A wind-driven generator set
Through the multi-step runner structure of the gas power unit, the problem of large volume and difficulty in installing the wind wheels in conventional wind turbines is solved, and efficient wind conversion and simple structural design are achieved, which is suitable for wind power generation on special terrain.
Patent Information
- Application Number
- CN201810944463.1
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- Filing Date
- 2018-08-19
- Publication Date
- 2025-01-17
- Estimated Expiration
- 2038-08-19
AI Technical Summary
The wind wheels of conventional wind turbines have large volume and low wind flow utilization, resulting in low conversion rate, and are difficult to install on steep terrain, short maintenance cycle and high cost.
The gas power device is adopted, including the outer ring and the core. Through the multi-step flow channel structure, the air flow enters through the intake passage, and the driving recess acting on the outer ring is gradually ejected, generating thrust to push the outer ring to rotate, realizing power output. It is also discharged through the exhaust passage, with a simple overall structure and small size, suitable for special terrain.
Improves torque transfer efficiency and air flow utilization, reduces overall weight and volume, makes transportation and assembly easy, and can be effectively applied to steep terrain such as canyons or mountain walls.
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Figure CN110836129B_ABST
Abstract
Description
Technical Field
[0001] The invention relates to the field of wind power generation, and in particular to a wind-driven generator set. Background Art
[0002] Wind power generation refers to converting the kinetic energy of wind into electrical energy. Conventional wind turbines include wind rotors and generators. The wind rotors contain blades, hubs, reinforcements, etc. The wind rotors are supported by a tower, and the wind source drives the wind rotors to rotate. The rotation of the wind rotors drives the generators to rotate through the transmission shaft, thereby generating electricity. Conventional wind turbines have large wind rotors, low wind flow utilization, and low conversion rates. They are also troublesome to transport and assemble.
[0003] Furthermore, conventional wind turbines are generally installed in relatively flat areas, such as plains with abundant wind sources. In some steeper canyons or mountain walls, where the wind sources are abundant and the wind direction is fixed, the installation is difficult if the conventional wind turbine structure is used. The wind rotor needs to be extended a certain distance, and the tower and wind rotor structure are easily damaged, resulting in a short maintenance cycle, which increases the difficulty and cost of maintenance. Summary of the invention
[0004] To this end, the present invention provides a new wind-driven generator set, which can replace the original wind-driven generator set, has a simpler structure and a smaller volume, and can also well overcome the defects of conventional wind power generation components, and can be well applied to special terrains, such as steep canyons or mountain walls.
[0005] To this end, the present invention provides a wind-driven generator set, including a gas power device and a power generation component, wherein the gas power device includes:
[0006] An outer ring, whose inner ring surface is provided with a plurality of driving recesses in the circumferential direction;
[0007] A core body is coaxially arranged in the outer ring and can rotate relative to the outer ring, and the outer ring surface of the core body is provided with at least one nozzle, at least one discharge port, and at least one flushing channel located between the nozzle and the discharge port;
[0008] at least one air inlet passage connected to at least one nozzle; and
[0009] at least one exhaust passage connected to at least one exhaust port;
[0010] The air flow enters from the air inlet channel, is ejected step by step through the nozzle of the core body and the secondary flow channel, acts on at least two driving recesses on the circumference of the outer ring, generates thrust on these driving recesses to drive the outer ring to rotate and do work, and finally, the air flow is discharged through the exhaust port of the core body and the exhaust channel;
[0011] The rotation work of the outer ring is used as kinetic energy for the power generation component to generate electricity.
[0012] Furthermore, at least one air inlet channel, at least one nozzle, at least two driving recesses, at least one primary flow channel, at least one discharge port and at least one exhaust channel form an independent working unit, and the gas power device includes at least one independent working unit.
[0013] Furthermore, the nozzle and the secondary flow channel on the core body are connected to the driving recess corresponding to the outer ring, and the secondary flow channel is arranged along the circumference of the core body or the outer ring.
[0014] Furthermore, an air intake passage and an air exhaust passage are formed in the core.
[0015] Furthermore, the core includes:
[0016] An air inlet passage, which forms a nozzle on the peripheral surface of the core body, and whose direction is an arc line extending from the middle to the outside, and the nozzle is connected with the driving concave portion corresponding to the outer ring to form a first-stage flow channel;
[0017] The secondary flow channel is an arc line extending from the edge of the core body inward and then bending to the edge. Each secondary flow channel is connected with the front and rear driving recesses corresponding to the outer ring, forming N-step flow channels along the circumference of the core body, where N is a natural number ≥ 2;
[0018] Each step of the flow channel cooperates with the corresponding driving recess of the outer ring to form a multi-step stroke structure with decreasing air flow energy.
