CN207242014U - A kind of device connected for unmanned plane rudder face with stabilization - Google Patents
A kind of device connected for unmanned plane rudder face with stabilization Download PDFInfo
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- CN207242014U CN207242014U CN201721041223.8U CN201721041223U CN207242014U CN 207242014 U CN207242014 U CN 207242014U CN 201721041223 U CN201721041223 U CN 201721041223U CN 207242014 U CN207242014 U CN 207242014U
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- bearing
- stabilization
- rudder face
- suspender member
- connection component
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Abstract
A kind of device connected for unmanned plane rudder face with stabilization is the utility model is related to, is made of end connection component and middle part connection component；End connection component is by end-fitting, end suspender member, gasket, UG oscillating bearings, self-locking nut and end bearing shell composition；One end of end-fitting is directly anchored on the beam of rudder face, and the other end of end-fitting is shaft, is connected in bearing embedded on fixed stabilization suspender member, for connecting rudder face and fixed stabilization；On the directly fixed stabilization beam face in end suspender member bottom surface, bearing card slot, fixing joint bearing, for connecting stabilization and bearing, and fixing bearing position are arranged at top.The utility model can effectively solve horizontal rudder face to be occurred slipping or stuck phenomenon during upper lower rotary shaft, and structure is easy to the care and maintenance of unmanned plane, and the steel alloy material of connector can be with elongate member service life.
Description
Technical field
Unmanned plane rudder face and stabilization interconnection technique field are the utility model is related to, is that one kind is used for nobody specifically
The device that machine rudder face is connected with stabilization.
Background technology
Unmanned airplane empennage is used for keeping longitudinal direction and the course balance of aircraft, aircraft is had longitudinal direction and shipping-direction stability, behaviour
Vertical property.Usually it is made of tailplane (horizontal stabilizer, elevator) and vertical tail (fixed fin, rudder).It is stable
Face is usually fixed, and rudder face can then manipulate.Connection and its important, such as appearance between the lifting rudder face and stabilization of tailplane
Slippage or stuck phenomenon, will influence aircraft and carry out pitch control.The utility model mainly solves unmanned plane tailplane rudder face
Slippage or the stuck phenomenon of appearance are connected between fixed stabilization, the utility model is simple and practical, and cost is low, such as parts depreciation
The advantages that being easily changed maintenance and maintenance.
Based on this, present application is made.
Utility model content
The purpose of the utility model is to overcome the deficiencies in the prior art, there is provided one kind is used for unmanned plane rudder face and stabilization
The device of connection.
The purpose of this utility model is achieved through the following technical solutions：
A kind of device connected for unmanned plane rudder face with stabilization, by end connection component and middle part connection component group
Into；End connection component is by end-fitting, end suspender member, gasket, UG oscillating bearings, self-locking nut and end bearing shell composition；
Middle part connection component is made of center contact, middle part bearing shell, middle part suspender member, gasket, UG oscillating bearings and self-locking nut；End
One end of connector is directly anchored on the beam of rudder face, and the other end of end-fitting is shaft, is connected to fixed stabilization suspender member
In the bearing of upper insertion, for connecting rudder face and fixed stabilization；On the directly fixed stabilization beam face in end suspender member bottom surface, on
There are bearing card slot, fixing joint bearing, for connecting stabilization and bearing, and fixing bearing position in portion.
Gap spacing adjusts and fixes the effect of rudder face Y-direction position between gasket rudder face and stabilization, prevents on rudder face
During lower rotation, double swerve；
UG oscillating bearings are rotated for end-fitting, and effectively prevent bearing and end-fitting when rudder face is slightly tilted rotation
The stuck phenomenon of appearance；
Self-locking nut is fixed on the screw top end of end-fitting, effectively prevents rudder face connector from slipping；
Bearing card slot also is provided with the inside of end bearing shell, in bearing, gasket, connector and self-locking nut are after installation is complete, then use
Bearing shell is fixed on suspender member by screw bolt and nut, and oscillating bearing Y-direction position is fixed, prevents oscillating bearing double swerve.
Middle part connection component is by center contact, middle part bearing shell, middle part suspender member, gasket, UG oscillating bearings and self-locking nut
Form；
Gasket is HB1-521 gaskets；
Self-locking nut is GB1337 self-locking nuts；
Middle part connection component is identical with end connection component operation principle, and only middle part suspender member structural shape is different, middle part
Suspender member both ends connect the connector of both sides, and middle part suspender member bottom surface is fixed in the middle part of stabilization, the joint at middle part suspender member both ends
After the completion of bearing, gasket are connected with self-locking nut, then middle part bearing shell is fixed on middle part and is hung, and end connection component is together
Both sides rudder face Y-direction position is fixed, prevents rudder face from slipping or deviating.
