CN209600791U - A kind of rudder face linkage mechanism - Google Patents
A kind of rudder face linkage mechanism Download PDFInfo
- Publication number
- CN209600791U CN209600791U CN201920145783.0U CN201920145783U CN209600791U CN 209600791 U CN209600791 U CN 209600791U CN 201920145783 U CN201920145783 U CN 201920145783U CN 209600791 U CN209600791 U CN 209600791U
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- Prior art keywords
- steering engine
- rudder
- rocker arm
- bulb
- rudder face
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Abstract
The utility model discloses a kind of rudder face linkage mechanisms, the rudder face linkage mechanism includes vertical rudder face, connecting rod A, water rudder, connecting rod B and steering engine, mounting disc is fixed on the vertical rudder face, one vertical fin rocker arm is installed in the mounting disc, connecting shaft is fixed on the water rudder, water rudder rocker arm is installed, the both ends of the connecting rod A are respectively fixed with bulb A, and connecting rod A is rotatablely connected with the vertical fin rocker arm and the water rudder rocker arm respectively by the bulb A at both ends in connecting shaft；The both ends of the connecting rod B are respectively fixed with bulb B, and steering engine rocker arm is equipped on the output shaft of the steering engine；The rudder face linkage mechanism of the utility model can be realized the linkage of vertical rudder face and water rudder, easy to operate, reduces production and maintenance cost, reduces the weight of aircraft；On the one hand the utility model facilitates the installation of steering engine by the steering engine mounting base and bumper post of setting, on the other hand can reduce the damage of steering engine stress by bumper post, extend the service life of steering engine.
Description
Technical field
The utility model belongs to aircraft technical field, and in particular to a kind of rudder face linkage mechanism.
Background technique
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, is using radio robot and to provide for oneself
The not manned aircraft of presetting apparatus manipulation, or fully or intermittently automatically operated by car-mounted computer, rudder face is
The hinged small aerofoil or adjustable small fin of the main control surface of aircraft (aileron, elevator, rudder) rear, in gabarit, adjustment
Piece is the rear edge part of main control surface, and the degree of bias for controlling trimmer can change hinge moment on main control surface.
Existing aircraft is difficult to realize the linkage of vertical rudder face and water rudder, and additional drive control device is needed to be driven
It is dynamic, the problem of improving the cost of aircraft, expand the volume and weight of aircraft, thus it is proposed that a kind of rudder face links
Mechanism.
Utility model content
The purpose of this utility model is to provide a kind of rudder face linkage mechanisms, mentioned above in the background art existing to solve
Some aircrafts are difficult to realize the linkage of vertical rudder face and water rudder, need additional drive control device to be driven, improve
The cost of aircraft, the problem of expanding the volume and weight of aircraft.
To achieve the above object, the utility model provides the following technical solutions: a kind of rudder face linkage mechanism, rudder face linkage
Mechanism includes vertical rudder face, connecting rod A, water rudder, connecting rod B and steering engine, mounting disc is fixed on the vertical rudder face, in the mounting disc
On a vertical fin rocker arm is installed, connecting shaft is fixed on the water rudder, water rudder rocker arm, the connecting rod are installed in the connecting shaft
The both ends of A are respectively fixed with bulb A, and the connecting rod A by the bulb A at both ends respectively with the vertical fin rocker arm and the water
The rotation connection of rudder rocker arm；The both ends of the connecting rod B are respectively fixed with bulb B, are equipped with steering engine on the output shaft of the steering engine and shake
Arm, the connecting rod B are rotatablely connected with the water rudder rocker arm and the steering engine rocker arm respectively by the bulb B at both ends.
Preferably, further include steering engine mounting base, be respectively fixed in the both ends of the surface of the steering engine mounting base and to be arranged symmetrically
Fixinig plate；The inside of the steering engine mounting base is the installation room that can accommodate the steering engine.