[0019] Furthermore, the secondary flow channel includes a return channel and a communicating stroke channel, the return channel is communicated with a driving recess corresponding to the outer ring, and the stroke channel is communicated with another driving recess.
[0020] Furthermore, the direction of the core air inlet channel is a logarithmic spiral extending from the middle to the outside, the pole of the logarithmic spiral is set on the central axis of the core, and the direction angle of the logarithmic spiral is 15°-45°.
[0021] Furthermore, an air inlet channel is provided on the core body, and its direction is a logarithmic spiral extending from the middle to the outside, and the direction of the stroke channel of the secondary flow channel is a logarithmic spiral. The direction of the logarithmic spiral of the stroke channel of the secondary flow channel is roughly the same as the direction of the logarithmic spiral of the air inlet channel.
[0022] Furthermore, the gas power device also includes a shaft, and the outer ring and the core body are coaxially arranged on the shaft.
[0023] Furthermore, the gas power device also includes a shaft, the outer ring is coaxially arranged on the shaft with the core body, and the shaft is provided with inlet and outlet shaft passages which are respectively connected to the inlet channel and the exhaust channel of the core body.
[0024] Furthermore, the air inlet and outlet shaft channels in the shaft form an air inlet and an air outlet, and the air inlet and outlet shaft channels are non-connected structures.
[0025] Furthermore, the outer ring is matched with the shaft through the side plates to form a closed space, and the core body is arranged in the closed space and is connected and fixed to the shaft.
[0026] Furthermore, the air inlet channel, the nozzle, the driving recess, the secondary flow channel, the exhaust port and the exhaust channel in the independent working unit constitute an air flow path.
[0027] Furthermore, the gas power device includes more than two independent working units to form a multi-stage driving structure, and is arranged along the circumference of the core or the outer ring.
[0028] Furthermore, more than two driving recesses are arranged on the inner ring surface of the outer ring, each driving recess has a contour bottom surface and a driving surface, and the contour line of the contour bottom surface is a logarithmic spiral line, and its pole is arranged at the center of the core body.
[0029] Furthermore, it also includes a wind boosting device, the outlet of which is connected to the air intake passage to allow the boosted air flow to enter from the air intake passage.
[0030] Furthermore, the wind boosting device includes but is not limited to a wind-guiding boosting channel or a turbocharger.
[0031] Furthermore, the outer ring of the gas power device drives the rotor of the power generation component through a transmission device, and the rotation of the outer ring drives the rotor of the power generation component to rotate, thereby generating electricity.
[0032] Furthermore, the outer ring of the gas power device replaces the rotor of the power generation component and is directly connected to the coil of the power generation component. The rotation of the outer ring drives the coil to rotate to achieve power generation.
[0033] The technical solution provided by the present invention has the following beneficial effects:
[0034] The wind-driven generator set provided by the present scheme replaces the structure of the conventional wind wheel with the gas power device of this scheme. The core of the gas power device is provided with multiple-stage flow channels, namely, the air inlet channel serves as the first-stage flow channel, and each secondary flow channel serves as the second-, third-, fourth-...,..., flow channels. The air flow acts on the driving recess of the outer ring from the first-stage flow channel, and the driving recess communicates with the second-stage flow channel. Then, after returning to the second-stage flow channel, it acts on another driving recess of the outer ring, and so on, until the air flow is discharged from the exhaust channel. The whole process is carried out in the forward direction of the outer ring rotation direction, with large torque, high transmission efficiency, high air flow utilization rate, and the output torque further increases with the increase of rotation speed.
[0035] At the same time, the flow channels arranged around the core effectively reduce the volume of the entire device. The more inlet flow channels are set on the core, the lower the overall weight is, which further improves the output speed and efficiency of the device. On the basis of the same wind flow rate, the wind flow utilization rate is high, the torque is large, the speed is high, and the transmission efficiency is high. The whole machine has a simple structure and a small volume, which makes transportation and assembly simple; at the same time, the significant reduction in volume allows it to be well used in special terrains, such as steep canyons or mountain walls. BRIEF DESCRIPTION OF THE DRAWINGS
[0036] Figure 1 Schematic diagram of the gas power device in the first embodiment.
