CN208140075U - A kind of rudder face gap measuring apparatus - Google Patents
A kind of rudder face gap measuring apparatus Download PDFInfo
- Publication number
- CN208140075U CN208140075U CN201820791614.XU CN201820791614U CN208140075U CN 208140075 U CN208140075 U CN 208140075U CN 201820791614 U CN201820791614 U CN 201820791614U CN 208140075 U CN208140075 U CN 208140075U
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- CN
- China
- Prior art keywords
- pedestal
- screw rod
- clamping
- rudder face
- measuring apparatus
- Prior art date
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Abstract
The utility model discloses a kind of rudder face gap measuring apparatus, including pedestal, fixed supporting mechanism, clamping device, displacement measurement mechanism and put slot, the fixed supporting mechanism is set on the rear and front end of pedestal, the clamping device is set to the middle of the base position, the displacement measurement mechanism is set to the rear end of pedestal, and the slot of putting is set on base upper surface side；The utility model structure is simple, and the measurement in gap is realized by automatic measurement test, can greatly improve measurement accuracy while meeting measurement request and reduce time of measuring, have stronger practicability.
Description
Technical field
The utility model relates to airplane component measuring technique related fieldss more particularly to a kind of rudder face clearance measurement to fill
It sets.
Background technique
The test of rudder face clearance measurement carries out a kind of automatic measurement test primarily directed to aircraft rudder surface gap.For aircraft
Left outside, right outer, left inside, right interior elevon rudder face, left and right canard rudder face, left and right front rudder surface, rudder surface etc. nine
Whether the rudder face gap of rudder face meets rudder face clearance requirement, and traditional measurement method is to be reinforced by counterweight form to rudder face
Implement measurement, this mode efficiency is lower, heavy workload.
Utility model content
The utility model provides a kind of rudder face gap measuring apparatus, to solve above-mentioned the deficiencies in the prior art, by automatic
The measurement to realize gap is tested in measurement, can be greatly improved measurement accuracy while meeting measurement request and be reduced measurement
Time has stronger practicability.
In order to realize the purpose of this utility model, the following technology of proposed adoption：
A kind of rudder face gap measuring apparatus, including pedestal, fixed supporting mechanism, clamping device, displacement measurement mechanism and
Slot is put, the fixed supporting mechanism is set on the rear and front end of pedestal, and the clamping device is set to the middle of the base position, described
Displacement measurement mechanism is set to the rear end of pedestal, and the slot of putting is set on base upper surface side；
It is several that the lower end of the pedestal is equipped with wheel, is equipped with rotation hole two on the rear and front end of the pedestal, described
The rear end of pedestal is equipped with handspike；
The quantity of the fixed supporting mechanism is two；
The fixed supporting mechanism includes rotary screw, and the rotary screw is set on the rear and front end of pedestal, the rotation
Turn screw rod between rotation hole, the upper end of the rotary screw is equipped with rotating wheel, and the lower end of the rotating wheel, which is equipped with, above to affect
Part, it is described on affect part to be assemblied on rotary screw, it is described on affect part side be equipped with rotating bar two, the rotating bar
Medium position be set in rotation hole, the lower end of the rotating bar is each equipped with lower drawing article, is all provided on the lower drawing article
There is support rod, the lower end of the support rod is equipped with support leg, and the upper end of the support rod is through on pedestal；
The clamping device includes lower branch screw rod, and the lower branch screw rod is set on pedestal, and the lower branch screw rod is equipped with down
Branch screw rod lifting turntable, the lower branch screw rod lifting turntable are located on the upper surface of pedestal, and the upper end of the lower branch screw rod is equipped with
Driving machine, the driving machine upper end are equipped with elevating lever, and the upper end of the elevating lever is equipped with pull pressure sensor, and the pressure passes
The upper end of sensor is equipped with support end, and the support end is equipped with clamping piece, and the clamping piece is equipped with holding tank, the folder
The front end of gripping member is equipped with end folder up and down, and the end folder includes clamping screw rod, before the clamping screw rod is set to clamping piece
Up and down, one end of the clamping screw rod is equipped with clamping disk, and the clamping disk is located in holding tank at end；
The displacement measurement mechanism includes lift adjustment screw rod, and the lower end of the lift adjustment screw rod is equipped on pedestal, institute
It states and turns on lift adjustment screw rod equipped with lift adjustment disk, the lift adjustment disk is located at the top of pedestal, the lift adjustment spiral shell
The upper end of bar is equipped with displacement measurement part, and the lower end of institute's displacement measurement part is connected with displacement sensor.
