CN214118801U - Novel autorotation rotorcraft prewhirl clutch device - Google Patents
Novel autorotation rotorcraft prewhirl clutch device Download PDFInfo
- Publication number
- CN214118801U CN214118801U CN202023251853.2U CN202023251853U CN214118801U CN 214118801 U CN214118801 U CN 214118801U CN 202023251853 U CN202023251853 U CN 202023251853U CN 214118801 U CN214118801 U CN 214118801U
- Authority
- CN
- China
- Prior art keywords
- prewhirl
- inner shaft
- gear
- gear ring
- outer gear
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Images
Abstract
The utility model provides a novel rotation gyroplane prewhirl wheeling unit is put, include the interior axle that links to each other with rotor hub device control cantilever through bearing structure, interior hub connection has the flexible axle, and interior epaxial ring gear that opens has, and the internal ring circles through skewed tooth and outer ring gear meshing, and the skewed tooth of interior axle is reciprocated along the external gear under centrifugal force, moves with rotor hub device gear wheel meshing when the highest point when the external gear. The utility model discloses having removed little jar of prewhirl and gas circuit controlling means on the basis of realizing original clutch function of prewhirl, having adopted inertia to get rid of the mode of tooth and realized this function, reduced the complexity and the structure weight of prewhirl system, improved its security and reliability.
Description
Technical Field
The utility model relates to the technical field of aviation, specifically a novel rotation gyroplane pre-rotation clutch device.
Background
The autorotation gyroplane (called gyroplane for short) is a gyroplane taking an autorotation rotor as a lifting surface, propeller pushing/pulling force or other energy supply modes as advancing power, and has the characteristics of simple mechanism, high safety, low cost and the like, and the rotor of the gyroplane realizes autorotation by depending on the forward incoming flow driving during flight to provide lift force. And adopt the rotor to revolve technique in advance, drive the rotor in advance through transmission before taking off, then take off after cutting off the transmission link through the clutch, can make the gyroplane can the ray formula jump or ultrashort apart from taking off.
The existing prerotation mechanism adopts a prerotation small cylinder and a gas circuit control device, and has the disadvantages of complex system, heavy structure weight, and low safety and reliability.
SUMMERY OF THE UTILITY MODEL
The utility model discloses a solve prior art's problem, provide a novel rotation gyroplane is clutch device in advance, removed little jar and gas circuit controlling means in advance on the basis of realizing original clutch function in advance, adopt inertia to get rid of the mode of tooth and realize this function, reduced the complexity and the structure weight of system in advance, improved its security and reliability.
The utility model discloses an interior axle that links to each other with rotor hub device manipulation cantilever through bearing structure, interior hub connection has the flexible axle, and it has the ring gear to open on the interior axle, and the internal ring circles through skewed tooth and outer ring gear meshing, and the external gear reciprocates along the skewed tooth of interior axle under the centrifugal force effect, moves with rotor hub device gear wheel meshing when the highest point when the external gear.
The improvement is further that during prerotation, the flexible shaft transmits power to the inner shaft to drive the inner shaft to rotate, the outer gear ring has a rotation speed difference with the inner gear ring under the inertia effect, and moves upwards along the helical teeth to be meshed with the large gear; when the pre-rotation is disconnected, the rotating speed of the outer gear ring is reduced to be lower than that of the large gear, the outer gear ring moves downwards along the helical gear and is separated from the large gear, and the pre-rotation clutch function is realized.
The bearing structure comprises an upper bearing, an upper bearing seat, a lower bearing and a lower bearing seat, wherein the upper part of the inner shaft is fixed with the operating cantilever through the upper bearing and the upper bearing seat, and the lower part of the inner shaft is fixed with the operating cantilever through the lower bearing and the lower bearing seat.
The utility model has the advantages that: the pre-rotation clutch has the advantages that the pre-rotation small cylinder and the gas circuit control device are removed on the basis of realizing the function of the original pre-rotation clutch, the function is realized by adopting an inertia tooth throwing mode, the complexity and the structural weight of the pre-rotation system are reduced, and the safety and the reliability of the pre-rotation system are improved.
Drawings
FIG. 1 is a perspective view of a pre-rotation clutch assembly;
FIG. 2 is a perspective view of an inner shaft of the pre-rotation clutch assembly;
FIG. 3 is a schematic view of the installation of a big fluted disc, a pre-rotation clutch device and a flexible shaft;
in the figure, an inner shaft 1, an outer gear ring 2, an upper bearing 3, an upper bearing seat 4, a lower bearing 5, a lower bearing seat 6, a large toothed disc 7, a large gear 8 and a flexible shaft 9.
Detailed Description
The present invention will be further explained with reference to the accompanying drawings.
The utility model discloses the structure is as shown in fig. 3, include the interior axle that links to each other with rotor hub device manipulation cantilever through bearing structure, interior axle construction is shown in fig. 1 and 2, and interior hub connection has the flexible axle, and interior epaxial ring gear that opens has, and the internal ring circles through skewed tooth and outer ring gear meshing, and the skewed tooth of outer gear edge interior axle reciprocates under the centrifugal force effect, moves with rotor hub device gear wheel meshing when the highest point when the outer gear.