[0037] Figure 2 It is a side view of the gas power device in the first embodiment along the axis A.
[0038] Figure 3 It is a side view of the gas power device in the first embodiment along the axis B.
[0039] Figure 4 It is a cross-sectional view of the gas power device in the first embodiment.
[0040] Figure 5 This is another layout diagram of the gas power device in Example 1.
[0041] Figure 6 It is a driving connection schematic diagram of the gas power device in the first embodiment.
[0042] Figure 7 It is a schematic diagram of the gas power device in the second embodiment.
[0043] Figure 8 It is a side view of the gas power device in the second embodiment along the axis C.
[0044] Fig. 9 It is a side view of the gas power device in the second embodiment along the axis D.
[0045] Fig.10 It is a radial cross-sectional view of the gas power device in the second embodiment.
[0046] Fig.11 It is a structural diagram of the wind source collection component in the third embodiment. DETAILED DESCRIPTION
[0047] To further illustrate the various embodiments, the present invention provides drawings. These drawings are part of the disclosure of the present invention, which are mainly used to illustrate the embodiments and can be used in conjunction with the relevant descriptions in the specification to explain the operating principles of the embodiments. With reference to these contents, a person of ordinary skill in the art should be able to understand other possible implementations and advantages of the present invention. The components in the figures are not drawn to scale, and similar component symbols are generally used to represent similar components.
[0048] The present invention will now be further described with reference to the accompanying drawings and specific implementation methods.
[0049] Embodiment 1
[0050] The present embodiment provides a wind-driven generator set, including a gas power device and a power generation component. Figures 1 to 4 As shown, the gas dynamic device comprises: an outer ring 1, whose inner ring surface is provided with a plurality of driving recesses 11 in the circumferential direction; a core body 3, which is coaxially arranged in the outer ring 1 and can rotate relative to the outer ring, and the outer ring surface of the core body 3 is provided with at least one nozzle 301, at least one discharge port 302, and at least one primary flushing channel 300 located between the nozzle and the discharge port;
[0051] At least one air inlet passage 31 connected to at least one nozzle 301; and
[0052] at least one exhaust passage 310 connected to at least one exhaust port 302;
[0053] The air flow enters from the air inlet channel 31, and is ejected step by step through the nozzle 301 of the core body 3 and the secondary flow channel 300, acting on at least two driving recesses 11 on the circumference of the outer ring 1, generating thrust on these driving recesses 11 to drive the outer ring 1 to rotate and do work, realizing continuous power output, and finally, the air flow is discharged through the exhaust channel through the exhaust port of the core body 3. The gas power device also includes a shaft 2, and the outer ring 1 and the core body 3 are coaxially arranged on the shaft 2.
[0054] like Figure 4 As shown, the air inlet channel 31 and the exhaust channel 310 are formed in the core body 3, and the nozzle 301 and the secondary flow channel 300 on the core body 3 are connected with the driving recess 11 corresponding to the outer ring 1, wherein the secondary flow channel 300 and the corresponding driving recess 11 are arranged alternately and connected in sequence, and the secondary flow channel 300 is arranged along the circumference of the core body or the outer ring.
[0055] like Figure 4 The core 3 includes: an air inlet channel 31, which forms a nozzle 31 on the peripheral surface of the core, and its direction is an arc line extending from the middle to the outside, and the nozzle 301 is connected with the driving recess 11 corresponding to the outer ring to form a first-stage flow channel;
[0056] The secondary flushing channel 300 is an arc line extending from the edge of the core 3 inward and then bending to the edge. Each flushing channel 300 is connected with the front and rear driving recesses 11 corresponding to the outer ring 1, forming N-stage flow channels along the circumference of the core, where N is a natural number ≥ 2. It should be noted that if it is a 2-stage flow channel, it includes the 1st stage flow channel (inlet channel) and the 2nd stage flow channel (primary flushing channel); if it is a 3-stage flow channel, it includes the 1st stage flow channel (inlet channel), the 2nd stage flow channel (primary flushing channel), the 3rd stage flow channel (another secondary flushing channel), ...
[0057] Each step of the flow channel cooperates with the corresponding driving recess of the outer ring to form a multi-step stroke structure with decreasing air flow energy.