Further, the support leg is horseshoe configuration.
Further, the driving machine is hybrid linear motor.
Further, the clamping piece is U-shaped structure.
Further, the inside of the holding tank is equipped with soft buffer layer.
Further, the clamping face of the clamping disk is equipped with soft buffer layer.
Further, the length and width dimensions for putting slot are greater than the length and width dimensions of clamping piece.
The advantages of above-mentioned technical proposal, is：
1, the wheel being equipped with according to the utility model pedestal, facilitates device to carry out transfer movement, can be improved motor-driven spirit
Activity；The handspike which is provided with facilitates applied force in pushing meanss movement, to improve the practicability of device；
2, the fixation supporting mechanism being equipped with according to the utility model, when device measures rudder face gap, lower end is implemented
It is fixed, so that device stablizes raising, while the precision of device is improved, and get rid of previous needs and implement repeatedly to fix
Mode of operation, and operate the mechanism is positioned with regard to achievable lower end twice effect, the operating time of reduced fixation improves
The working efficiency of measurement；
3, the clamping device being equipped with according to the utility model can provide power for measurement rudder face gap, so that rudder
Face rotates, while measuring shift offset by displacement measurement mechanism, and be accurately controlled applied force for convenience
Size is equipped with pull pressure sensor on it, so as to realize the effect of accurate control rotation, to improve device
Measurement accuracy, and the height of holing clip being adjusted by lower branch screw rod, so that increase device facilitates operability, with
And increase the measurable space of device；It can be clamped in rudder face is stable in holding tank by clamping piece, and by upper
The clamping disk at lower both ends carries out a step and clamps rudder face, and the distinctive appearance structure in order to use clamped rudder face, clamping disk energy
It enough rotates, to improve range workable for whole device；
4, the displacement measurement mechanism being equipped with according to the utility model is the core component of whole device, and that replace existing
The general measure means that some is displaced by weight measurement improve the precision of displacement measurement using displacement sensor, and mention
The high efficiency of measurement, and can clearly react the collection for facilitating subsequent processing and mass data on computers
And scientific research；
5, slot is put according to what the utility model was equipped with, clamping piece can be placed in one when not using clamping piece, thus
Facilitate transfer and to clamping piece transfer when further protection, to extend the service life of device, and improve
The practicability of device.
6, the utility model structure is simple, and the measurement in gap is realized by automatic measurement test, can measure meeting
It is required that while, it greatly improves measurement accuracy and reduces time of measuring, there is stronger practicability.
Detailed description of the invention
It is practical to this below in conjunction with attached drawing in order to keep the purpose of this utility model, technical solution and advantage clearer
It is novel to be described in further detail.Wherein：
Fig. 1 shows the utility model three-dimensional structure diagram.
Specific embodiment
As shown in Figure 1, a kind of rudder face gap measuring apparatus, including pedestal 1, fixed supporting mechanism 2, clamping device 3, displacement
Measuring mechanism 4 and slot 5 is put, the fixed supporting mechanism 2 is set on the rear and front end of pedestal 1, and the clamping device 3 is set to
1 medium position of pedestal, the displacement measurement mechanism 4 are set to the rear end of pedestal 1, and the slot 5 of putting is set on 1 upper surface one of pedestal
Side；
The lower end of the pedestal 1 is several equipped with wheel 10, and 11 liang of rotation hole are equipped on the rear and front end of the pedestal 1
A, the rear end of the pedestal 1 is equipped with handspike 12；
The quantity of the fixed supporting mechanism 2 is two；
The fixed supporting mechanism 2 includes rotary screw 20, and the rotary screw 20 is set on the rear and front end of pedestal 1,
