines there are very big distances between the blades; for example, in the three-blade turbine with rotor diameter 100 m the distances between the blade tips will be more than 100 m and part of wind streams merely passes between the blades without to interact with them). Each blade has a rotating supporting post to which the blade is attached and which provides the angle-of-attack regulating. The multiple blade configuration of the rotor is well visible to the birds which may lightly overcome the rotor through flight. In addition, the rotor is rotating at very low rotational speed - this is possible since very high rotation transfer ratio of the gear rim-to-roller. Low rotational speed provides decreasing of stresses and loads, decreases noise emission, allows to use more effective angles-of-attack for the blades, allows to increase the square of the blades. As result, we get increased power of the rotor. Also, the low rotational speed additionally decreases the danger for the birds.

The ensemble of six inner-blades provides the free-to-pass area in the pivotal zone of the rotor. Of course the air streams of this area do not interact with the blades and do not bring energy to the rotor at direct mode. But these streams bring additional energy by indirect mode.

The wind flows through interacting with the rotor produce an increased pressure in front of the rotor. Part of the air from this zone passes through the free pivotal zone and goes out with risen speed - the free pivotal zone works as giant diffuser producing a giant air jet. Outgoing high speed air flows (jet) are mixing with low speed air flows passed the inner-blades and are dragging these low speed flows from the rotor forming the pressure decreasing (and, accordingly growth the pressure difference between air before and after the rotor's disk). This increased pressure difference provides more active air flow passing through the rotor, and accordingly elevates the rotor efficiency. Therefore, the jet produced by the pivotal zone in the present turbine works at indirect mode and not being lost - it brings additional power.

Two lowest roller based components of RS-SET in the discussed preferred embodiment capture the rotating from the rim and through a rotation transfer means (RTM) transfer the rotation to one or two generators. The generators are placed into the standing-portion at very low height in the closed space. That decreases the load moments, provides additional protection from environmental conditions and protection from noise emission.

In the first embodiment the rotor has inner-rim. One of the variants is that the inner-rim is attached to the tips of the inner-blades. Other variant is that the turbine has three blades' ensembles - one of outer-blades and two of inner-blades. One of ensemble of inner-blades has three blades with long enough length (equal roughly radius of the rim minus radius of the inner- rim). To the tips of these blades the inner-rim is attached. Another ensemble of inner-blades contains three more short blades. They extend from the rim inward to the rim's center, but do not reach the inner-rim. Such configuration provides optimal distances between the blades through all rotor's square both near to the rotor's axis as well as at periphery of the rotor. The twelve outer-blades are allocated analogously to noted above preferable embodiment. The inner-rim is used to increase the diffuser effect for the pivotal zone air streams.

In another embodiments the arms may have different form. For example, it may be used single arc- or pear-like shape arm carrying one or more roller components of the RS-SET.

In the still another embodiments the present turbine comprise several (one, two, three, etc.) generators preferably having different power. Through operating accordingly to different wind conditions the roller based components of RS-SET and the RTM transfer the rotation energy to any certain ensemble of generators (usually being according in power level with the wind power factor). That allows at the certain moment to use only certain generators at optimal regimes and disconnect generators of exceeding power.

In the yet another embodiment the rotor's suspension is provided by magnet based components of the RS-SET. That significantly decreases the friction in the present turbine.

In alternate embodiments the present turbine may be configured to operate in upwind or downwind mode. In small embodiments the present turbine may be equipped with vane providing yaw

orientation of the yaw-portion relative wind direction.

BRIEF DESCRIPTION OF THE DRAWINGS FIG.l illustrates the preferable embodiment of the present wind turbine.

FIG.2 illustrates the same preferable embodiment of the present wind turbine at the perspective view to provide clear understanding the turbine's configuration.

FIG.3 depicts the perspective view of the tower. FIG.4 shows the vertical cut of the wind turbine and possible location of some roller based components of the rotor suspend set (RS-SET), the rotation transfer means (RTM), and the generator.

