CN206813298U - Rudder angle position governor motion and aircraft - Google Patents
Rudder angle position governor motion and aircraft Download PDFInfo
- Publication number
- CN206813298U CN206813298U CN201720409553.1U CN201720409553U CN206813298U CN 206813298 U CN206813298 U CN 206813298U CN 201720409553 U CN201720409553 U CN 201720409553U CN 206813298 U CN206813298 U CN 206813298U
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- rudder
- connecting seat
- pedal
- seat
- fixed seat
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Abstract
The utility model provides a kind of rudder angle position governor motion and aircraft, is related to technical field of aerospace, solves the problems, such as that prior art has some pilots because height is inconvenient to step on the technical problem of rudder pedals.Direction rudder angles position adjusting mechanism includes rudder pedals, pedal position adjustment structure and transmission mechanism, wherein：Pedal position adjustment structure is connected between rudder pedals and transmission mechanism, transmission mechanism is connected with rudder, rudder pedals are trampled, structure drive transmission device can be adjusted by pedal position during movement and changes angle and/or the position of rudder by transmission mechanism, and the distance between rudder pedals and seat can be changed by adjusting structure by pedal position.The utility model make it that rudder pedals are adjustable apart from the position of seat, is adapted to the pilot of different heights.
Description
Technical field
Technical field of aerospace is the utility model is related to, more particularly, to a kind of rudder angle position governor motion and flight
Device.
Background technology
Rudder is steerable airfoil portion in vertical tail, and it is to carry out yaw control to aircraft that it, which is acted on, for repairing
Positive vector and low-angle turn to.The manipulation principle of rudder is similar with elevator, when aircraft needs left-hand rotation flight, drives
Member will manipulate rudder and deflect to the left, and now the aerodynamic force suffered by rudder, which will produce one, makes what Nose Left deflected
Torque, the course of aircraft also change therewith.Equally, if pilot control rudder deflects to the right, the head of aircraft will be
Turned right in the presence of aerodynamic moment.
Rudder pedals, can control the rudder on vertical tail, and effect is when there is crosswind or has a hair on one side
Low-angle amendment vector during motivation failure, wide-angle, which is turned, just needs rotation control stick to be realized by craft inclination.
Existing rudder angle position governor motion, including rudder pedals and transmission mechanism, wherein：Transmission mechanism
Be connected between rudder pedals and rudder, rudder pedals are trampled, it is mobile during can drive transmission device and by
Transmission mechanism changes angle and/or the position of rudder.
Applicants have discovered that at least there is following technical problem in prior art：
Rudder pedals need to step on realization with pin to be operated to it, but because everyone height is different, and existing side
Into rudder angles position adjusting mechanism, the distance between rudder pedals and seat can not be adjusted, and rudder pedals are apart from seat
Position is fixed, and makes some pilots be inconvenient to step on rudder pedals, such as：The relatively low pilot of height, to step on because distance is remote
Lower rudder pedals are gruelling；The higher pilot of height, both legs are in a kind of state of heap contracting, and time length can feel fatigue.
Utility model content
The purpose of this utility model is the governor motion and aircraft for providing rudder pedals, to solve in the prior art
Some existing pilots are inconvenient to step on rudder pedals technical problem because of height problem.Many skills provided by the utility model
Optimal technical scheme in art scheme can make it that rudder pedals are adjustable apart from the position of seat, be adapted to the flight of different heights
Member so that the relatively low pilot of height also can easily step on the higher pilot of rudder pedals, height and drive an airplane
When, both legs are not at a kind of state of heap contracting, and easily sitting posture avoids driving time length from the situation of fatigue occur.
To achieve the above object, the utility model provides following technical scheme：
Rudder angle position provided by the utility model governor motion, including rudder pedals, pedal position adjustment knot
Structure and transmission mechanism, wherein：Pedal position adjustment structure be connected to the rudder pedals and the transmission mechanism it
Between, the transmission mechanism is connected with rudder, the rudder pedals are trampled, it is mobile during can be by the pedal
Position adjustment structure drives the transmission mechanism and changes angle and/or the position of rudder by the transmission mechanism, by stepping on
Board position adjustment structure can change the distance between the rudder pedals and seat.