The improvement is further that during prerotation, the flexible shaft transmits power to the inner shaft to drive the inner shaft to rotate, the outer gear ring has a rotation speed difference with the inner gear ring under the inertia effect, and moves upwards along the helical teeth to be meshed with the large gear; when the pre-rotation is disconnected, the rotating speed of the outer gear ring is reduced to be lower than that of the large gear, the outer gear ring moves downwards along the helical gear and is separated from the large gear, and the pre-rotation clutch function is realized.
The bearing structure comprises an upper bearing, an upper bearing seat, a lower bearing and a lower bearing seat, wherein the upper part of the inner shaft is fixed with the operating cantilever through the upper bearing and the upper bearing seat, and the lower part of the inner shaft is fixed with the operating cantilever through the lower bearing and the lower bearing seat.
The utility model discloses the concrete application way is many, and the above-mentioned only is the preferred embodiment of the utility model, should point out, to ordinary skilled person in this technical field, under the prerequisite that does not deviate from the utility model discloses the principle, can also make a plurality of improvements, and these improvements also should be regarded as the utility model discloses a protection scope.
Claims (3)
1. The utility model provides a novel rotation gyroplane is wheeling clutch device soon which characterized in that: the inner shaft is connected with a flexible shaft, an inner gear ring is arranged on the inner shaft, the inner gear ring is meshed with an outer gear ring through helical teeth, an outer gear moves up and down along the helical teeth of the inner shaft under the action of centrifugal force, and when the outer gear moves to the highest position, the outer gear is meshed with a large gear of the rotor hub device.
2. The novel autogiration clutch assembly of claim 1, wherein: when in prerotation, the flexible shaft transmits power to the inner shaft to drive the inner shaft to rotate, the outer gear ring has a rotation speed difference with the inner gear ring under the inertia effect, and moves upwards along the helical teeth to be meshed with the large gear; when the pre-rotation is disconnected, the rotating speed of the outer gear ring is reduced to be lower than that of the large gear, and the outer gear ring moves downwards along the helical teeth to be disconnected with the large gear.
3. The novel autogiration clutch assembly of claim 1, wherein: the bearing structure comprises an upper bearing, an upper bearing seat, a lower bearing and a lower bearing seat, wherein the upper part of the inner shaft is fixed with the control cantilever through the upper bearing and the upper bearing seat, and the lower part of the inner shaft is fixed with the control cantilever through the lower bearing and the lower bearing seat.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202023251853.2U CN214118801U (en) | 2020-12-29 | 2020-12-29 | Novel autorotation rotorcraft prewhirl clutch device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202023251853.2U CN214118801U (en) | 2020-12-29 | 2020-12-29 | Novel autorotation rotorcraft prewhirl clutch device |
Publications (1)
Publication Number | Publication Date |
---|---|
CN214118801U true CN214118801U (en) | 2021-09-03 |
Family
ID=77485747
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202023251853.2U Active CN214118801U (en) | 2020-12-29 | 2020-12-29 | Novel autorotation rotorcraft prewhirl clutch device |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN214118801U (en) |
-
2020
- 2020-12-29 CN CN202023251853.2U patent/CN214118801U/en active Active
Similar Documents
Publication | Publication Date | Title |
---|---|---|
JP4742390B2 (en) | Electric motor built-in hub for rotary wing aircraft, and rotary wing aircraft using the same | |
CN112805218A (en) | Machine comprising a hybrid powertrain and corresponding control method | |
CN100431921C (en) | Synchronous switching adjusting device of coaxial double-oared self-spinning wing aircraft | |
CN107235155A (en) | A kind of transmission device for high speed multirotor helicopter | |
CN104960664A (en) | Composite jump takeoff system for heavy gyroplane with jump takeoff capability | |
CN214118801U (en) | Novel autorotation rotorcraft prewhirl clutch device | |
CN201240501Y (en) | Speed reducing driver for helicopter rotor | |
RU2525353C1 (en) | Rotorcraft adjustable transmission | |
CN2920826Y (en) | Synchronous changing-over regulator for coaxle double-paddle self-rotor aerobat | |
CN110356546B (en) | Electric control variable-pitch single-rotor tailless-propeller electric unmanned helicopter | |
KR101654799B1 (en) | drone | |
JP5027631B2 (en) | Fixed-pitch coaxial double inversion helicopter | |
CN206485568U (en) | A kind of many rotor unmanned aircrafts | |
CN108408060A (en) | A kind of unmanned plane oil electric mixed dynamic coupled system | |
CN206900651U (en) | A kind of transmission device for high speed multirotor helicopter | |
CN102673785A (en) | Flapping-wing aircraft | |
KR20070001117U (en) | Taking off and landing airplane using variable rotary wings | |
CN206871352U (en) | Hybrid power unmanned plane with small rotor | |
CN115402505A (en) | Diameter-variable rotor wing device adopting connecting rod driving mechanism | |
CN210240458U (en) | Coaxial planetary gear reducer | |
CN211001870U (en) | Multi-rotor unmanned aerial vehicle timely speed regulation internal tooth planetary gear train mechanism | |
CN108995793B (en) | Rotor wing pitch-changing system | |
CN208035876U (en) | A kind of land and air double-used aircraft | |
CN214112864U (en) | Rotor pre-rotation operating device of autorotation rotorcraft | |
CN216154023U (en) | Rotorcraft capable of vertically taking off and landing |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
GR01 | Patent grant | ||
GR01 | Patent grant |