FIG.5 depicts one of possible variants of the rim's suspension at the top part of the arm on the roller based component of the RS-SET.

FIGs. 6A and 6B illustrate one of possible embodiment of the wind turbine with pear-like shape of arm. FIG.6A depicts the tower of the wind turbine comprising the standing-portion and the yaw-portion equipped with four roller based components of the RS-SET. FIG.6B depicts the fully assembled wind turbine having pear-like arm's shape - the tower (with said pear-like shape arm) and the rotor suspended by said four roller based components of the RS-SET. FIG.7 depicts one of possible variants of the rotor's configuration - the rotor with central additional rim.

FIG.8 depicts another possible variant of the rotor's configuration - the rotor with two ensembles of the inner-blades, where blades from one ensemble have the length substantially equal to the radius of the rim and attached one with another through a central spindle.

DETAILED DESCRIPTION OF THE INVENTION

FIG.l illustrates the preferable embodiment of the present wind turbine. FIG.2 illustrates the preferable embodiment of the present wind turbine at the perspective view to provide clear understanding the turbine's configuration. Both FIG.l and FIG.2. represent the same turbine and have the same components' numbering. At the FIG. l and FIG.2 they are shown: ground 1 onto which the wind turbine is established by use a foundation (it is not visible and therefore not signed individually); standing-portion 2 being fixedly vertically mounted onto the ground 1; root-part 3 of yaw-portion mounted onto the top of the standing-portion 2, the root-part 3 of the yaw-portion is jointed with the standing-portion 2 through the yaw-mechanism (it is located into the yaw -portion and is not visible and not signed); onto the root-part 3 two arms 4-1 and 4- 2 are mounted, the arm 4-1 is substantially extending upward and left-ward, the arm 4-2 is substantially extending upward and right- ward from the root-part 3; the root-part 3 and the arms 4-1 and 4-2 constitute the yaw -portion (not singed individually) of the present wind turbine; onto the root-part 3 two roller based components of the rotor suspend set (RS-SET) are mounted - left component of the RS-SET 5-1 and right component of the RS-SET 5-2; these RS-SET's components 5-1 and 5-2 are mechanically carrying the most weight of the rim 6 and attached to the rim 6 ensemble of inner-blades 7 and ensemble of the outer-blades 8; the rim 6, the inner-blades 7 and the outer-blades 8 constitute the rotor (not signed individually) of the present wind turbine; at the top parts of the arms 4-1 and 4-2 they are mounted two additional roller based components of the RS-SET - 5-4 and 5-3 accordingly, they do not carry a significant weight or loads but they provide a definite suspension of the rotor relative the yaw- portion; at the center of the rotor there is a free pivotal zone 9 constituting a large diffuser.

The components 5-1, ... 5-4 of the RS-SET provide the rotor the rotatable and definite suspension relative the yaw-portion. The rotor does not perform any yaw related turnings through guiding the wind direction. This function performs the yaw-portion. Therefore, the yaw -portion always has a unidirectional orientation relative the wind. That allows to build the yaw -portion, generally the arms (in the discussed case of the preferable embodiment - the arms 4-1 and 4-2), with streamlined aerofoil shape through the wind line passing. That at a significant degree decreases at drag forces of the present wind turbine's tower and decreases the load moments at yaw -portion, yaw-mechanism, standing-portion, foundation, etc. Also this allows to use the present turbine both in upwind as well as in downwind mode operating.

FIG.3 illustrates said streamlined aerofoil shape of the arms 4-1 and 4-2. The round pointer illustrates the turning of the yaw-portion through the wind direction guidance. The plane passing substantially vertically through the arms 4-1 and 4-2 and the standing-portion 2 we name "sagittal plane". The vertical plane being perpendicular to the sagittal plane and parallel to the wind direction we name "longitudinal plane". The rotor and, accordingly, its swept area are substantially located at the sagittal plane of the present turbine to capture maximal possible air flow. The RS-SET 5-1,...5-4 is mounted onto the yaw -portion and, therefore is turning together with it. I.e., the suspension of the rotor is performed by the four points located at a significant distances one from another providing a large bases. Such bases drastic decrease the yaw related moments and loads appeared in the rotor and in the tower's elements.

