CN207580197U - Boomerang unmanned plane test device is not played - Google Patents
Boomerang unmanned plane test device is not played Download PDFInfo
- Publication number
- CN207580197U CN207580197U CN201721677227.5U CN201721677227U CN207580197U CN 207580197 U CN207580197 U CN 207580197U CN 201721677227 U CN201721677227 U CN 201721677227U CN 207580197 U CN207580197 U CN 207580197U
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- upper plate
- fixing head
- slide bar
- unmanned plane
- fixedly connected
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Abstract
The utility model discloses one kind not to play boomerang unmanned plane test device, including upper plate, lower plate and the gas spring support column being set between upper plate and lower plate, upper plate center is centrally formed spherical pair with lower plate, and the clamping device for fixing unmanned plane stabilizer blade is provided on upper plate；The clamping device include single-degree-of-freedom be slidably connected to upper plate left fixing head and it is right fix head and for drive it is left fixing head and it is right fix head slid inward pre-tightening apparatus；The pre-tightening apparatus includes left slide bar, left extension spring, slide cartridge, right slide bar and right extension spring；The left end of left slide bar is fixedly connected on the left lower part for fixing head, and right end is in axial sliding connection in slide cartridge；Zola stretches spring pocket outside left slide bar and both ends are fixedly connected respectively with left fixing head and slide cartridge；The right end of right slide bar is fixedly connected on the right lower part for fixing head, and left end is axially slidably connected to slide cartridge；Right extension spring is sleeved on outside right slide bar and both ends are fixedly connected respectively with right fixing head and slide cartridge.
Description
Technical field
The utility model is related to a kind of unmanned apparatus test devices, more particularly to a kind of not play boomerang unmanned plane test device.
Background technology
Before unmanned plane comes into operation, it is essential process that debugging is carried out to unmanned plane.It needs to detect nothing during debugging
Man-machine static cental position, drives whether the installation situation of motor etc. of propeller will correctly carry out observation test at propeller；It is existing
Have in technology, detection needs unmanned plane to rolling takeoff, but unmanned plane rollings takeoff and debugged or tested, often will appear by
In it is when assembled carelessness by the anti-loaded either motor steering of propeller on the contrary, flight control system debug when data exception situations such as,
Cause to take off the phenomenon that falling machine and frequently occur.It is asked therefore, it is necessary to be improved to the prior art to solve above-mentioned technology
Topic.
Utility model content
The purpose of this utility model is to provide one kind not to play boomerang unmanned plane test device, can be without taking off to nothing
It is man-machine to be detected debugging, machine is fallen caused by reducing detection process to reduce loss.
The unmanned apparatus test device of the utility model, including upper plate, lower plate and the gas bullet being set between upper plate and lower plate
Spring support column, upper plate center are centrally formed spherical pair with lower plate, and the fixing dress for fixing unmanned plane stabilizer blade is provided on upper plate
It puts；
The clamping device includes single-degree-of-freedom and is slidably connected to the left fixing head of upper plate and right fixing head and for driving
It is left to fix head and the right pre-tightening apparatus for fixing head slid inward；The pre-tightening apparatus include left slide bar, left extension spring, slide cartridge,
Right slide bar and right extension spring；The left end of left slide bar is fixedly connected on the left lower part for fixing head, and right end is in axial sliding connection in cunning
Cylinder；Zola stretches spring pocket outside left slide bar and both ends are fixedly connected respectively with left fixing head and slide cartridge；The right end of right slide bar
The right lower part for fixing head is fixedly connected on, left end is axially slidably connected to slide cartridge；Right extension spring be sleeved on right slide bar it is outer and
Both ends are fixedly connected respectively with right fixing head and slide cartridge.
Further, it is provided with inclinator on the upper plate.
Further, it is provided with scale on the gas spring support column.
Further, the gas spring support column is set to upper plate and the corner of lower plate.
The beneficial effects of the utility model：The utility model does not play boomerang unmanned plane test device, is risen without unmanned plane
Whether normal and the utility model is simple in structure, easy to operate, manufacture is at low cost, warp for the winged performance that can just measure unmanned plane
Ji property is easy to use promotes well；It, can stretching according to gas spring support column under unmanned plane is in static when on the upper plate
Whether contracting situation judgement unmanned plane static cental position is normal；It, can be according to the deformation feelings of gas spring support column after unmanned plane starts
Condition observes aspect, to judge whether properller installation and flight control system parameter are normal；Other of the utility model have
Beneficial effect will combine embodiment in detail below and be further detailed.