Preferably, the pedal position adjustment structure includes pedal connecting seat, fixed seat and connected for connecting the pedal
The fixture of joint chair and the fixed seat, the pedal connecting seat are connected with the rudder pedals, the fixed seat and side
It is connected to rudder angles position adjusting mechanism, rudder angle adjusting mechanism change side can be driven in the fixed seat moving process
Angle and/or position to rudder, when changing the link position of the fixture and the pedal connecting seat, the pedal connecting seat
Changed with the relative position of the fixed seat.
Preferably, connecting seat adjustment hole has been set along the length direction of the pedal connecting seat, has been opened in the fixed seat
Provided with fixed seat adjustment hole, the fixture inserts the connecting seat adjustment hole and corresponding with the connecting seat adjustment hole described
Fixed seat adjustment hole realizes the connection of the pedal connecting seat and the fixed seat.
Preferably, the fixture is bearing pin.
Preferably, the top of the fixture is connected with the handle for facilitating the fixture rotation process.
Preferably, in addition to for locking the locking member of the fixture, one end of the locking member and the fixture
It is fitted close, the other end is fixed in the pedal connecting seat or/and the fixed seat.
Preferably, connecting seat locking hole is offered along the length direction of the pedal connecting seat, is opened up in the fixed seat
There is fixed seat locking hole, one end of the locking member passes through the connecting seat locking hole and the corresponding fixed seat locking hole.
Preferably, the connecting seat locking hole is arranged on the side of the connecting seat adjustment hole, and the connecting seat is adjusted
The distance at the center in hole to the center of two adjacent connecting seat locking holes is equal.
Preferably, the pedal connecting seat and the fixed seat are that inner hollow, cross sectional shape are rectangle, and described
Pedal connecting seat is arranged in the fixed seat, is moved along the length direction of the pedal connecting seat and is changed the pedal connecting seat
With the relative position of the fixed seat.
A kind of aircraft provided by the utility model, including the direction rudder angles that any technical scheme of the utility model provides
Position adjusting mechanism.
The utility model provides direction rudder angles position adjusting mechanism, simple in construction, realize rudder pedals and seat it
Between distance it is adjustable；Fixture top is connected with handle, is easy to the operation to fixture；Also include the lock for the part that is locked
Tight part, improves security, and rudder pedals are in the feelings that uncontrollable state triggers serious consequence when avoiding the fixed seat from coming off
Condition；The distance at the center of connecting seat adjustment hole to the center of two adjacent connecting seat locking holes is equal, realizes pedal connecting seat
The flexibility coordinated with fixed seat；The aircraft of rudder angle position governor motion is installed, avoids some pilots because of body
High problem is inconvenient to step on the situation of rudder pedals.
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 rudder angle position provided by the utility model governor motion；
Fig. 2 is the structural representation of fixed seat provided by the utility model；
Fig. 3 is the structural representation of locking member provided by the utility model.
1- rudder pedals in figure；2- pedal positions adjust structure；21- pedal connecting seats；211- connecting seat adjustment holes；
212- connecting seat locking holes；22- fixed seats；221- fixed seat adjustment holes；222- fixed seat locking holes；23- fixtures；231- handles
Hand；24- locking members.
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 rudder angle position governor motion, including rudder pedals 1, pedal position are adjusted
Whole structure 2 and transmission mechanism, wherein：Pedal position adjustment structure 2 is connected between rudder pedals 1 and transmission mechanism, is passed
Motivation structure is connected with rudder, and rudder pedals 1 are trampled, can driven during movement by pedal position adjustment structure 2
Dynamic transmission mechanism and angle and/or the position for changing rudder by transmission mechanism, adjusting structure 2 by pedal position can change side
To the distance between rudder pedal 1 and seat.The utility model solves the problems, such as that some pilots are because of height present in prior art
Be inconvenient to step on rudder pedals technical problem, rudder angle position provided by the utility model governor motion causes rudder
Pedal is adjustable apart from the position of seat, is adapted to the pilot of different heights so that the relatively low pilot of height also can be easily
The higher pilot of rudder pedals, height is stepped on when driving an airplane, both legs are not at a kind of state of heap contracting, easily
Sitting posture avoids driving time length from the situation of fatigue occur.