Further, shape can be changed according to rudder face structure type as end-fitting, connector shaft end can be according to specific position
Put the length and size that each section of axis is adjusted with the model of oscillating bearing；End suspender member can be changed according to stabilization planform
Shape, and according to the form and dimension of bearing designation change card slot；Card slot can be carried out according to the model of oscillating bearing in the middle part of bearing shell
Adjustment；Suspender member and bearing shell two-half structure, easy to disassemble, maintenance and maintenance, are furtherly easy to check junction situation
And the vulnerable part such as bearing or connector is replaced in time.
The application unmanned plane end face and stabilization connection method are mainly a kind of unmanned plane rudder face and stabilization connection method,
It is made of end connection component and middle part connection component.End connection component is padded by end-fitting, end suspender member, HB1-521
Piece, UG oscillating bearings, GB1337 self-locking nuts and end bearing shell are formed；Middle part connection component by center contact, middle part bearing shell, in
Portion's suspender member, HB1-521 gaskets, UG oscillating bearings and GB1337 self-locking nuts are formed.End and middle part suspender member are using boat
Empty 7050 or 7075 aluminium alloys, it is light-weight, intensity is good.Connector is because rotation needs wearability good, and intensity is high, to prevent joint axis from becoming
Shape, it is stuck when rudder face is swung up and down, therefore connector uses high rigidity 30CrMnSiA hard alloy steels, wearability is good.Connector and
Belong to interference fit between bearing, the stage casing axis of all connectors uses h6 tolerance fits.Gasket, oscillating bearing and self-locking nut
Equal selection standard part, so easy to purchase.
The operation principle of the utility model is：In the middle part of stabilization and both ends installation suspender member, the erection joint of rudder face both sides,
After filling gasket and oscillating bearing on connector, oscillating bearing is embedded into suspender member card slot, then spacer is put into connector both sides
Self-locking nut is installed after piece, finally bearing shell is fixed on suspender member using bolt and nut, bearing Y-direction position is fixed.Need
Only need first to remove bearing shell when replacing component or maintenance.
Compared with prior art, the good effect of the utility model is：
The utility model can effectively solve horizontal rudder face to be occurred slipping or stuck existing during upper lower rotary shaft
As, and structure is easy to the care and maintenance of unmanned plane, and the steel alloy material of connector can be with elongate member service life.
This case connector uses steel alloy, can prevent joints wear；Connection transition uses oscillating bearing, can effectively prevent
Directly there is stuck phenomenon in bearing and end connecting joint when rudder face is slightly tilted rotation；There is card inside bearing shell and suspender member
Groove, bearing shell are fixed on suspender member, and both sides are adjusted with after self-locking nut fixation by gasket, can consolidate both sides rudder face Y-direction position
It is fixed, prevent rudder face from slipping or deviating.Junction is checked in suspender member and bearing shell two-half structure, easy to disassemble, maintenance and maintenance, and
The vulnerable part such as bearing or connector is replaced in time.The utility model is simple and practical in structure, and cost is low, and service life length, also allows for
The care and maintenance of unmanned plane moving component.
Brief description of the drawings
Fig. 1 is the schematic diagram of termination connection component；
Fig. 2 is termination connection component profile；
Fig. 3 is middle part connection component schematic diagram；
Fig. 4 is middle part connection component profile；
Fig. 5 is connector schematic diagram；
Fig. 6 is end suspender member schematic diagram；
Fig. 7 is middle part suspender member schematic diagram；
Fig. 8 is bearing shell schematic diagram；
Figure label：1. end-fitting；2 end suspender members；3HB1-521 gaskets；4UG oscillating bearings；5GB1337 self-lockings
Nut；6 end bearing shells；7 center contacts；8 middle part bearing shells；9 middle part suspender members.
Embodiment
A kind of embodiment of the device connected for unmanned plane rudder face with stabilization of the utility model presented below.
Embodiment 1
A kind of device connected for unmanned plane rudder face with stabilization of the present embodiment, mainly by end connection component and middle part
Connection component forms, and refers to Fig. 1-4.Mainly hung with reference to figure end connection component and middle part connection component by end-fitting 1, end
Suspension member 2, HB1-521 gaskets 3, UG oscillating bearings 4, GB1337 self-locking nuts 5；End bearing shell 6, center contact 7, middle part bearing shell 8,
Middle part suspender member 9 is formed.End-fitting 1 and center contact 7 are connected on rudder face, and end suspender member 2 and middle part suspender member 9 connect
On stabilization, oscillating bearing 4 is installed on end connecting joint and middle part jointing stage casing axis, and gasket 3 is in end-fitting 1
With on the axis of stage casing, self-locking nut 5 is fixed in end-fitting 1 and center contact 7 in top end shaft in center contact 7, its center tap,
End suspender member, middle part suspender member and bearing shell can restructure according to stabilization and rudder face structural shape, oscillating bearing model etc.
Shape, refers to Fig. 5-8.