[0058] The gas power device can be designed according to the load requirements, in which the core 3 can be set to a 2-stage flow channel, a 3-stage flow channel, or more stages of intake flow channels. Each stage cycle performs work, fully utilizes energy, and maximizes the use efficiency to meet the output torque and speed requirements.
[0059] like Figure 5 Schematic diagram of a 4-stage flow channel. After the compressed air flow enters from the 1st-stage flow channel 311, it passes through the 2nd, 3rd, and 4th-stage flow channels 312, 313, and 314, and is ejected to act on the corresponding driving recess 11, and finally is output through the exhaust flow channel 310; Figure 4 This is a schematic diagram of the 5-stage intake air duct. The working process is the same as Figure 5 The schematic is similar. Figure 5 The secondary flow channel 300 includes a return channel and a connected stroke channel, such as Figure 5 The return path 3131 and the connected stroke path 3132 in the third-stage flow channel, the return path 3131 is connected to the driving recess corresponding to the outer ring, and the stroke path 3132 is connected to another driving recess.
[0060] See also Figure 1 The gas power device also includes a shaft 2, the outer ring 1 is coaxially arranged on the shaft 2 with the core 3, and the shaft 2 is provided with inlet and outlet shaft channels 21, 210 respectively connected to the inlet channel 31 and the exhaust channel 310 of the core 3. The inlet and outlet shaft channels in the shaft form an inlet and an outlet, and the inlet and outlet shaft channels are non-connected structures. The outer ring 1 is matched with the shaft 2 through the side plates 41, 42 to form a closed space, and the core 3 is arranged in the closed space and connected and fixed to the shaft 2. In this solution, the core 3 is provided with at least 2 steps of flow channels, each step of the flow channel is connected to the driving recess corresponding to the outer ring, and finally the air flow is discharged by the exhaust flow channel.
[0061] See also Figure 1 In this solution, the core body 3 can be formed by the cooperation of a left core body and a right core body, and the cooperation surfaces of the left and right core bodies are provided with an air intake channel 31 and an exhaust channel 310. The core body 3 can also be integrally cast.
[0062] See also Figure 1 , Figure 4 This embodiment is a primary drive structure. An air channel is arranged circumferentially on the core 3 to form a primary drive structure. The air channel is also called an independent working unit. An air inlet channel 31, a nozzle 301, at least two driving recesses 11, at least one primary flow channel 300, a discharge port 302 and an exhaust channel 310 on the core 3 and the outer ring 1 form an independent working unit. The gas power device includes at least one independent working unit. The air inlet channel 31, the nozzle 301, the driving recess 11, the secondary flow channel 300, the discharge port 302 and the exhaust channel 310 in the independent working unit constitute an air flow path.
[0063] See also Figure 1 , Figure 4 or Figure 5 In this solution, more than two driving recesses 11 are arranged on the inner ring surface of the outer ring 1, each driving recess has a contour bottom surface 111 and a driving surface 112, the contour line of the contour bottom surface 111 can be a common arc line or a spiral line, when the contour line of the contour bottom surface is a logarithmic spiral line, its pole is set on the axis, each driving recess 11 is also connected with the adjacent step flow channel so that the air flow entering the previous step flow channel is output by the next step flow channel.
[0064] In this solution, the direction of the air inlet channel of the core body 3, namely the first-stage flow channel, can be a common arc line or a spiral line, and the direction of the stroke channel in each secondary flow channel, namely the Nth-stage flow channel, can also be a common arc line or a spiral line.
[0065] like Figure 4 and Figure 5 In this embodiment, the core 3 is provided with an air inlet channel 31, which runs in a logarithmic spiral extending from the middle to the outside. The stroke channel of the secondary flow channel 300 runs in a logarithmic spiral, and the logarithmic spiral of the stroke channel of the secondary flow channel runs in a direction substantially the same as the logarithmic spiral of the air inlet channel. The air inlet channel of the core 3 runs in a logarithmic spiral extending from the middle to the outside, and the pole of the logarithmic spiral is set on the central axis of the core. The logarithmic spiral runs in an angle of 15°-45°. The smaller the angle, the longer the flow channel and the more the loss. The larger the angle, the smaller the tangential component of the driving outer ring.
[0066] See also Figure 1 , Figure 2 and Figure 3 In this embodiment, the inlet and outlet shaft channels 21, 210 in the shaft 2 form an inlet and an outlet, and the inlet and outlet shaft channels are non-connected structures. The inlet and outlet of the shaft can be set at one end or both ends of the shaft, the inlet shaft channel 21 is connected to the inlet channel 31 of the core body, and the shaft outlet extends axially to form the outlet shaft channel 210, which is connected to the exhaust channel 310 of the core body.