Preferably, it is described installation room side wall on and inner bottom surface be separately installed with side buffer board and bottom buffer board,
The side buffer board and it is described installation room side wall between and the bottom buffer board and it is described installation room inner bottom surface it
Between distributing installation there are two the bumper posts of Relative distribution, be distributed between two bumper posts and be fixed on the side buffer board
And the carrying tablet on the bottom buffer board.
Preferably, longitudinal section of the carrying tablet is " L " type binding structure, and carrying is offered in the carrying tablet
Hole.
Preferably, the bumper post includes telescopic mast and fixed column, and the inside of the fixed column is offered for described flexible
The cushion chamber of column end insertion, one end of the cushion chamber are reciprocally actively embedded in the cushion chamber, and the other end stretches out institute
Cushion chamber is stated, buffer spring is distributed between the built-in end end face of the telescopic mast and the bottom of chamber of the cushion chamber.
Preferably, fixed restraining position ring block B on the inside of the port of the cushion chamber, the built-in end outer surface of the telescopic mast is fixed
Restraining position ring block A.
Preferably, bulb bearing is respectively equipped in the bulb A and the bulb B.
Compared with prior art, the utility model has the beneficial effects that
(1) the rudder face linkage mechanism of the utility model can be realized the linkage of vertical rudder face and water rudder, easy to operate, drop
Low production and maintenance cost, reduce the weight of aircraft；
(2) on the one hand the utility model facilitates the installation of steering engine, another party by setting steering engine mounting base and bumper post
Face can reduce the damage of steering engine stress by bumper post, extend the service life of steering engine.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of the utility model；
Fig. 2 is the portion the A enlarged structure schematic diagram of Fig. 1 of the utility model；
Fig. 3 is the portion the B enlarged structure schematic diagram of Fig. 1 of the utility model；
Fig. 4 is the portion the C enlarged structure schematic diagram of Fig. 1 of the utility model；
Fig. 5 is the steering engine mounting base forward sight structural schematic diagram of the utility model；
Fig. 6 is the steering engine mounting base overlooking structure diagram of the utility model；
Fig. 7 is the buffer board side structure schematic view of the utility model；
Fig. 8 is the bumper post forward sight schematic cross-sectional view of the utility model；
In figure: 1, vertical rudder face；2, connecting rod A；3, water rudder；4, mounting disc；5, vertical fin rocker arm；6, bulb A；7, connecting shaft；
8, connecting rod B；9, bulb B；10, water rudder rocker arm；11, steering engine；12, steering engine rocker arm；13, steering engine mounting base；14, side buffer board；
15, room is installed；16, bottom buffer board；17, bearing holes；18, carrying tablet；19, bumper post；20, fixinig plate；21, telescopic mast；22,
Fixed column；23, cushion chamber；24, buffer spring；25, stop collar A；26, stop collar B.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
Every other embodiment obtained, fall within the protection scope of the utility model.
Please refer to Fig. 1, Fig. 2, Fig. 3, Fig. 4, Fig. 5, Fig. 6, Fig. 7 and Fig. 8, the utility model provides a kind of technical solution: one
Kind rudder face linkage mechanism, which includes vertical rudder face 1, connecting rod A2, water rudder 3, connecting rod B8 and steering engine 11, vertical rudder
It is fixed with mounting disc 4 on face 1, a vertical fin Rocker arm 5 is installed in the mounting disc 4, is fixed with connecting shaft 7, connecting shaft on water rudder 3
Water rudder rocker arm 10 is installed, the both ends of connecting rod A2 are respectively fixed with bulb A6, and connecting rod A2 is distinguished by the bulb A6 at both ends on 7
It is rotatablely connected with vertical fin Rocker arm 5 and water rudder rocker arm 10；The both ends of connecting rod B8 are respectively fixed with bulb B9, the output shaft of steering engine 11
On steering engine rocker arm 12 is installed, connecting rod B8 is connected with water rudder rocker arm 10 and the rotation of steering engine rocker arm 12 respectively by the bulb B9 at both ends
It connects；Bulb bearing is respectively equipped in bulb A6 and bulb B9；It further include steering engine mounting base 13, in the both ends of the surface of steering engine mounting base 13
It is respectively fixed with the fixinig plate 20 being arranged symmetrically；The inside of steering engine mounting base 13 is the installation room 15 that can accommodate steering engine 11, installation
On the side wall of room 15 and inner bottom surface is separately installed with side buffer board 14 and bottom buffer board 16, side buffer board 14 and installation
There are two Relative distributions for distributing installation between the side wall of room 15 and between bottom buffer board 16 and the inner bottom surface for installing room 15
The carrying tablet being fixed on side buffer board 14 and bottom buffer board 16 is distributed between two bumper posts 19 in bumper post 19
18, longitudinal section of carrying tablet 18 is " L " type binding structure, and bearing holes 17 are offered in carrying tablet 18.
