CN206900657U - Gyroplane auto-leveling mechanism - Google Patents
Gyroplane auto-leveling mechanism Download PDFInfo
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- CN206900657U CN206900657U CN201720543542.2U CN201720543542U CN206900657U CN 206900657 U CN206900657 U CN 206900657U CN 201720543542 U CN201720543542 U CN 201720543542U CN 206900657 U CN206900657 U CN 206900657U
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- leveling
- gyroplane
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- rotor
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Abstract
The utility model provides a kind of gyroplane auto-leveling mechanism, is related to technical field of aerospace, and solving in the prior art can not be by adjusting rotor and whole gyroplane is in the technical problem of stable state.The device includes leveling components, the transmission device and connector of rotor, wherein：Leveling components are connected with the transmission device of rotor and one end of connector respectively, the other end of connector is connected with control stick, connected between leveling components and connector for attachment force adjustable, control stick can drive adjustment part by connector and change position of the rotor relative to fuselage by adjusting the transmission device of part drive rotor.The utility model is by adjusting levelling gear so that gyroplane is in balanced steady state, facilitates driver to drive gyroplane, also improves the security that driver drives gyroplane.
Description
Technical field
Technical field of aerospace is the utility model is related to, more particularly, to a kind of gyroplane auto-leveling mechanism.
Background technology
Rotor is the prevailing lift part of the rotary wing aircrafts such as helicopter and gyroplane.Rotor is by propeller hub and several pieces blade structures
Into.Propeller hub is arranged in rotor shaft, and the blade shaped like slender wing is then connected on propeller hub.The effect of rotor：Lift is produced, to
The component of part in vertical direction such as the gravity and fuselage of balancing helicopter, horizontal tail, wing；Produce level point forward
Power：Air drag is overcome helicopter is advanced；In hovering, lateral or horizontal component backward is produced, helicopter is carried out side and flies
It is or rear winged；Produce component and helicopter is controlled torque or maneuvering flight, similar to the various control surfaces on aircraft.
The rotor of gyroplane and the angle of fuselage are not fixed, can be adjusted within the specific limits, in rotor master
There are some thinner connecting rods around axle, the main purpose of these bars is exactly to draw main rotor to change angle, and pilot can lead to
Cross control stick control and change pitch, that is, change the angle between main rotor and fuselage realize the pitching of aircraft, rolling and on
Rise and decline.
Existing gyroplane is directly to be connected by control stick by connector with the transmission device of rotor, changes rotor and machine
The angle of body.
Applicants have discovered that at least there is following technical problem in prior art：
The function of rotor is single, and gyroplane can not be by adjusting rotor and shape of the whole gyroplane in stabilization at present
State.
Utility model content
The purpose of this utility model is to provide gyroplane auto-leveling mechanism, can not led to solving presence in the prior art
Overregulate rotor and cause whole gyroplane to be in the technical problem of stable state.Many technical schemes provided by the utility model
In many technique effects elaboration as detailed below that can be generated of optimal technical scheme.
To achieve the above object, the utility model provides following technical scheme：
A kind of gyroplane auto-leveling mechanism provided by the utility model, including the transmission device of leveling components, rotor and
Connector, wherein：The leveling components are connected with the transmission device of the rotor and one end of the connector respectively, described
The other end of connector is connected with control stick, is connected between the leveling components and the connector for attachment force adjustable,
Control stick can drive the leveling components by the connector and drive the transmission of the rotor to fill by the leveling components
Put to change position of the rotor relative to fuselage.
Preferably, the levelling gear includes leveling board, elastic component and leveling connector, and one end of the elastic component passes through
The leveling connector is connected with the leveling board, and the other end of the elastic component is connected with the connector, and the elasticity
Part is in the state of stretching.
Preferably, the elastic component is spring, and one end of the elastic component is detachably connected with the connector, the other end
Removably it is connected with the leveling connector.
Preferably, the leveling connector includes annulus bolt and the nut being engaged with the annulus bolt, the circle
Collar bolt is fixed on the leveling board by the nut, and one end of the elastic component and the annulus of the annulus bolt connect
Connect.
Preferably, connecting hole and adjustment hole are offered on the leveling board, the transmission of the connecting hole and the rotor fills
Put and be engaged, the adjustment hole is engaged with the annulus bolt.
Preferably, the adjustment hole is opened on the leveling board away from the connecting hole side, and the adjustment hole
It is evenly distributed in the form of yi word pattern on the leveling board.
Preferably, the number scope of the adjustment hole is 6~15.
Preferably, length direction of the leveling board along the leveling board has certain radian.
Preferably, one end of the connector is provided with connection ring, and one end of the elastic component is connected with the connection ring.
Preferably, the transmission device of the leveling components and the rotor is detachably connected.