[0067] Among them, the power generation component 103 is a conventional generator structure, including: a rotor shaft, a coil arranged on the rotor shaft and a stator winding. The coil is energized to generate a magnetic field, and the rotor shaft rotates to drive the coil to rotate, generating a rotating magnetic field. The coil of the stator winding cuts the magnetic lines of force to generate current and output it. Of course, in the existing generator structure, components such as carbon brushes, conductive slip rings, and stator cores are usually provided. Their specific connection structures are all existing structures and will not be described in detail. Depending on the structure, the existing power generation component can be an existing two-phase AC generator, a DC generator, a three-phase AC generator, etc.
[0068] The rotation work of the outer ring 1 is used as kinetic energy for the power generation component 103 to generate electricity. In this specific embodiment, the outer ring 1 drives the rotor shaft connected to the power generation component through a transmission device, and the rotation work of the outer ring drives the rotor shaft of the power generation component to rotate to achieve power generation. Figure 1 As shown, in this embodiment, a plurality of assembly holes are provided on the circumferential side of the outer ring. Figure 6 As shown, the bolt 60 passes through the assembly hole and is fixedly screwed on a rotating shaft 60, and the rotating shaft 60 is connected to the rotor shaft of the power generation component to realize the driving connection between the outer ring and the rotor shaft of the power generation component. Of course, in other embodiments, the driving connection between the outer ring and the rotor shaft of the power generation component can also be realized by other transmission devices, such as a gear transmission mechanism, that is, an outer tooth is provided on the outer ring to facilitate the output of kinetic energy through gear transmission; another example is that the outer ring has a belt groove to output kinetic energy through belt transmission; another example is that the outer ring has a mounting flange, which can be conveniently installed with a coupling to output kinetic energy; and so on.
[0069] In the wind-driven generator set, the air flow needs to be introduced into the air intake passage, and preferably introduced into the air intake passage after wind boosting. This can be achieved by using all known technologies, such as a wind-guiding boosting flow channel designed by fluid mechanics (to achieve wind boosting at the outlet), a turbocharger, etc.
[0070] The gas power device involved in this application refers to a device that can convert air flow energy into mechanical rotation, wherein the device may include other components in addition to the necessary outer ring, core body and its corresponding recessed structure or flow channel structure design; for example, it may include a housing and a sealing structure that provide external protection, or a coupling that provides torque transmission. The core body and the outer ring are made of hard materials, not limited to metals, metal alloys, plastics, and composite materials. The processing method of the recessed structure or flow channel structure of the core body and the outer ring can be realized by all known production means, including but not limited to die casting, forging, extrusion, 3D printing, etc.
[0071] Figure 1 and Figure 4It should be noted that the air inlet channel 31 and the exhaust channel 310 of the core body and the air inlet shaft channel 21 and the air outlet shaft channel 210 do not correspond to each other according to the drawing rules, but for the sake of illustration, Figure 1 The air inlet channel and the exhaust channel of the central core body refer to the air inlet channel and the exhaust channel. Figure 7 and Fig.10 A similar schematic diagram is shown here.
[0072] Embodiment 2
[0073] The structure of a wind-driven generator set provided in this embodiment is substantially the same as that of the embodiment 1, except that: Figures 7 to 10 The gas power device includes two independent working units to form a two-stage driving structure, that is, two air channels are arranged circumferentially on the core 3, each air channel includes an intake channel 31 of more than one order and a secondary flow channel 300 and an exhaust flow channel arranged circumferentially along the core 3. The gas power device comprises an outer ring 1, whose inner ring surface is provided with a plurality of driving recesses 11 on the circumference; a core body 3, which is coaxially arranged in the outer ring 1 and can rotate relative to the outer ring, and the outer ring surface of the core body is provided with two groups of nozzles and exhaust ports, and at least one primary flow channel is provided between each group of nozzles and exhaust ports; the core body is provided with two air inlet channels 31, 32, which correspond to the connected nozzles; and two exhaust channels 310, 320, which correspond to the connected exhaust ports; two air flows enter from the two air inlet channels of the core body respectively, and are ejected step by step through the nozzles of the core body 3 and the secondary flow channels 300, acting on the corresponding driving recesses 11 on the circumference of the outer ring, generating thrust on these driving recesses to drive the outer ring 1 to rotate and do work, thereby realizing power output, and finally, the air flow is discharged through the exhaust port of the core body through the exhaust channel. The above-mentioned one air inlet channel, one nozzle, a corresponding number of driving recesses and corresponding secondary flow channels, exhaust ports and one exhaust channel form an independent work unit.