In the present embodiment, it is preferred that bumper post 19 includes telescopic mast 21 and fixed column 22, and the inside of fixed column 22 offers
For the cushion chamber 23 of 21 end of telescopic mast insertion, one end of cushion chamber 23 is reciprocally actively embedded in cushion chamber 23, the other end
Cushion chamber 23 is stretched out, buffer spring 24 is distributed between the built-in end end face of telescopic mast 21 and the bottom of chamber of cushion chamber 23, is buffered
Fixed restraining position ring block B26 on the inside of the port of chamber 23, the fixed restraining position ring block A25 in the built-in end outer surface of telescopic mast 21.
The working principle and process for using of the utility model: the output shaft driving steering engine rocker arm 12 of steering engine 11 rotates, thus
The bulb B9 of the one end drive link B8 is rotated, and connecting rod B8 does the reciprocating movement of left and right, and the bulb B9 of the connecting rod B8 other end is toward physical pendulum
It is dynamic, and 10 reciprocally swinging of water rudder rocker arm is driven, 3 reciprocally swinging of water rudder is driven by water rudder rocker arm 10, meanwhile, water rudder rocker arm 10 is logical
The bulb A6 for crossing the one end connecting rod A2 drives connecting rod A2 reciprocally swinging, so that connecting rod A2 be driven to drive by the bulb A6 of its other end
Vertical fin Rocker arm 5 reciprocally swinging drives vertical 1 reciprocally swinging of rudder face immediately, realizes the linkage of vertical rudder face 1 and water rudder 3；
Steering engine mounting base 13 is installed on aircraft, and steering engine 11 is mounted in the installation room 15 of steering engine mounting base 13, is passed through
Bolt is fixed, and side buffer board 14 and bottom buffer board 16 are arranged in installation room 15, and are in 11 output shaft of steering engine
On Impact direction, by squeezing side buffer board 14 and bottom buffer board 16, telescopic mast 21 is enabled to squeeze the buffering in cushion chamber 23
Spring 24 can realize buffering, in addition, carrying tablet 18 and bearing holes 17 also play the role of support buffering to a certain extent.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art,
It is understood that these embodiments can be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaired
Change, replacement and variant, the scope of the utility model is defined by the appended claims and the equivalents thereof.
Claims (7)
1. a kind of rudder face linkage mechanism, it is characterised in that: the rudder face linkage mechanism includes vertical rudder face (1), connecting rod A (2), water rudder
(3), connecting rod B (8) and steering engine (11) are fixed with mounting disc (4) on the vertical rudder face (1), are equipped in the mounting disc (4)
One vertical fin rocker arm (5) is fixed with connecting shaft (7) on the water rudder (3), is equipped with water rudder rocker arm (10) on the connecting shaft (7),
The both ends of the connecting rod A (2) are respectively fixed with bulb A (6), and the connecting rod A (2) by the bulb A (6) at both ends respectively with institute
State vertical fin rocker arm (5) and the water rudder rocker arm (10) rotation connection；The both ends of the connecting rod B (8) are respectively fixed with bulb B
(9), it is equipped with steering engine rocker arm (12) on the output shaft of the steering engine (11), the connecting rod B (8) is divided by the bulb B (9) at both ends
It is not rotatablely connected with the water rudder rocker arm (10) and the steering engine rocker arm (12).