A kind of unmanned plane rudder face of the application and stabilization connection method, mainly by end connection component and middle part connection component
Composition.End connection component is by end-fitting 1, end suspender member 2, HB1-521 gaskets 3, UG oscillating bearings 4, GB1337 self-lockings
Nut 5 and end bearing shell 6 are formed；Middle part connection component is padded by center contact 7, middle part bearing shell 8, middle part suspender member 9, HB1-521
Piece 3, UG oscillating bearings 4 and GB1337 self-locking nuts 5 are formed.First stabilization both ends and middle-end installation suspender member 2 and 9, rudder face two
Side erection joint 1 and 7, it is respectively that oscillating bearing 4 is embedding after gasket 3 and oscillating bearing 4 are installed on the connector of rudder face both sides respectively
Enter into 2 and 9 card slot of suspender member, then self-locking nut 5 is installed after being put into adjusting gasket 3 in the both sides of connector 1 and 7, finally use
Bearing shell 6 and 8 is fixed on suspender member 2 and 9 by bolt and nut respectively, and bearing Y-direction position is fixed.Need replacing component or maintenance
When only need first to remove bearing shell.
The application can effectively solve horizontal rudder face to be occurred slipping or stuck phenomenon during upper lower rotary shaft, and
And simple in structure it is easy to care and maintenance.
The above is only the preferred embodiment of the utility model, it is noted that for the common skill of the art
Art personnel, without departing from the concept of the premise utility, can also make some improvements and modifications, these improvements and modifications
Also should be regarded as in the scope of protection of the utility model.
Claims (1)
1. a kind of device connected for unmanned plane rudder face with stabilization, it is characterised in that connected by end connection component and middle part
Connected components form；End connection component is by end-fitting, end suspender member, gasket, UG oscillating bearings, self-locking nut and end axis
Watt composition；One end of end-fitting is directly anchored on the beam of rudder face, and the other end of end-fitting is shaft, is connected to fixed peace
Determine in bearing embedded on the suspender member of face, for connecting rudder face and fixed stabilization；End suspender member bottom surface is directly fixed stable
On the beam face of face, bearing card slot, fixing joint bearing, for connecting stabilization and bearing, and fixing bearing position are arranged at top.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721041223.8U CN207242014U (en) | 2017-08-19 | 2017-08-19 | A kind of device connected for unmanned plane rudder face with stabilization |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721041223.8U CN207242014U (en) | 2017-08-19 | 2017-08-19 | A kind of device connected for unmanned plane rudder face with stabilization |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207242014U true CN207242014U (en) | 2018-04-17 |
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ID=61881939
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721041223.8U Active CN207242014U (en) | 2017-08-19 | 2017-08-19 | A kind of device connected for unmanned plane rudder face with stabilization |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207242014U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109080814A (en) * | 2018-09-30 | 2018-12-25 | 西安爱生技术集团公司 | A kind of full-height foam core unmanned plane lifting rudder face shaft installing mechanism |
| CN112373687A (en) * | 2020-11-17 | 2021-02-19 | 中航通飞华南飞机工业有限公司 | Large-scale seaplane rudder face suspension structure |
-
2017
- 2017-08-19 CN CN201721041223.8U patent/CN207242014U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109080814A (en) * | 2018-09-30 | 2018-12-25 | 西安爱生技术集团公司 | A kind of full-height foam core unmanned plane lifting rudder face shaft installing mechanism |
| CN112373687A (en) * | 2020-11-17 | 2021-02-19 | 中航通飞华南飞机工业有限公司 | Large-scale seaplane rudder face suspension structure |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP03 | Change of name, title or address | ||
| CP03 | Change of name, title or address |
Address after: 312000 Building 2, Haitu jiuyiqiu, Binhai Industrial Zone, Keqiao District, Shaoxing City, Zhejiang Province Patentee after: Shaoxing Baojing composite material Co.,Ltd. Patentee after: JINGGONG (SHAOXING) COMPOSITE TECHNOLOGY R & D CO.,LTD. Address before: 312030 Building 2, Haitu jiuyiqiu, Binhai Industrial Zone, Keqiao District, Shaoxing City, Zhejiang Province Patentee before: JINGGONG (SHAOXING) COMPOSITE MATERIAL CO.,LTD. Patentee before: JINGGONG (SHAOXING) COMPOSITE TECHNOLOGY R & D CO.,LTD. |
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| CP01 | Change in the name or title of a patent holder | ||
| CP01 | Change in the name or title of a patent holder |
Address after: 312000 Building 2, Haitu jiuyiqiu, Binhai Industrial Zone, Keqiao District, Shaoxing City, Zhejiang Province Patentee after: Shaoxing Baojing composite material Co.,Ltd. Patentee after: Shaoxing Baojing Composite Technology Research and Development Co.,Ltd. Address before: 312000 Building 2, Haitu jiuyiqiu, Binhai Industrial Zone, Keqiao District, Shaoxing City, Zhejiang Province Patentee before: Shaoxing Baojing composite material Co.,Ltd. Patentee before: JINGGONG (SHAOXING) COMPOSITE TECHNOLOGY R & D CO.,LTD. |