CN208468182U - A kind of aircraft control stick assembly ground joint-trial platform - Google Patents
A kind of aircraft control stick assembly ground joint-trial platform Download PDFInfo
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- CN208468182U CN208468182U CN201820518497.XU CN201820518497U CN208468182U CN 208468182 U CN208468182 U CN 208468182U CN 201820518497 U CN201820518497 U CN 201820518497U CN 208468182 U CN208468182 U CN 208468182U
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- erecting bed
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- control stick
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Abstract
A kind of aircraft control stick assembly ground joint-trial platform, its mounting structure of simulated flight device control stick assembly in aircraft cabin, is equipped with frame base and rear deck drives bar assembly erecting bed, rear deck rocker arm support, rear deck sealing shroud erecting bed, intermediate rockers support erecting bed, intermediate rockers mounting assembly, front deck sealing shroud erecting bed, front deck rocker arm support, front deck and drives bar assembly erecting bed, longitudinal damper and longitudinal drive person's sensor support base, double redundancy trim motor drive mechanism support；The frame base is fixed on level ground；The rear deck drives bar assembly erecting bed, rear deck sealing shroud erecting bed, intermediate rockers support erecting bed, front deck sealing shroud erecting bed, front deck and drives bar assembly erecting bed and be sequentially arranged on frame base from the front to the back.The utility model solves the problems, such as to be not easy to debugging operations after the installation of control stick assembly during twin overhaul, has achieved the purpose that improve working efficiency, guaranteed aircraft control stick general assembly reliability.
Description
Technical field
The utility model relates to a kind of aircraft control stick assembly ground joint-trial platforms, belong to test, field of measuring technique.
Background technique
With the continuous development of science and technology, electronic product specific gravity is increasing in aircraft control stick assembly, with
Traditional control stick assembly based on mechanical part compares, and has easy to operate, high reliablity, small in size, light-weight etc. one
Serial advantage, but since electronic product is more demanding to mutual matching, and with the promotion of aircraft performance,
All technical and control accuracy requirement to steerable system are also more stringent, especially for twin, drive at it
It sails and is equipped with rear deck driving bar assembly, rear deck rocker arm, rear deck rocker arm pull rod, intermediate rockers component, front deck rocker arm, front deck in bar assembly
Rocker arm pull rod, front deck drive bar assembly, longitudinal damper, longitudinal drive person's sensor and double redundancy trim motor drive mechanism, at this
During aircraft overhaul, the debugging work load for needing to carry out after the installation of control stick assembly is very big, the sky by aircraft cabin
Between limit, be not easy to very much debugging operations, working efficiency is lower.
To solve the above problems, people, which imagine, carries out debugging work in laboratory before the installation of twin control stick assembly
Industry, it is therefore desirable to design a kind of and consistent ground joint-trial of twin control stick assembly assembling structure in aircraft cabin
Platform.
Utility model content
The utility model provides a kind of aircraft control stick assembly ground joint-trial platform, it is intended to solve big in twin
During repairing, the problem of being not easy to debugging operations after the installation of control stick assembly, reaches and improves working efficiency, guarantees that aircraft drives
The purpose of bar general assembly reliability.
To achieve the above objectives, the present invention adopts the following technical solutions:
A kind of aircraft control stick assembly ground joint-trial platform, it simulates aircraft control stick assembly in aircraft cabin
In mounting structure, be equipped with frame base and rear deck and drive bar assembly erecting bed, rear deck rocker arm support, the installation of rear deck sealing shroud
Platform, intermediate rockers support erecting bed, intermediate rockers mounting assembly, front deck sealing shroud erecting bed, front deck rocker arm support, front deck drive
Bar assembly erecting bed, longitudinal damper and longitudinal drive person's sensor support base, double redundancy trim motor drive mechanism support；The frame
Pedestal is fixed on level ground；The rear deck drives bar assembly erecting bed, rear deck sealing shroud erecting bed, intermediate rockers support peace
Dress platform, front deck sealing shroud erecting bed, front deck drive bar assembly erecting bed and are sequentially arranged on frame base from the front to the back；After described
Cabin rocker arm support is fixed on rear deck and drives on bar assembly erecting bed；The intermediate rockers mounting assembly is fixed on intermediate rockers support
On erecting bed；The front deck rocker arm support is fixed on the bottom surface that front deck drives bar assembly erecting bed, the longitudinal damper and vertical
Front deck, which is fixed on, to driver sensor's support, double redundancy trim motor drive mechanism support drives the upper surface of bar assembly erecting bed.
