CN216477669U

CN216477669U - Aerogenerator aircraft nose positioner

Info

Publication number: CN216477669U
Application number: CN202220217986.8U
Authority: CN
Inventors: 韩玉霞; 李鑫; 汪建文; 金凯宁; 杨斌
Original assignee: Inner Mongolia University of Technology
Current assignee: Inner Mongolia University of Technology
Priority date: 2022-01-26
Filing date: 2022-01-26
Publication date: 2022-05-10
Anticipated expiration: 2032-01-26

Abstract

The utility model provides a aerogenerator aircraft nose positioner relates to aerogenerator technical field, has solved present because natural wind direction is changeable, can lead to the aircraft nose frequently to shake, causes the problem of wearing and tearing, including the aircraft nose body, aircraft nose body facial make-up is equipped with the wind vane, and the bottom of aircraft nose body installs on the mount pad, the first bull stick of bottom fixedly connected with of mount pad, and fixed mounting has a conical gear on the first bull stick, the bottom activity of a conical gear is inserted and is established on the mount, and mount fixed mounting is in adjustment mechanism's inside, adjustment mechanism facial make-up is equipped with the axostylus axostyle seat, and the activity is inserted and is equipped with the second bull stick on the axostylus axostyle seat. The utility model discloses a driving motor's function makes the mount pad rotate to be convenient for adjust the position to the aircraft nose body, be convenient for fix the position of aircraft nose body through electric telescopic handle's extension.

Description

Aerogenerator aircraft nose positioner

Technical Field

The utility model belongs to the technical field of aerogenerator, more specifically says, in particular to aerogenerator aircraft nose positioner.

Background

The wind driven generator is a device for converting wind energy into electric energy, mainly comprises blades, a generator, mechanical parts and electrical parts, and is mainly divided into a horizontal axis wind driven generator and a vertical axis wind driven generator according to different rotating shafts, and the horizontal axis wind driven generator occupies the mainstream position in the market at present.

Based on the above, the present inventors found that the following problems exist: the existing wind power generation motor blows blades to rotate through wind power and then converts the wind energy into electric energy, a wind direction control device is generally adopted to adjust the machine head body, and the machine head frequently shakes due to the fact that the natural wind direction is changeable, abrasion is caused, and the service life is shortened.

Therefore, in view of the above, research and improvement are made for the existing structure and defects, and a positioning device for a head of a wind turbine generator is provided, so as to achieve the purpose of higher practical value.

SUMMERY OF THE UTILITY MODEL

In order to solve the technical problem, the utility model provides a aerogenerator aircraft nose positioner to solve now because natural wind direction is changeable, can lead to the aircraft nose to shake frequently, cause the problem of wearing and tearing.

The utility model relates to a purpose and efficiency of aerogenerator aircraft nose positioner reach by following specific technological means:

a wind driven generator head positioning device comprises a head body, wherein a wind vane is arranged on the head body, the bottom end of the head body is arranged on an installation seat, a first rotating rod is fixedly connected to the bottom end of the installation seat, a first bevel gear is fixedly arranged on the first rotating rod, the bottom end of the first bevel gear is movably inserted on a fixing frame, the fixing frame is fixedly arranged inside an adjusting mechanism, a shaft rod seat is arranged on the adjusting mechanism, a second rotating rod is movably inserted on the shaft rod seat, a second bevel gear is fixedly arranged at one end of the second rotating rod, a base is arranged at the bottom end of the installation seat, a shaft seat is arranged inside the base, a fixing plate is fixedly arranged on the shaft seat, electric telescopic rods are arranged at two ends of the fixing plate, an inserting rod is arranged at the other end of the electric telescopic rod, and the inserting rod is movably inserted in a sleeve, the limiting block has been installed to the inside of base, and the cover is equipped with the snap ring on the limiting block, the snap ring is installed in the roating seat, and roating seat fixed mounting inside the base, the movable sleeve is equipped with the ring on the roating seat, and ring fixed mounting is in the bottom of mount pad.

Furthermore, a groove is formed in the fixing frame, and the bottom end of the first rotating rod is inserted into the groove.

Furthermore, the fixing frame is provided with a driving motor, and the output end of the driving motor is in transmission connection with the other end of the second rotating rod.

Furthermore, the second bevel gear is meshed with the first bevel gear, and the second bevel gear and the first bevel gear form a rotating structure.

Furthermore, the top end of the limiting block is attached to the inner wall of the circular ring.

Furthermore, a plurality of groups of grooves are arranged on the inner side of the circular ring, and the caliber size of each groove is larger than the diameter size of the corresponding plug rod.

