CN107839897A - The disconnected oar test device of unmanned plane - Google Patents
The disconnected oar test device of unmanned plane Download PDFInfo
- Publication number
- CN107839897A CN107839897A CN201711130198.5A CN201711130198A CN107839897A CN 107839897 A CN107839897 A CN 107839897A CN 201711130198 A CN201711130198 A CN 201711130198A CN 107839897 A CN107839897 A CN 107839897A
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- China
- Prior art keywords
- unmanned plane
- test device
- breaks
- support bar
- support
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- 238000012360 testing method Methods 0.000 title claims abstract description 44
- 238000013016 damping Methods 0.000 claims abstract description 25
- 230000001105 regulatory effect Effects 0.000 claims description 9
- 238000010586 diagram Methods 0.000 description 8
- 238000005516 engineering process Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- UPLPHRJJTCUQAY-WIRWPRASSA-N 2,3-thioepoxy madol Chemical compound C([C@@H]1CC2)[C@@H]3S[C@@H]3C[C@]1(C)[C@@H]1[C@@H]2[C@@H]2CC[C@](C)(O)[C@@]2(C)CC1 UPLPHRJJTCUQAY-WIRWPRASSA-N 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000000007 visual effect Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/60—Testing or inspecting aircraft components or systems
Landscapes
- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Transportation (AREA)
- Aviation & Aerospace Engineering (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
Abstract
The present invention relates to a kind of disconnected oar test device of unmanned plane, it includes：Support, the governor motion being installed on support, the supporting mechanism being connected with governor motion.Governor motion is protruded out including the base being installed on support, the support column being installed on base, the adjusting set being placed on support column, self-regulation set inside and rotatable spherical support bar, the damping adjusting knob and reclining lock knob that are installed in adjusting set, one end of spherical support bar abuts with support column, the other end of spherical support bar is connected with supporting mechanism, damping adjusting knob is horizontally through adjusting set and abutted with the support column, and reclining lock knob is horizontally through adjusting set and abutted with spherical support bar.The disconnected oar test device of the unmanned plane is by damping adjusting knob, the setting of reclining lock knob can carry out corresponding regulation to logical flight progress, is easy to the test of different flight attitudes, rational in infrastructure.
Description
Technical field
The present invention relates to unmanned air vehicle technique field, more particularly to a kind of disconnected oar test device of unmanned plane.
Background technology
With the continuous development and the extensive use of more rotation oar unmanned planes in recent years of unmanned air vehicle technique, when more rotation oar unmanned planes
In high-altitude flight, by complex internal system and external environment influence, disconnected oar state out of control often occurs, once air crash
It can bring about very big loss.In order to which to more rotation oar unmanned planes, various operational factors have further in the case of the disconnected oar of difference
Solution, the various reply performances of more rotation oar unmanned planes are improved, are clear how to avoid air crash, often more rotation oar unmanned planes broken
Oar test experiments.But the unreasonable structure of disconnected oar test device at present, it can not be adjusted according to being actually needed to realize pair
The test of different flight attitudes, makes troubles to test.
The content of the invention
Based on this, it is necessary to for unmanned plane break oar test exist the problem of, there is provided a kind of rational in infrastructure, adjustability is strong
The disconnected oar test device of unmanned plane.
A kind of disconnected oar test device of unmanned plane, including：Support, the governor motion being installed on the support and the tune
Save the supporting mechanism of mechanism connection；The governor motion include be installed on the support base, be installed on the base
Support column, be placed on the support column adjusting set, protrude out from inside the adjusting set and rotatable spherical support bar,
The damping adjusting knob and reclining lock knob being installed in the adjusting set, one end and the support of the spherical support bar
Post is abutted, and the other end of the spherical support bar is connected with the supporting mechanism, and the damping adjusting knob is horizontally through described
Adjusting set abuts with the support column, and the reclining lock knob is horizontally through the adjusting set and supported with the spherical support bar
Connect.
Above-mentioned unmanned plane breaks oar test device, including support, be installed on support governor motion, be connected with governor motion
Supporting mechanism, in use, installing corresponding tester respectively on the bottom of governor motion and top.Due to spherical support bar certainly
Protrude out and inside adjusting set, and can rotate, can so bear very big pulling force, it is excessive broken without having to worry about unmanned plane pulling force
Bad test device, it is highly reliable, it is rational in infrastructure.The position of support column can be changed by damping due to rotation adjusting knob, to change
The frictional resistance of support column and spherical support bar, so as to adapt to the test of different flight environment of vehicle；Can be with by reclining lock knob
The angle of inclination of locked spherical support bar, ensure that unmanned plane can only do horizontal revolving motion, adjustability is strong, is easy to simulate a variety of true
Real flight environment of vehicle and flight attitude.