Above-mentioned aircraft control stick assembly ground joint-trial platform, the rear deck sealing shroud erecting bed are vertically arranged board-like
Structure is arranged rear deck rocker arm pull rod on rear deck sealing shroud erecting bed and passes through hole.
Above-mentioned aircraft control stick assembly ground joint-trial platform, the front deck sealing shroud erecting bed are the board-like of inclination arrangement
Structure is arranged front deck rocker arm pull rod on front deck sealing shroud erecting bed and passes through hole.
Above-mentioned aircraft control stick assembly ground joint-trial platform, the intermediate rockers mounting assembly include left rear side rocker arm branch
Seat, right lateral side rocker arm support, front left side rocker arm support and forward right side rocker arm support, installation site and height respectively with aircraft
Counter element matches in the intermediate rockers component of control stick assembly.
Above-mentioned aircraft control stick assembly ground joint-trial platform, the longitudinal damper and longitudinal drive person's sensor support base
The integral structure being made of sensor support base part, damper abutment portion is arranged and is flown on damper abutment portion
The arc-shaped curved surface that longitudinal damper matches in row device control stick assembly.
Above-mentioned aircraft control stick assembly ground joint-trial platform, the rear deck rocker arm support are connected through a screw thread structure with after
Cabin drives the assembly of bar assembly erecting bed；Left rear side rocker arm support, right lateral side rocker arm support, a left side in the intermediate rockers mounting assembly
Front side rocker arm support and forward right side rocker arm support are connected through a screw thread structure and intermediate rockers support erecting bed assembles.
The utility model is a kind of aircraft control stick assembly ground joint-trial platform, it is during aircraft overhaul to driving
When sailing bar assembly and being debugged, control stick assembly can be mounted on the aircraft control stick assembly ground joint-trial platform, be passed through
Installation state is simulated, carries out the debugging process of aircraft control stick assembly in ground experiment room, due to no longer by aircraft
The space of cockpit limits, so that entire debugging process (including performance test and troubleshooting) is all very flexibly and convenient, when each
Part is installed again after debugging qualification, is not only increased working efficiency in this way, is avoided in debugging process in cockpit other zero
The damage of component, and ensure that aircraft control stick general assembly reliability.
Detailed description of the invention
Fig. 1 is the utility model structure diagram；
Fig. 2 is the K direction view of Fig. 1；
Fig. 3 is that rear deck drives bar assembly erecting bed, rear deck rocker arm support, rear deck sealing shroud erecting bed and frame base (office
Portion) structure and assembly relation schematic diagram；
Fig. 4 is that intermediate rockers support erecting bed, intermediate rockers mounting assembly, front deck sealing shroud erecting bed structure and assembly are closed
It is schematic diagram；
Fig. 5 is front deck rocker arm support, front deck driving bar assembly erecting bed, longitudinal damper and longitudinal drive person's sensor branch
Seat, double redundancy trim motor drive mechanism support and frame base (part) structure and assembly relation schematic diagram；
Fig. 6 is aircraft control stick assembly assembling schematic diagram on the joint-trial platform of aircraft control stick assembly ground.
Each list of reference numerals in figure are as follows: 1, rear deck driving bar assembly erecting bed, 2, rear deck rocker arm support, 3, rear deck sealing shroud peace
Platform is filled, 3-1, rear deck rocker arm pull rod pass through hole, 4, intermediate rockers mounting assembly, 4-1, left rear side rocker arm support, 4-2, right lateral side
Rocker arm support, 4-3, front left side rocker arm support, 4-4, forward right side rocker arm support, 5, intermediate rockers support erecting bed, 6, front deck it is close
Big envelope erecting bed, 6-1, front deck rocker arm pull rod pass through hole, 7, frame base, 8, front deck driving bar assembly erecting bed, 9, longitudinal resistance
Buddhist nun's device and longitudinal drive person's sensor support base, 10, double redundancy trim motor drive mechanism support, 11, front deck rocker arm support, 12, flight
Device control stick assembly.