Compared with the prior art, the utility model discloses following beneficial effect has:

1. the wind driven generator head positioning device is used by matching the mounting seat with the adjusting mechanism, when the position of a head body on the mounting seat needs to be adjusted, the second rotating rod is rotated through the operation of the driving motor, the first rotating rod is driven to rotate through the rotation of the second rotating rod through the second bevel gear, and the head body on the mounting seat is effectively adjusted in position to generate electricity;

2. according to the wind driven generator head positioning device, the mounting seat is matched with the base for use, when the mounting seat rotates and the direction is adjusted, the electric telescopic rods on the two sides of the fixing plate start to extend, and the insertion rods are inserted into the grooves in the inner wall of the circular ring through the extension of the electric telescopic rods, so that the position of the mounting seat is convenient to fix; the utility model has the advantages of simple and reasonable structure, the modern design, easy operation is convenient, can effectively fix the angle after the aircraft nose body is rotatory, has higher practical value.

Drawings

Fig. 1 is a perspective view of the present invention.

Fig. 2 is a sectional structure view of the mounting base of the present invention.

Fig. 3 is a cross-sectional view of the base of the present invention.

Fig. 4 is an enlarged schematic view of the structure a in fig. 3 according to the present invention.

In the drawings, the corresponding relationship between the component names and the reference numbers is as follows:

1. a handpiece body; 101. a wind vane; 102. a mounting seat; 103. a first rotating lever; 104. a first bevel gear; 105. a fixed mount; 106. an adjustment mechanism; 107. a spindle base; 108. a second rotating rod; 109. a second bevel gear; 110. a drive motor; 2. a base; 201. a shaft seat; 202. a fixing plate; 203. an electric telescopic rod; 204. inserting a rod; 205. a sleeve; 206. a limiting block; 207. a snap ring; 208. a rotating base; 209. a circular ring.

Detailed Description

The following describes embodiments of the present invention in further detail with reference to the accompanying drawings and examples. The following examples are intended to illustrate the invention, but are not intended to limit the scope of the invention.

In the description of the present invention, "a plurality" means two or more unless otherwise specified; the terms "upper", "lower", "left", "right", "inner", "outer", "front", "rear", "head", "tail", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are merely for convenience of description and simplicity of description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first," "second," "third," and the like are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.

In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "connected" and "connected" are to be interpreted broadly, and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; may be directly connected or indirectly connected through an intermediate. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.

Example (b):

as shown in figures 1 to 4:

the utility model provides a wind driven generator aircraft nose positioner, including aircraft nose body 1, aircraft nose body 1 facial make-up is equipped with wind vane 101, and the bottom of aircraft nose body 1 is installed on mount pad 102, the bottom of mount pad 102 is fixedly connected with first bull stick 103, and fixedly install first bevel gear 104 on first bull stick 103, the bottom activity of first bevel gear 104 is inserted and is established on mount 105, and mount 105 is fixedly installed in the inside of adjustment mechanism 106, adjustment mechanism 106 facial make-up is equipped with shaft rod seat 107, and movably insert and be equipped with second bull stick 108 on shaft rod seat 107, the one end fixed mounting of second bull stick 108 has second bevel gear 109, the bottom of mount pad 102 is provided with base 2, and the inside of base 2 is equipped with axle bed 201, fixed mounting has fixed plate 202 on the axle bed 201, and the both ends of fixed plate 202 are equipped with electric telescopic handle 203, inserted bar 204 is installed to the other end of electric telescopic handle 203, the inserting rod 204 is movably inserted into the sleeve 205, the limiting block 206 is arranged inside the base 2, the limiting block 206 is sleeved with a clamping ring 207, the clamping ring 207 is arranged in the rotating seat 208, the rotating seat 208 is fixedly arranged inside the base 2, the rotating seat 208 is movably sleeved with a ring 209, and the ring 209 is fixedly arranged at the bottom end of the mounting seat 102.

Wherein, the inside recess that is provided with of mount 105, and the bottom of first bull stick 103 is inserted and is established in the recess, and the bottom of the mount 105 of being convenient for rotates in the recess of first bull stick 103.

The fixing frame 105 is provided with a driving motor 110, an output end of the driving motor 110 is in transmission connection with the other end of the second rotating rod 108, and the second rotating rod 108 rotates through the operation of the driving motor 110.