Gyroplane auto-leveling mechanism provided by the utility model, solve that by adjusting rotor whole gyroplane can not be made
Technical problem in stable state, driver when driving gyroplane and feeling that gyroplane is in uneven, unsure state,
By adjusting auto-leveling mechanism, gyroplane is in balanced steady state, facilitate driver to drive gyroplane, also improve and drive
The person of sailing drives the security of gyroplane.
Brief description of the drawings
, below will be to embodiment in order to illustrate more clearly of the utility model embodiment or technical scheme of the prior art
Or the required accompanying drawing used is briefly described in description of the prior art, it should be apparent that, drawings in the following description are only
It is some embodiments of the utility model, for those of ordinary skill in the art, is not paying the premise of creative work
Under, other accompanying drawings can also be obtained according to these accompanying drawings.
Fig. 1 is the structural representation of the leveling board of wing machine auto-leveling mechanism；
Fig. 2 is the structural representation of wing machine auto-leveling mechanism.
1- connectors in figure；2- leveling boards；21- connecting holes；22- adjustment holes；3- elastic components；4- annulus bolts；5- nuts；
The transmission device of 6- rotors.
Embodiment
, below will be to technology of the present utility model to make the purpose of this utility model, technical scheme and advantage clearer
Scheme is described in detail.Obviously, described embodiment is only the utility model part of the embodiment, rather than all
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not before creative work is made
Resulting all other embodiment is put, belongs to the scope that the utility model is protected.
The utility model provides a kind of gyroplane auto-leveling mechanism, includes the and of transmission device 6 of leveling components, rotor
Connector 1, wherein：Leveling components are connected with the transmission device 6 of rotor and one end of connector 1 respectively, connector 1 it is another
End is connected with control stick, is connected between leveling components and connector 1 for attachment force adjustable, and control stick passes through the energy of connector 1
Drive leveling components and drive the transmission device 6 of rotor by leveling components to change position of the rotor relative to fuselage, rotor
Transmission device 5 be the structure that is connected with rotor.The utility model solves to make whole gyroplane be in stable by adjusting rotor
The technical problem of state so that gyroplane is in balanced steady state, facilitates driver to drive gyroplane, improves driver and drive
Sail the security of gyroplane.
Optionally embodiment, levelling gear include leveling board 2, elastic component 3 and leveling connector, elastic component 3
One end is connected by leveling connector with leveling board 2, and the other end of elastic component 3 is connected with connector 1, and elastic component 3 is in and drawn
The state stretched, on leveling board 2, leveling board 2 is connected the pulling force effect of elastic component 3 with the transmission device 6 of rotor, will act at tune
Power on flat board 2 passes to the transmission device 6 of rotor, changes the position between elastic component 3 and leveling board 2, changes elastic component 3 and makees
With the active force on leveling board 2, and then change the active force on the transmission device 6 for acting on rotor so that the biography of rotor
Relative to fuselage change in location occurs for dynamic device 6, and the transmission device 6 of rotor is connected with rotor so that rotor is relative to fuselage
Position is adjusted.
Optionally embodiment, elastic component 3 can be spring, and one end and the connector 1 of elastic component 3 detachably connect
Connect, the other end and leveling connector removably connect, and now spring be in stretching state.
Optionally embodiment, leveling connector include annulus bolt 4 and the nut 5 being engaged with annulus bolt 4,
Annulus bolt 4 is fixed on leveling board 2 by nut 5, and one end of elastic component 3 is connected with the annulus of annulus bolt 4.Elastic component 3
Elastic force is acted on the annulus of annulus bolt 4, by the extruding force of screw nut 5 and leveling board 2, annulus bolt 4 fixed
On leveling board 2.
Optionally embodiment, connecting hole 21 and adjustment hole 22, connecting hole 21 and rotor are offered on leveling board 2
Transmission device 6 be engaged, adjustment hole 22 is engaged with annulus bolt 4.Pass through leveling connector and the different phases of adjustment hole 22
Coordinate, change the position of elastic component 3 and leveling board 2, that is, change the active force between elastic component 3 and leveling board 2.
Optionally embodiment, adjustment hole 22 is opened on the leveling board 2 away from the side of connecting hole 21, and adjustment hole
22 are evenly distributed in the form of yi word pattern on leveling board 2.
Optionally embodiment, the number scope of adjustment hole 22 is 6~15, the number energy of the adjustment hole 22
Enough realize adjustment of the rotor relative to fuselage.
Optionally embodiment, length direction of the leveling board 2 along leveling board 2 have certain radian.
Optionally embodiment, one end of connector 1 are provided with connection ring, and one end and the connection ring of elastic component 3 connect
Connect.
The transmission device 6 of optionally embodiment, leveling components and rotor is detachably connected.