Specific embodiment
With reference to the accompanying drawing and specific embodiment the utility model is described in further detail.
Referring to Fig. 1, Fig. 2, the utility model is a kind of aircraft control stick assembly ground joint-trial platform, it simulates flight
Mounting structure of the device control stick assembly 12 in aircraft cabin, be equipped with frame base 7 and rear deck drive bar assembly erecting bed 1,
Rear deck rocker arm support 2, rear deck sealing shroud erecting bed 3, intermediate rockers support erecting bed 5, intermediate rockers mounting assembly 4, front deck are close
Big envelope erecting bed 6, front deck rocker arm support 11, front deck drive bar assembly erecting bed 8, longitudinal damper and longitudinal drive person's sensor
Support 9, double redundancy trim motor drive mechanism support 10；The frame base 7 is fixed on level ground；The rear deck control stick group
Part erecting bed 1, rear deck sealing shroud erecting bed 3, intermediate rockers support erecting bed 5, front deck sealing shroud erecting bed 6, front deck control stick
Component erecting bed 8 is sequentially arranged at from the front to the back on frame base 7.
Referring to Fig. 3, aircraft control stick assembly ground described in the utility model joint-trial platform, the rear deck rocker arm support 2
Rear deck is fixed on to drive on bar assembly erecting bed 1；The rear deck sealing shroud erecting bed 3 is vertically arranged plank frame, rear
Rear deck rocker arm pull rod is set on cabin sealing shroud erecting bed 3 and passes through hole 3-1.
Referring to Fig. 4, aircraft control stick assembly ground described in the utility model joint-trial platform, the intermediate rockers support group
Part 4 is fixed on intermediate rockers support erecting bed 5, and intermediate rockers mounting assembly 4 includes left rear side rocker arm support 4-1, right lateral side
Rocker arm support 4-2, front left side rocker arm support 4-3 and forward right side rocker arm support 4-4, their installation site and height respectively with
Counter element matches in the intermediate rockers component of aircraft control stick assembly 12；The front deck sealing shroud erecting bed 6 is inclination
The plank frame of arrangement is arranged front deck rocker arm pull rod on front deck sealing shroud erecting bed 6 and passes through hole 6-1.
Referring to Fig. 5, aircraft control stick assembly ground described in the utility model joint-trial platform, the front deck rocker arm support 11
It is fixed on the bottom surface that front deck drives bar assembly erecting bed 8, it is the longitudinal damper and longitudinal drive person's sensor support base 9, double remaining
Degree trim motor drive mechanism support 10 is fixed on front deck and drives the upper surface of bar assembly erecting bed 8；The longitudinal damper and longitudinal direction are driven
The integral structure that the person's of sailing sensor support base 9 is made of sensor support base part 9-1, damper abutment portion 9-2, is damping
The arc-shaped curved surface to match with longitudinal damper in aircraft control stick assembly 12 is set on device abutment portion 9-2.
Referring to Fig. 6, the utility model is a kind of aircraft control stick assembly ground joint-trial platform, it is in aircraft overhaul
When debugging in journey to aircraft control stick assembly 12, aircraft control stick assembly 12 can be mounted on to aircraft driving
On the joint-trial platform of bar assembly ground, by simulating installation state, make the debugging process of aircraft control stick assembly 12 in ground reality
It tests in room and carries out, since the space no longer by aircraft cabin is limited, so that entire debugging process (including performance test and failure
Exclude) it is all very flexibly and convenient, it installs again after various pieces debug qualification, not only increases working efficiency in this way, avoids
To the damage of components other in cockpit in debugging process, and it ensure that aircraft control stick general assembly reliability.