2. a kind of rudder face linkage mechanism according to claim 1, it is characterised in that: further include steering engine mounting base (13), institute
State the fixinig plate (20) for being respectively fixed with and being arranged symmetrically in the both ends of the surface of steering engine mounting base (13)；The steering engine mounting base (13)
Inside is the installation room (15) that can accommodate the steering engine (11).
3. a kind of rudder face linkage mechanism according to claim 2, it is characterised in that: it is described installation room (15) side wall on
And inner bottom surface is separately installed with side buffer board (14) and bottom buffer board (16), the side buffer board (14) and the installation
There is distributing installation between the side wall of room (15) and between the bottom buffer board (16) and the inner bottom surface of installation room (15)
The bumper post (19) of two Relative distributions is distributed between two bumper posts (19) and is fixed on the side buffer board (14)
And the carrying tablet (18) on the bottom buffer board (16).
4. a kind of rudder face linkage mechanism according to claim 3, it is characterised in that: longitudinal section of the carrying tablet (18)
For " L " type binding structure, and bearing holes (17) are offered in the carrying tablet (18).
5. a kind of rudder face linkage mechanism according to claim 3, it is characterised in that: the bumper post (19) includes telescopic mast
(21) and fixed column (22), the inside of the fixed column (22) offer the cushion chamber for the insertion of the telescopic mast (21) end
(23), one end of the cushion chamber (23) is reciprocally actively embedded in the cushion chamber (23), and the other end stretches out the buffering
Buffer spring is distributed between the built-in end end face of the telescopic mast (21) and the bottom of chamber of the cushion chamber (23) in chamber (23)
(24)。
6. a kind of rudder face linkage mechanism according to claim 5, it is characterised in that: on the inside of the port of the cushion chamber (23)
The built-in end outer surface of fixed restraining position ring block B (26), the telescopic mast (21) is fixed restraining position ring block A (25).
7. a kind of rudder face linkage mechanism according to claim 1, it is characterised in that: the bulb A (6) and the bulb B
(9) bulb bearing is respectively equipped in.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920145783.0U CN209600791U (en) | 2019-01-28 | 2019-01-28 | A kind of rudder face linkage mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920145783.0U CN209600791U (en) | 2019-01-28 | 2019-01-28 | A kind of rudder face linkage mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209600791U true CN209600791U (en) | 2019-11-08 |
Family
ID=68402287
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920145783.0U Active CN209600791U (en) | 2019-01-28 | 2019-01-28 | A kind of rudder face linkage mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209600791U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110888459A (en) * | 2019-12-02 | 2020-03-17 | 中国空气动力研究与发展中心 | Vertical wind tunnel tail spin test model movable control surface deflection control mechanism |
| CN111674542A (en) * | 2020-06-19 | 2020-09-18 | 四川省天域航通科技有限公司 | Unmanned aerial vehicle's landing gear and unmanned aerial vehicle thereof |
-
2019
- 2019-01-28 CN CN201920145783.0U patent/CN209600791U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110888459A (en) * | 2019-12-02 | 2020-03-17 | 中国空气动力研究与发展中心 | Vertical wind tunnel tail spin test model movable control surface deflection control mechanism |
| CN111674542A (en) * | 2020-06-19 | 2020-09-18 | 四川省天域航通科技有限公司 | Unmanned aerial vehicle's landing gear and unmanned aerial vehicle thereof |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20200601 Address after: 243000 Huitong standardized workshop 5, Zhongfei Avenue, zhengpugang New District, Ma'anshan City, Anhui Province Patentee after: Anhui Zhixiang Aviation Technology Co.,Ltd. Address before: 723000 Aircraft Intelligence New Town of Liulin Town, Chenggu County, Hanzhong City, Shaanxi Province Patentee before: SHAANXI ZHIXIANG AVIATION TECHNOLOGY DEVELOPMENT Co.,Ltd. |
|
| TR01 | Transfer of patent right |