The rotary screw 20 is set between rotation hole 11, and the upper end of the rotary screw 20 is equipped with rotating wheel 21, the rotating wheel 21
Lower end be equipped with and above affect part 22, it is described on affect part 22 to be assemblied on rotary screw 20, it is described on affect on the side of part 22
Equipped with rotating bar 23 two, the medium position of the rotating bar 23 is set in rotation hole 11, and the lower end of the rotating bar 23 is equal
It is equipped with lower drawing article 24, support rod 25 is equipped on the lower drawing article 24, the lower end of the support rod 25 is equipped with support
The upper end of foot 26, the support rod 25 is through on pedestal 1；
The clamping device 3 includes lower branch screw rod 31, and the lower branch screw rod 31 is set on pedestal 1, the lower branch screw rod 31
It is equipped with lower branch screw rod lifting turntable 32, the lower branch screw rod lifting turntable 32 is located on the upper surface of pedestal 1, the lower branch spiral shell
The upper end of bar 31 is equipped with driving machine 33, and 33 upper end of driving machine is equipped with elevating lever 34, and the upper end of the elevating lever 34, which is equipped with, draws
Pressure sensor 35, the upper end of the pull pressure sensor 35 are equipped with support end 36, and the support end 36 is equipped with clamping
Part 37, the clamping piece 37 are equipped with holding tank 38, and the front end of the clamping piece 37 is equipped with end folder 39, the end folder up and down
Part 39 includes clamping screw rod 390, and the clamping screw rod 390 is set to the front end of clamping piece 37 or more, described to clamp the one of screw rod 390
End is equipped with clamping disk 391, and the clamping disk 391 is located in holding tank 38；
The displacement measurement mechanism 4 includes lift adjustment screw rod 40, and the lower end of the lift adjustment screw rod 40 is equipped with pedestal 1
On, turn be furnished with lift adjustment disk 41 on the lift adjustment screw rod 40, the lift adjustment disk 41 is located at the top of pedestal 1, institute
The upper end for stating lift adjustment screw rod 40 is equipped with displacement measurement part 42, and the lower end of institute's displacement measurement part 42 is connected with displacement sensor
43。
The support leg 26 is horseshoe configuration.
The driving machine 33 is hybrid linear motor.
The clamping piece 37 is U-shaped structure.
The inside of the holding tank 38 is equipped with soft buffer layer.
The clamping face of the clamping disk 391 is equipped with soft buffer layer.
The length and width dimensions for putting slot 5 are greater than the length and width dimensions of clamping piece 37.
When the utility model is used, one, clamping piece 37 taken out from putting in slot 5, and be installed at support end 36；
Two, clamping piece 37 is adjusted to proper height using lower branch screw rod lifting turntable 32；Three, rudder face is placed in holding tank 38, is rotated
Upper and lower two clampings screw rod 390, so that clamping disk 391 clamps rudder face；Four, lift adjustment disk 41 is adjusted, so that displacement measurement
Part 42 is located at the downside of rudder face and contact；Five, start driving machine 33, linear motor is used to load to rudder face, works as linear motor
It is controlled when power output reaches the value of 90kg or setting through computer and changes the linear motor direction of motion, and pull pressure sensor 35
Tension and compression force signal is output on Main Control Tank panel electric connector, data are for computer acquisition, calculating；Six, pass through displacement simultaneously
Measuring piece 42 measures displacement, and is passed the information on by displacement sensor 43 to computer.
Above-mentioned steps can be controlled by computer other than clipping operation and are automatically performed.
The above is only the preferred embodiment of the present invention, is not intended to limit the utility model, it is clear that this field
Technical staff various modification and variations can be carried out to the utility model without departing from the spirit and scope of the utility model.This
Sample, if these modifications and variations of the present invention belong to the claims of the present invention and its equivalent technology range it
Interior, then the utility model is also intended to include these modifications and variations.