Optionally embodiment, referring to Fig. 1 and Fig. 2, pedal position adjustment structure 2 includes pedal connecting seat 21, consolidated
Reservation 22 and the fixture 23 for connecting pedal connecting seat 21 and fixed seat 22, pedal connecting seat 21 and the phase of rudder pedals 1
Connection, fixed seat 22 are connected with rudder angle position governor motion, and direction rudder angles can be driven in the moving process of fixed seat 2
Governor motion changes angle and/or the position of rudder, and fixture 23 can be bearing pin, along the length direction of pedal connecting seat 21
On set connecting seat adjustment hole 211, offer fixed seat adjustment hole 221 in fixed seat 22, fixture 23 inserts connecting seat and adjusted
Knothole 211 and fixed seat adjustment hole 221 corresponding with connecting seat adjustment hole 211 realize the company of pedal connecting seat 21 and fixed seat 22
Connect, when changing the link position of fixture 23 and pedal connecting seat 21, pedal connecting seat 21 and the relative position of fixed seat 22 are sent out
Changing, realize that rudder pedals 1 and the distance between seat are adjustable.
Optionally embodiment, Fig. 1 is participated in, the top of fixture 23, which is connected with, facilitates the rotation process of fixture 23
Handle 231, fixture 23 and handle 231 can be bolt connection, and handle 231 is easy to the operation to fixture 23.
Optionally embodiment, Fig. 3, in addition to the locking member 24 for the part 23 that is locked are participated in, is connected along pedal
The length direction of joint chair 21 offers connecting seat locking hole 212, and fixed seat locking hole 222, locking member are offered in fixed seat 22
24 one end is fitted close with fixture 23, the other end passes through connecting seat locking hole 212 and corresponding fixed seat locking hole 222,
The fastening fastening members 23 of locking member 24, prevent fixture 23 from departing from, and fixture 23 is fixed on into connection pedal connecting seat 21 and fixed
On seat 22, security is improved, rudder pedals be in the serious consequence of uncontrollable state initiation when avoiding the fixed seat 23 from coming off
Situation.
Optionally embodiment, connecting seat locking hole 212 is arranged on the side of connecting seat adjustment hole 211, and connects
The distance at center to the center of two adjacent connecting seat locking holes 212 of seat adjustment hole 211 is equal, adds connection pedal and connects
The flexibility that joint chair 21 and fixed seat 22 coordinate, when pedal connecting seat 21 and fixed seat 22 are that inner hollow, cross sectional shape are
Rectangle, and when pedal connecting seat 21 is arranged in fixed seat 22, connection pedal connecting seat 21 can be inserted from the one end of fixed seat 22
Enter into fixed seat 22, can also be inserted from the other end of fixed seat 22, different mounting means can realize that connecting seat is locked
Tieholen 212 is engaged with corresponding fixed seat locking hole 222, i.e., the center of connecting seat locking hole 212 is locked with corresponding fixed seat
The center of tieholen 222 is conllinear, can realize the installation of locking member 24.Change pedal is moved along the length direction of pedal connecting seat 21
The relative position of connecting seat 21 and fixed seat 22, change the distance between rudder pedals 1 and seat.
The utility model provides direction rudder angles position adjusting mechanism and make it that rudder pedals are adjustable apart from the position of seat,
It is adapted to the pilot of different heights.
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 rudder angle position governor motion, it is characterised in that including rudder pedals (1), pedal position adjustment knot
Structure (2) and transmission mechanism, wherein：The pedal position adjustment structure (2) is connected to the rudder pedals (1) and the biography
Between motivation structure, the transmission mechanism is connected with rudder, and the rudder pedals (1) are trampled, energy during movement
Structure (2) is adjusted by the pedal position and drives the transmission mechanism and by the angle of transmission mechanism change rudder
And/or position, the distance between the rudder pedals (1) and seat can be changed by adjusting structure (2) by pedal position.