[0074] The gas power device also includes a shaft 2, on which the outer ring 1 and the core 3 are coaxially arranged. The shaft 2 is provided with air inlet channels 21, 22 and air outlet channels 210, 220 which are respectively connected to the air inlet channels 31, 32 and the air outlet channels 310, 320 of the core. The shaft 2 is provided with two air inlets and two air outlets corresponding to the air channels; the compressed air flows into the shaft 2 from the two air inlets, and is ejected through the air inlet channel of the core 3 to act on the driving recess 11 of the outer ring 1, generating thrust to drive the outer ring 1 to rotate and do work, and finally the compressed air flows back to the corresponding air outlet through the exhaust channel of the core 3, thereby realizing the continuous output of power.
[0075] Furthermore, in order to further increase the intake volume, in this embodiment, a wind boosting device is also included, specifically a conventional turbocharger, the compressor air outlet of the turbocharger is connected to the intake channels 31, 32 of the gas power device, the turbine inlet of the turbocharger is connected to the exhaust channels 310, 320 of the gas power device, and the exhaust gas flowing out of the exhaust channels 310, 320 of the gas power device drives the compressor impeller of the turbocharger to rotate, thereby supercharging the wind flow input into the intake channels 31, 32 of the gas power device. No power source is required, it is directly driven by the input airflow, and no other energy is consumed. Of course, in other embodiments, the wind boosting device can also use a mechanical supercharger device driven by electricity with lower energy consumption.
[0076] Embodiment 3
[0077] The present embodiment provides a wind-driven generator set, the structure of which is substantially the same as that of the embodiment 1 or the embodiment 2, except that: Fig.11 As shown, in this embodiment, it also includes a wind source collection component, which includes a collection port 71 and a wind-guiding and pressurizing flow channel 72. One end of the wind-guiding and pressurizing flow channel 72 is connected to the collection port 71, and the other end is connected to the air intake channel of the gas power device. The collection port 71 corresponds to the wind flow direction and collects the wind flow. The collected wind flow is guided by the wind-guiding and pressurizing flow channel 72 to the air intake channel of the gas power device.
[0078] Furthermore, the collecting port 71 is a bell-shaped structure, wherein the large bell-shaped portion of the collecting port 71 corresponds to the wind flow direction, and the small bell-shaped portion is connected to the wind guiding and pressurizing flow channel 72 .
[0079] The wind source collection component is added, and its collection port 71 can be set at a location where the wind flow is more concentrated, so as to better collect the wind flow and conduct it to the air intake channel of the gas power device through the wind guide and boost flow channel 72, so that the gas power device and the power generation component can be placed in a safer and more convenient location for easy operation and maintenance. For example, when it is set on a steeper mountain wall, the collection port 71 can be set at a higher position on the mountain wall to collect more wind flow, and the wind guide and boost flow channel 72 can be set along the mountain wall to extend to the foot of the mountain, and the gas power device and the power generation component can be set at the foot of the mountain.
[0080] Embodiment 4
[0081] The wind-driven generator set provided in this embodiment has the same structure as that of the first embodiment, except that, in this embodiment, the outer ring of the gas power device replaces the rotor shaft of the power generation component and is directly connected to the coil of the power generation component, and the rotation of the outer ring drives the coil to rotate to achieve power generation.
[0082] In this way, the gas power device can be directly installed on the power generation component without the need for an additional transmission device for power transmission. It is simpler in structure and smaller in size.
[0083] Through the wind-driven generator set provided above, the structure of the conventional wind wheel is replaced by the gas power device of this case. The core of the gas power device is provided with multiple-stage flow channels, that is, the air inlet channel serves as the first-stage flow channel, and each secondary flow channel serves as the second-, third-, fourth-...,..., flow channels. The air flow acts on the driving recess of the outer ring from the first-stage flow channel, and the driving recess is connected to the second-stage flow channel. Then, it returns to the second-stage flow channel and acts on another driving recess of the outer ring, and so on, until the air flow is discharged from the exhaust channel. The whole process is carried out in the forward direction of the rotation direction of the outer ring, with large torque, high transmission efficiency, high air flow utilization rate, and the output torque further increases with the increase of the rotation speed.