Claims (7)
1. a kind of rudder face gap measuring apparatus, which is characterized in that including pedestal（1）, fixed supporting mechanism（2）, clamping device
（3）, displacement measurement mechanism（4）And put slot（5）, the fixed supporting mechanism（2）Set on pedestal（1）Rear and front end on,
The clamping device（3）Set on pedestal（1）Medium position, the displacement measurement mechanism（4）Set on pedestal（1）Rear end, it is described
Put slot（5）Set on pedestal（1）Upper surface side；
The pedestal（1）Lower end be equipped with wheel（10）It is several, the pedestal（1）Rear and front end on be equipped with rotation hole（11）
Two, the pedestal（1）Rear end be equipped with handspike（12）；
The fixed supporting mechanism（2）Quantity be two；
The fixed supporting mechanism（2）Including rotary screw（20）, the rotary screw（20）Set on pedestal（1）Rear and front end
On, the rotary screw（20）Set on rotation hole（11）Between, the rotary screw（20）Upper end be equipped with rotating wheel（21）, institute
State rotating wheel（21）Lower end be equipped with above affect part（22）, it is described on affect part（22）It is assemblied in rotary screw（20）On, it is described
On affect part（22）Side be equipped with rotating bar（23）Two, the rotating bar（23）Medium position be set to rotation hole
（11）It is interior, the rotating bar（23）Lower end be each equipped with lower drawing article（24）, the lower drawing article（24）On be equipped with support
Bar（25）, the support rod（25）Lower end be equipped with support leg（26）, the support rod（25）Upper end be through at pedestal（1）
On；
The clamping device（3）Including lower branch screw rod（31）, the lower branch screw rod（31）Set on pedestal（1）On, the lower branch spiral shell
Bar（31）It is equipped with lower branch screw rod lifting turntable（32）, the lower branch screw rod lifting turntable（32）Positioned at pedestal（1）Upper surface
On, the lower branch screw rod（31）Upper end be equipped with driving machine（33）, the driving machine（33）Upper end is equipped with elevating lever（34）, described
Elevating lever（34）Upper end be equipped with pull pressure sensor（35）, the pull pressure sensor（35）Upper end be equipped with support end
（36）, the support end（36）It is equipped with clamping piece（37）, the clamping piece（37）It is equipped with holding tank（38）, the clamping
Part（37）Front end be equipped with end folder up and down（39）, the end folder（39）Including clamping screw rod（390）, the clamping screw rod
（390）Set on clamping piece（37）Front end above and below, the clamping screw rod（390）One end be equipped with clamping disk（391）, the folder
Hold disk（391）Positioned at holding tank（38）It is interior；
The displacement measurement mechanism（4）Including lift adjustment screw rod（40）, the lift adjustment screw rod（40）Lower end be equipped with bottom
Seat（1）On, the lift adjustment screw rod（40）It is upper to turn be furnished with lift adjustment disk（41）, the lift adjustment disk（41）Positioned at pedestal
（1）Top, the lift adjustment screw rod（40）Upper end be equipped with displacement measurement part（42）, institute's displacement measurement part（42）Under
End is connected with displacement sensor（43）.
2. rudder face gap measuring apparatus according to claim 1, which is characterized in that the support leg（26）For horse-hof shape knot
Structure.
3. rudder face gap measuring apparatus according to claim 1, which is characterized in that the driving machine（33）It is hybrid straight
Line motor.
4. rudder face gap measuring apparatus according to claim 1, which is characterized in that the clamping piece（37）For U-shaped structure.
5. rudder face gap measuring apparatus according to claim 1, which is characterized in that the holding tank（38）Inside be equipped with
Soft buffer layer.
6. rudder face gap measuring apparatus according to claim 1, which is characterized in that the clamping disk（391）Clamping face
It is equipped with soft buffer layer.
7. rudder face gap measuring apparatus according to claim 1, which is characterized in that described to put slot（5）Length and width dimensions
Greater than clamping piece（37）Length and width dimensions.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820791614.XU CN208140075U (en) | 2018-05-25 | 2018-05-25 | A kind of rudder face gap measuring apparatus |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820791614.XU CN208140075U (en) | 2018-05-25 | 2018-05-25 | A kind of rudder face gap measuring apparatus |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208140075U true CN208140075U (en) | 2018-11-23 |
Family
ID=64314258
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820791614.XU Expired - Fee Related CN208140075U (en) | 2018-05-25 | 2018-05-25 | A kind of rudder face gap measuring apparatus |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208140075U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111252265A (en) * | 2018-12-03 | 2020-06-09 | 江西洪都航空工业集团有限责任公司 | Control surface clearance test equipment |
| CN113443168A (en) * | 2021-06-11 | 2021-09-28 | 江西洪都航空工业股份有限公司 | Device for fixedly detecting clearance of control surface of airplane |
| CN116986015A (en) * | 2023-09-28 | 2023-11-03 | 航天江南集团有限公司 | Steering engine detection device |
-
2018
- 2018-05-25 CN CN201820791614.XU patent/CN208140075U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111252265A (en) * | 2018-12-03 | 2020-06-09 | 江西洪都航空工业集团有限责任公司 | Control surface clearance test equipment |
| CN113443168A (en) * | 2021-06-11 | 2021-09-28 | 江西洪都航空工业股份有限公司 | Device for fixedly detecting clearance of control surface of airplane |
| CN116986015A (en) * | 2023-09-28 | 2023-11-03 | 航天江南集团有限公司 | Steering engine detection device |
| CN116986015B (en) * | 2023-09-28 | 2023-12-12 | 航天江南集团有限公司 | Steering engine detection device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20181123 Termination date: 20210525 |