Claims (6)
1. a kind of aircraft control stick assembly ground joint-trial platform, characterized in that it simulates aircraft control stick assembly (12)
Mounting structure in aircraft cabin, is equipped with frame base (7) and rear deck drives bar assembly erecting bed (1), rear deck rocker arm branch
Seat (2), rear deck sealing shroud erecting bed (3), intermediate rockers support erecting bed (5), intermediate rockers mounting assembly (4), front deck sealing
Erecting bed (6), front deck rocker arm support (11), front deck driving bar assembly erecting bed (8), longitudinal damper and longitudinal drive person is covered to pass
Sensor support (9), double redundancy trim motor drive mechanism support (10)；The frame base (7) is fixed on level ground；After described
Cabin drives bar assembly erecting bed (1), rear deck sealing shroud erecting bed (3), intermediate rockers support erecting bed (5), front deck sealing shroud peace
Dress platform (6), front deck drive bar assembly erecting bed (8) and are sequentially arranged on frame base (7) from the front to the back；The rear deck rocker arm branch
Seat (2) is fixed on rear deck and drives on bar assembly erecting bed (1)；The intermediate rockers mounting assembly (4) is fixed on intermediate rockers branch
On seat erecting bed (5)；The front deck rocker arm support (11) is fixed on the bottom surface that front deck drives bar assembly erecting bed (8), described vertical
Front deck control stick is fixed on to damper and longitudinal drive person's sensor support base (9), double redundancy trim motor drive mechanism support (10)
The upper surface of component erecting bed (8).
2. aircraft control stick assembly ground according to claim 1 joint-trial platform, characterized in that the rear deck sealing shroud
Erecting bed (3) is vertically arranged plank frame, and rear deck rocker arm pull rod is arranged on rear deck sealing shroud erecting bed (3) and passes through hole
(3-1)。
3. aircraft control stick assembly ground according to claim 2 joint-trial platform, characterized in that the front deck sealing shroud
Erecting bed (6) is the plank frame being in tilted layout, and front deck rocker arm pull rod is arranged on front deck sealing shroud erecting bed (6) and passes through hole
(6-1)。
4. aircraft control stick assembly ground according to claim 3 joint-trial platform, characterized in that the intermediate rockers branch
Holder assembly (4) includes left rear side rocker arm support (4-1), right lateral side rocker arm support (4-2), front left side rocker arm support (4-3) and the right side
Front side rocker arm support (4-4), their installation site and height the intermediate rockers group with aircraft control stick assembly (12) respectively
Counter element matches in part.
5. aircraft control stick assembly ground according to claim 4 joint-trial platform, characterized in that the longitudinal damper
And longitudinal drive person's sensor support base (9) be made of sensor support base part (9-1), damper abutment portion (9-2) one
Body formula structure is arranged on damper abutment portion (9-2) and matches with longitudinal damper in aircraft control stick assembly (12)
Arc-shaped curved surface.
6. aircraft control stick assembly ground according to claim 4 or 5 joint-trial platform, characterized in that the rear deck shakes
Arm support (2) is connected through a screw thread structure and rear deck drives bar assembly erecting bed (1) assembly；The intermediate rockers mounting assembly
(4) left rear side rocker arm support (4-1), right lateral side rocker arm support (4-2), front left side rocker arm support (4-3) and forward right side rocker arm in
Support (4-4) is connected through a screw thread structure and intermediate rockers support erecting bed (5) assembles.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820518497.XU CN208468182U (en) | 2018-04-12 | 2018-04-12 | A kind of aircraft control stick assembly ground joint-trial platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820518497.XU CN208468182U (en) | 2018-04-12 | 2018-04-12 | A kind of aircraft control stick assembly ground joint-trial platform |
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| Publication Number | Publication Date |
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| CN208468182U true CN208468182U (en) | 2019-02-05 |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108453650A (en) * | 2018-04-12 | 2018-08-28 | 中国人民解放军第五七二工厂 | A kind of aircraft control stick assembly debugging tool |
-
2018
- 2018-04-12 CN CN201820518497.XU patent/CN208468182U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108453650A (en) * | 2018-04-12 | 2018-08-28 | 中国人民解放军第五七二工厂 | A kind of aircraft control stick assembly debugging tool |
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