2. rudder angle position according to claim 1 governor motion, it is characterised in that the pedal position adjustment knot
Structure (2) includes pedal connecting seat (21), fixed seat (22) and for connecting the pedal connecting seat (21) and the fixed seat
(22) fixture (23), the pedal connecting seat (21) are connected with the rudder pedals (1), the fixed seat (22) with
Rudder angle position governor motion is connected, and rudder angle adjusting mechanism can be driven in fixed seat (22) moving process
Change angle and/or the position of rudder, when changing the fixture (23) and the link position of the pedal connecting seat (21),
The pedal connecting seat (21) and the relative position of the fixed seat (22) change.
3. rudder angle position according to claim 2 governor motion, it is characterised in that along the pedal connecting seat
(21) connecting seat adjustment hole (211) has been set on length direction, fixed seat adjustment hole is offered on the fixed seat (22)
(221), the fixture (23) inserts the connecting seat adjustment hole (211) and corresponding with the connecting seat adjustment hole (211)
The fixed seat adjustment hole (221) realizes the connection of the pedal connecting seat (21) and the fixed seat (22).
4. rudder angle position according to claim 2 governor motion, it is characterised in that the fixture (23) is pin
Axle.
5. rudder angle position according to claim 4 governor motion, it is characterised in that the top of the fixture (23)
End is connected with the handle (231) for facilitating the fixture (23) rotation process.
6. rudder angle position according to claim 2 governor motion, it is characterised in that also include described for locking
The locking member (24) of fixture (23), one end of the locking member (24) and the fixture (23) tight fit, the other end are solid
It is scheduled in the pedal connecting seat (21) or/and the fixed seat (22).
7. rudder angle position according to claim 5 governor motion, it is characterised in that along the pedal connecting seat
(21) length direction offers connecting seat locking hole (212), and fixed seat locking hole is offered on the fixed seat (22)
(222), one end of the locking member (24) passes through the connecting seat locking hole (212) and the corresponding fixed seat locking hole
(222)。
8. rudder angle position according to claim 7 governor motion, it is characterised in that the connecting seat locking hole
(212) it is arranged on the side of the connecting seat adjustment hole (211), and the center of the connecting seat adjustment hole (211) is to adjacent
The distance at the center of two connecting seat locking holes (212) is equal.
9. rudder angle position according to claim 2 governor motion, it is characterised in that the pedal connecting seat (21)
Be that inner hollow, cross sectional shape are rectangle with the fixed seat (22), and the pedal connecting seat (21) be arranged on it is described
In fixed seat (22), moved along the length direction of the pedal connecting seat (21) and change the pedal connecting seat (21) and described solid
The relative position of reservation (22).
10. a kind of aircraft, it is characterised in that including any described rudder angle position governor motions of claim 1-9.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720409553.1U CN206813298U (en) | 2017-04-18 | 2017-04-18 | Rudder angle position governor motion and aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720409553.1U CN206813298U (en) | 2017-04-18 | 2017-04-18 | Rudder angle position governor motion and aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206813298U true CN206813298U (en) | 2017-12-29 |
Family
ID=60753472
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720409553.1U Active CN206813298U (en) | 2017-04-18 | 2017-04-18 | Rudder angle position governor motion and aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206813298U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107097935A (en) * | 2017-04-18 | 2017-08-29 | 河北天启通宇航空器材科技发展有限公司 | Rudder angle position governor motion and aircraft |
-
2017
- 2017-04-18 CN CN201720409553.1U patent/CN206813298U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107097935A (en) * | 2017-04-18 | 2017-08-29 | 河北天启通宇航空器材科技发展有限公司 | Rudder angle position governor motion and aircraft |
| CN107097935B (en) * | 2017-04-18 | 2023-09-19 | 河北天启通宇航空器材科技发展有限公司 | Rudder angle position adjusting mechanism and aircraft |
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| GR01 | Patent grant | ||
| GR01 | Patent grant |