Gyroplane auto-leveling mechanism provided by the utility model, by adjusting auto-leveling mechanism so that at gyroplane
In balanced steady state, facilitate driver to drive gyroplane, also improve the security that driver drives gyroplane.
It is described above, only specific embodiment of the present utility model, but the scope of protection of the utility model is not limited to
In this, any one skilled in the art can readily occur in change in the technical scope that the utility model discloses
Or replace, it should all cover within the scope of protection of the utility model.Therefore, the scope of protection of the utility model should be with the power
The protection domain that profit requires is defined.
Claims (10)
1. a kind of gyroplane auto-leveling mechanism, it is characterised in that including leveling components, the transmission device (6) of rotor and connection
Part (1), wherein：The leveling components connect with the transmission device (6) of the rotor and one end of the connector (1) respectively
Connect, the other end of the connector (1) is connected with control stick, is attachment force between the leveling components and the connector (1)
Adjustable connects, and control stick can drive the leveling components by the connector (1) and be driven by the leveling components
The transmission device (6) of the rotor is to change position of the rotor relative to fuselage.
2. gyroplane auto-leveling mechanism according to claim 1, it is characterised in that the levelling gear includes leveling board
(2), elastic component (3) and leveling connector, one end of the elastic component (3) pass through the leveling connector and the leveling board
(2) connect, the other end of the elastic component (3) is connected with the connector (1), and the elastic component (3) is in the shape of stretching
State.
3. gyroplane auto-leveling mechanism according to claim 2, it is characterised in that the elastic component (3) is spring, institute
State one end of elastic component (3) and the connector (1) is detachably connected, the other end removably connects with the leveling connector
Connect.
4. gyroplane auto-leveling mechanism according to claim 3, it is characterised in that the leveling connector includes annulus
Bolt (4) and the nut (5) being engaged with the annulus bolt (4), the annulus bolt (4) are fixed by the nut (5)
On the leveling board (2), one end of the elastic component (3) is connected with the annulus of the annulus bolt (4).
5. gyroplane auto-leveling mechanism according to claim 4, it is characterised in that offered on the leveling board (2)
Connecting hole (21) and adjustment hole (22), the connecting hole (21) are engaged with the transmission device (6) of the rotor, the adjustment hole
(22) it is engaged with the annulus bolt (4).
6. gyroplane auto-leveling mechanism according to claim 5, it is characterised in that the adjustment hole (22) is opened in far
On the leveling board (2) from the connecting hole (21) side, and the adjustment hole (22) is uniformly distributed in the form of yi word pattern
On the leveling board (2).
7. gyroplane auto-leveling mechanism according to claim 5, it is characterised in that the number model of the adjustment hole (22)
Enclose for 6~15.
8. gyroplane auto-leveling mechanism according to claim 4, it is characterised in that the leveling board (2) is along the tune
The length direction of flat board (2) has certain radian.
9. gyroplane auto-leveling mechanism according to claim 2, it is characterised in that one end of the connector (1) is set
Connection ring is equipped with, one end of the elastic component (3) is connected with the connection ring.
10. gyroplane auto-leveling mechanism according to claim 1, it is characterised in that the leveling components and the rotation
The transmission device (6) of the wing is detachably connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720543542.2U CN206900657U (en) | 2017-05-15 | 2017-05-15 | Gyroplane auto-leveling mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720543542.2U CN206900657U (en) | 2017-05-15 | 2017-05-15 | Gyroplane auto-leveling mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206900657U true CN206900657U (en) | 2018-01-19 |
Family
ID=61289096
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720543542.2U Active CN206900657U (en) | 2017-05-15 | 2017-05-15 | Gyroplane auto-leveling mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206900657U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109131838A (en) * | 2018-09-21 | 2019-01-04 | 湖南湘晨飞机工业有限公司 | A kind of rotorcraft rotor disk trimmer |
| CN109131852A (en) * | 2018-09-21 | 2019-01-04 | 湖南湘晨飞机工业有限公司 | A kind of rotorcraft rotor disk manipulation position-limit mechanism |
-
2017
- 2017-05-15 CN CN201720543542.2U patent/CN206900657U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109131838A (en) * | 2018-09-21 | 2019-01-04 | 湖南湘晨飞机工业有限公司 | A kind of rotorcraft rotor disk trimmer |
| CN109131852A (en) * | 2018-09-21 | 2019-01-04 | 湖南湘晨飞机工业有限公司 | A kind of rotorcraft rotor disk manipulation position-limit mechanism |
| CN109131852B (en) * | 2018-09-21 | 2024-03-12 | 湖南湘晨飞机工业有限公司 | Rotary wing disk control limiting mechanism of rotary wing aircraft |
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