The second bevel gear 109 is engaged with the first bevel gear 104, the second bevel gear 109 and the first bevel gear 104 form a rotating structure, the second bevel gear 109 is fixedly mounted at one end of the second rotating rod 108, the second rotating rod 108 is rotated through the operation of the driving motor 110, and the rotation of the second rotating rod 108 drives the first rotating rod 103 to rotate through the second bevel gear 109.

Wherein, the top of stopper 206 laminates on the inner wall of ring 209, is convenient for support the whole of ring 209.

Wherein, be provided with a plurality of groups of recesses on the inboard of ring 209, and the bore size of recess is greater than the diameter size of inserted bar 204, is convenient for inserted bar 204 to pass through electric telescopic handle 203 and inserts in the recess of ring 209 through the promotion of electric telescopic handle 203.

The specific use mode and function of the embodiment are as follows:

when the product is used, firstly, whether the connection part of the product is fastened or not is detected, the handpiece body 1 needs to be rotated and adjusted to the downwind position after the product is ensured to be intact, the driving motor 110 is fixedly arranged in the adjusting mechanism 106, and the output end of the driving motor 110 is connected with a second rotating rod 108 in a transmission way, and the other end of the second rotating rod 108 is fixedly provided with a second bevel gear 109, the second rotating rod 108 is rotated by the operation of the driving motor 110, the rotation of the second rotating rod 108 drives the first rotating rod 103 to rotate through the second bevel gear 109, thereby facilitating the rotation and direction adjustment of the handpiece body 1 on the mounting seat 102, when the handpiece body 1 is adjusted, the electric telescopic rod 203 begins to extend, the extension of the electric telescopic rod 203 moves the insertion rod 204, and the movement of the insertion rod 204 is conveniently clamped in the groove of the circular ring 209 to fix the rotating position of the mounting seat 102.

The embodiments of the present invention have been presented for purposes of illustration and description, and are not intended to be exhaustive or limited to the invention in the form disclosed. Many modifications and variations will be apparent to those of ordinary skill in the art. The embodiment was chosen and described in order to best explain the principles of the invention and the practical application, and to enable others of ordinary skill in the art to understand the invention for various embodiments with various modifications as are suited to the particular use contemplated.

Claims

1. The utility model provides a aerogenerator aircraft nose positioner, includes aircraft nose body (1), its characterized in that: the wind vane (101) is arranged on the handpiece body (1), the bottom end of the handpiece body (1) is arranged on the mounting seat (102), the bottom end of the mounting seat (102) is fixedly connected with a first rotating rod (103), a first bevel gear (104) is fixedly arranged on the first rotating rod (103), the bottom end of the first bevel gear (104) is movably inserted on a fixing frame (105), the fixing frame (105) is fixedly arranged in an adjusting mechanism (106), a shaft rod seat (107) is arranged on the adjusting mechanism (106), a second rotating rod (108) is movably inserted on the shaft rod seat (107), a second bevel gear (109) is fixedly arranged at one end of the second rotating rod (108), a base (2) is arranged at the bottom end of the mounting seat (102), a base (201) is arranged in the base (2), a fixing plate (202) is fixedly arranged on the shaft seat (201), and the both ends of fixed plate (202) all are equipped with electric telescopic handle (203), inserted bar (204) are installed to the other end of electric telescopic handle (203), and inserted bar (204) activity is inserted and is established in sleeve (205), stopper (206) have been installed to the inside of base (2), and the cover is equipped with snap ring (207) on stopper (206), snap ring (207) are installed in roating seat (208), and roating seat (208) fixed mounting inside base (2), the movable sleeve is equipped with ring (209) on roating seat (208), and ring (209) fixed mounting is in the bottom of mount pad (102).

2. The wind turbine head positioning device according to claim 1, wherein: the fixing frame (105) is internally provided with a groove, and the bottom end of the first rotating rod (103) is inserted into the groove.

3. The wind turbine head positioning device according to claim 1, wherein: the fixing frame (105) is provided with a driving motor (110), and the output end of the driving motor (110) is in transmission connection with the other end of the second rotating rod (108).

4. The wind turbine head positioning device according to claim 1, wherein: the second bevel gear (109) is meshed with the first bevel gear (104), and the second bevel gear (109) and the first bevel gear (104) form a rotary structure.

5. The wind turbine head positioning device according to claim 1, wherein: the top end of the limiting block (206) is attached to the inner wall of the circular ring (209).

6. The wind turbine head positioning device of claim 1, wherein: a plurality of groups of grooves are arranged on the inner side of the circular ring (209), and the caliber size of each groove is larger than the diameter size of the corresponding inserted rod (204).