[0084] At the same time, the flow channels arranged around the core effectively reduce the volume of the entire device. The more inlet flow channels are set on the core, the lower the overall weight is, which further improves the output speed and efficiency of the device. On the basis of the same wind flow rate, the wind flow utilization rate is high, the torque is large, the speed is high, and the transmission efficiency is high. The whole machine has a simple structure and a small volume, which makes transportation and assembly simple; at the same time, the significant reduction in volume allows it to be well used in special terrains, such as steep canyons or mountain walls.
[0085] Although the present invention has been specifically shown and described in conjunction with the preferred embodiments, it should be understood by those skilled in the art that various changes may be made to the present invention in form and details without departing from the spirit and scope of the present invention as defined by the appended claims, all of which are within the scope of protection of the present invention.
Claims
1. A wind-driven generator set, comprising a gas power device and a power generation assembly, characterized in that: The gas powered device comprises: An outer ring, whose inner ring surface is provided with a plurality of driving recesses in the circumferential direction; A core body is coaxially arranged in the outer ring and can rotate relative to the outer ring, and the outer ring surface of the core body is provided with at least one nozzle, at least one discharge port, and at least one flushing channel located between the nozzle and the discharge port; at least one air inlet passage connected to at least one nozzle; and at least one exhaust passage connected to at least one exhaust port; An intake passage and an exhaust passage are formed in the core; The core includes An air inlet passage, which forms a nozzle on the peripheral surface of the core body, and whose direction is an arc line extending from the middle to the outside, and the nozzle is connected with the driving concave portion corresponding to the outer ring to form a first-stage flow channel; The secondary flow channel is an arc line extending from the edge of the core body inward and then bending to the edge. Each secondary flow channel is connected with the front and rear driving recesses corresponding to the outer ring, forming N-step flow channels along the circumference of the core body, where N is a natural number ≥ 2; Each step of the flow channel cooperates with the corresponding driving concave portion of the outer ring to form a multi-step stroke structure with decreasing air flow energy; The direction of the core air inlet channel is a logarithmic spiral extending from the middle to the outside, the pole of the logarithmic spiral is set on the central axis of the core, and the logarithmic spiral direction angle is 15°-45°; The air flow enters from the air inlet channel, is ejected step by step through the nozzle of the core body and the secondary flow channel, acts on at least two driving recesses on the circumference of the outer ring, generates thrust on these driving recesses to drive the outer ring to rotate and do work, and finally, the air flow is discharged through the exhaust port of the core body and the exhaust channel; The rotation work of the outer ring is used as kinetic energy for the power generation assembly to generate electricity; The outer ring of the gas power device is driven and connected to the rotor shaft of the power generation component through a transmission device, and the rotation of the outer ring drives the rotor shaft of the power generation component to rotate to achieve power generation; or the outer ring of the gas power device is directly connected to the coil of the power generation component, and the rotation of the outer ring drives the coil to rotate to achieve power generation.
2. The wind-driven generator set according to claim 1, characterized in that: At least one air inlet channel, at least one nozzle, at least two driving recesses, at least one primary flow channel, at least one discharge port and at least one exhaust channel form an independent working unit. The gas power device includes at least one independent working unit.
3. The wind-driven generator set according to claim 1, characterized in that: The nozzle and the secondary flow channel on the core body are connected with the driving recess corresponding to the outer ring, and the secondary flow channel is arranged along the circumference of the core body or the outer ring.
4. The wind-driven generator set according to claim 1, characterized in that: The gas power device also includes a shaft, on which the outer ring is coaxially arranged with the core body, and on which an inlet and an outlet shaft passage are opened, which are respectively connected to an inlet passage and an outlet passage of the core body.
5. The wind-driven generator set according to claim 2, characterized in that: The gas power device comprises more than two independent working units to form a multi-stage driving structure, and the units are arranged along the circumference of the core or the outer ring.
6. The wind-driven generator set according to any one of claims 1 to 5, characterized in that: More than two driving recesses are arranged on the inner ring surface of the outer ring, each driving recess has a contour bottom surface and a driving surface, the contour line of the contour bottom surface is a logarithmic spiral line, and its pole is arranged at the center of the core body.
Citation Information
Patent Citations
Wind driven generator set
CN209179821U