FIG.4 shows more particular one of possible schemes of the rotor suspension. The lowest roller based component of the RS-SET 5-2 performs generally the supporting function. It supports the rotor through supporting the rim 6. In the component 5-2 of the RS-SET it may be used one- roller scheme where the roller is located from below the rim 6. Through the supporting functions the component 5-2 of the RS-SET is rotating in accordance with the rim 6 rotation (for this a special path in the rim 6 may be provided, this path may be toothed as well as the roller 5-2 too). This rotation is sent to the rotation transfer means 10, which transfers said rotation to the generator 12. It is obvious that the rotation transfer means 10 and, especially, the generator 12 are mounted at the very low positions. That drastically decreases the load moments onto/into the present wind turbine. Also that allows to perform the installation and maintenance works very simply and with low cost.

At the top part 11 of the arm 4-1 (see FIG.4) the upper roller based component of the RS-SET is shown, it comprises (in the discussed embodiment) two rollers 5-4-1 and 5-4-2. These rollers 5-4-1 and 5-4-2 fix the rim 6 from both upward and downward shifts. Thus, the ensemble of the components of the RS-SET 5-1, ....,5-4 provide a fixed position (suspension) of the rotor relative the yaw-portion while the rotor has possibility to be rotated by the wind.

FIR.5 at a much more particular degree depicts at possible suspension of the rim 6 at the top part 11 of the arm 4-1. They are shown: the arm 4-1 having the top part 11; two rollers 5-4-1 and 5-4-2 of the upper component 5-4 (see FIGs 1, 2, 3) of the RS-SET, said rollers 5-4-1 and 5-4-2 (see FIG.5) are mounted onto shafts 5-4-1-3 and 5-4-2-3 accordingly; the said shafts 5-4- 1-3 and 5-4-2-3 are rotatable supported by the bearings 5-4-1-1, 5-4-1-2, 5-4-2-1, and 5-4-2-2 accordingly. Two rollers 5-4-1 and 5-4-2 are fixing the rim 6 from up- and down- and for- and backward shifts since said rollers 5-4-1 and 5-4-2 are rotary passing through the upper and inner paths (not signed individually) provided onto the rim 6.

FIGs 6A and 6B illustrate another possible shape of the yaw-portion - the single arm with pearlike shape. This arm 4 (see FIG.6A) provides the similar positions of the upper roller based components 5-3 and 5-4 of the RS-SET. The pear-like arm 4 may be used if additional strength and rigidity are necessary. FIG.6B represents the view of the wind turbine with said pear-like shape arm 4 (the signs are analogous to noted above FIGs 1, 2, 3).

FIG.7 depicts one of possible variants of the rotor's configuration - the rotor with central additional rim 13. This additional central rim 13 increases effect of diffuser and increases the aerodynamic efficiency of the rotor. FIG.8 depicts another possible variant of the rotor's configuration - the rotor with two ensembles of the inner-blades 7-1 and 7-2, where blades from the ensemble 7-2 have the length substantially equal to the radius of the rim and attached one with another through a central spindle 14. The spindle 14 has small dimensions and does not affect onto the diffuser passes of the air flows in the pivotal area. The tips of the blades 7-2 in the diffuser zone, singed with char "d" have a null angle-of-attack relative the air flows into the pivotal zone and do not affect onto the diffuser effect in this zone too. Such rotor's configuration may be used for increasing the rigidity of the rotor.

To suspend the rotor in the RS-SET may by used the magnet effects based components providing the support forces between rim 6 and one or more components of the RS-SET. The magnet forces may be provided by permanent or/and by electro-magnet means. The magnet suspense is preferably to combine with mechanical, generally roller based suspense

components. Such suspense may significantly decrease the friction between rim and components of the RS-SET.

Small embodiments of the present turbine may be equipped with a vane attached to the yaw- portion and configured to orient the yaw-portion accordingly the wind direction.