Description of the drawings
The utility model is further described with reference to the accompanying drawings and examples：
Fig. 1 is the structure diagram of the utility model
Specific embodiment
Fig. 1 is the structure diagram of the utility model, as shown in the figure：Boomerang unmanned plane test dress is not played in the present embodiment
It puts, including upper plate 3, lower plate 8 and the gas spring support column 1 being set between upper plate 3 and lower plate 8, in 3 center of upper plate and lower plate 8
It is formed centrally spherical pair；Hemisphere 7 can be set in lower plate 8, bottom surface setting bulb-shaped recess and the hemisphere 7 of upper plate 3 form spherical pair,
Hemisphere, the top surface setting bulb-shaped recess of lower plate can certainly be set in the bottom surface of upper plate；It is provided with to fix nothing on upper plate 3
The clamping device of man-machine stabilizer blade 4；
The clamping device includes single-degree-of-freedom and is slidably connected to the left fixing head 2 of upper plate 3 and right fixing head 5 and for driving
The dynamic left pre-tightening apparatus for fixing head 2 and right fixing 5 slid inward of head；Using cunning between left fixing head 2 and right fixing head 5 and upper plate
Rail sliding slot realizes that single-degree-of-freedom is slidably connected；The pre-tightening apparatus includes left slide bar, left extension spring 11, slide cartridge 10, right slide bar
With right extension spring 9；The left end of left slide bar is fixedly connected on the left lower part for fixing head 2, and right end is in axial sliding connection in slide cartridge 10；
Left extension spring 11 is sleeved on outside left slide bar and both ends are fixedly connected respectively with left fixing head 2 and slide cartridge 10；The right side of right slide bar
End is fixedly connected on the right lower part for fixing head 5, and left end is axially slidably connected to slide cartridge 10；Right extension spring 9 is sleeved on right slide bar
Outer and both ends are fixedly connected respectively with right fixing head 5 and slide cartridge 10.
In the present embodiment, inclinator 6 is provided on the upper plate 3.Utilize unmanned plane centre-of gravity shift at inclinator detection
Concrete condition realizes quantitative detection.
In the present embodiment, scale is provided on the gas spring support column 1, is not indicated in figure.Visual pattern is shown
Unmanned plane center of gravity, propeller installation and flight control system parameter etc..
In the present embodiment, the gas spring support column 1 is set to upper plate 3 and the corner of lower plate 8.Rational deployment does not influence
The proper motion of spherical pair.
Finally illustrate, above example is merely intended for describing the technical solutions of the present application, but not for limiting the present application, although ginseng
The utility model is described in detail according to preferred embodiment, it will be understood by those of ordinary skill in the art that, it can be to this
The technical solution of utility model is modified or replaced equivalently, without departing from the objective and model of technical solutions of the utility model
It encloses, should all cover in the right of the utility model.
Claims (4)
1. one kind does not play boomerang unmanned plane test device, it is characterised in that：Including upper plate, lower plate and be set to upper plate and lower plate it
Between gas spring support column, upper plate center and lower plate are centrally formed spherical pair, are provided with to fix unmanned plane stabilizer blade on upper plate
Clamping device；
The clamping device includes single-degree-of-freedom and is slidably connected to the left fixing head of upper plate and right fixing head and for driving left card
Gu head and the right pre-tightening apparatus for fixing head slid inward；The pre-tightening apparatus includes left slide bar, left extension spring, slide cartridge, right cunning
Bar and right extension spring；The left end of left slide bar is fixedly connected on the left lower part for fixing head, and right end is in axial sliding connection in slide cartridge；It is left
Extension spring is sleeved on outside left slide bar and both ends are fixedly connected respectively with left fixing head and slide cartridge；The right end of right slide bar, which is fixed, to be connected
The right lower part for fixing head is connected to, left end is axially slidably connected to slide cartridge；Right extension spring is sleeved on outside right slide bar and both ends point
It is not fixedly connected with right fixing head and slide cartridge.
2. according to claim 1 do not play boomerang unmanned plane test device, it is characterised in that：It is provided with and inclines on the upper plate
Angle instrument.
3. according to claim 1 do not play boomerang unmanned plane test device, it is characterised in that：On the gas spring support column
It is provided with scale.
4. according to claim 1 do not play boomerang unmanned plane test device, it is characterised in that：The gas spring support column is set
It is placed in upper plate and the corner of lower plate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721677227.5U CN207580197U (en) | 2017-12-06 | 2017-12-06 | Boomerang unmanned plane test device is not played |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721677227.5U CN207580197U (en) | 2017-12-06 | 2017-12-06 | Boomerang unmanned plane test device is not played |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207580197U true CN207580197U (en) | 2018-07-06 |
Family
ID=62735852
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721677227.5U Active CN207580197U (en) | 2017-12-06 | 2017-12-06 | Boomerang unmanned plane test device is not played |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207580197U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113385913A (en) * | 2021-06-25 | 2021-09-14 | 成都飞机工业（集团）有限责任公司 | Lug joint locking mechanism with multi-degree-of-freedom adjustment |
-
2017
- 2017-12-06 CN CN201721677227.5U patent/CN207580197U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113385913A (en) * | 2021-06-25 | 2021-09-14 | 成都飞机工业（集团）有限责任公司 | Lug joint locking mechanism with multi-degree-of-freedom adjustment |
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| GR01 | Patent grant |