In one of the embodiments, the support column is provided with deep-slotted chip breaker, regulating tank and holding groove, the deep-slotted chip breaker position
Being abutted in the top of the support column with the spherical support bar, the regulating tank is oppositely arranged with the damping adjusting knob,
The holding groove accepts the base.
In one of the embodiments, there is inclined plane, the inclined plane and the damping regulation rotation on the regulating tank
Button abuts.
In one of the embodiments, the regulation that the spherical support bar includes ball-type portion, protruded out from the ball-type portion
Portion and supporting part, the adjustment portion are abutted with the deep-slotted chip breaker, and the supporting part is connected with the supporting mechanism.
In one of the embodiments, socket passage is provided with inside the adjusting set, the socket passage is close to the branch
The bore of support mechanism is less than the diameter in the ball-type portion.
In one of the embodiments, the first receiving hole and the second receiving hole are offered in the adjusting set, described first
Receiving hole is adapted to the damping adjusting knob, second receiving hole and the angle locking knob fit.
In one of the embodiments, the supporting mechanism includes installing plate, the installation being connected with the spherical support bar
In the pinboard on the installing plate, some undertaking posts being installed on the pinboard, it is installed on holding on the undertaking post
Fishplate bar.
In one of the embodiments, the bearing plate is provided with some mounting holes.
In one of the embodiments, the support includes drum portion, the connecting rod being installed in the drum portion.
In one of the embodiments, the support also includes fastener, the fastener respectively with the drum portion and
Connecting rod connects.
Brief description of the drawings
Fig. 1 is the schematic diagram of the disconnected oar test device of a preferred embodiment of the present invention unmanned plane；
Fig. 2 is the partial schematic diagram in the disconnected oar test device of unmanned plane shown in Fig. 1；
Fig. 3 is the sectional view of the partial schematic diagram in the disconnected oar test device of unmanned plane shown in Fig. 2；
Fig. 4 is another sectional view of the partial schematic diagram in the disconnected oar test device of unmanned plane shown in Fig. 2；
Fig. 5 is the schematic diagram of support column in the disconnected oar test device of unmanned plane shown in Fig. 1；
Fig. 6 is the schematic diagram of adjusting set in the disconnected oar test device of unmanned plane shown in Fig. 1；
Fig. 7 is the schematic diagram at another visual angle of adjusting set shown in Fig. 6；
Fig. 8 is the schematic diagram of spherical support bar in the disconnected oar test device of unmanned plane shown in Fig. 1；
Accompanying drawing marks explanation：
The disconnected oar test device of 10- unmanned planes, 20- supports, 21- drum portion, 22- connecting rods, 23- fasteners, 30- regulation machines
Structure, 31- bases, 32- support columns, 33- adjusting sets, 34- spherical support bars, 35- damping adjusting knobs, 36- reclining lock knobs,
37- limited screws, 321- deep-slotted chip breakers, 322- regulating tanks, 323- holding grooves, 324- inclined planes, 331- socket passages, 332- first
Receiving hole, the receiving holes of 333- second, the receiving holes of 334- the 3rd, 341- ball-types portion, 342- adjustment portions, 343- supporting parts, 40- supports
Mechanism, 41- installing plates, 42- pinboards, 43- accept post, 44- bearing plates, 45- mounting holes.
Embodiment
For the ease of understanding the present invention, the present invention is described more fully below with reference to relevant drawings.In accompanying drawing
Give presently preferred embodiments of the present invention.But the present invention can realize in many different forms, however it is not limited to this paper institutes
The embodiment of description.On the contrary, the purpose for providing these embodiments is to make the understanding to the disclosure more thorough
Comprehensively.
It should be noted that when element is referred to as " being fixed on " another element, it can be directly on another element
Or there may also be element placed in the middle.When an element is considered as " connection " another element, it can be directly connected to
To another element or it may be simultaneously present centering elements.
Unless otherwise defined, all of technologies and scientific terms used here by the article is with belonging to technical field of the invention
The implication that technical staff is generally understood that is identical.Term used in the description of the invention herein is intended merely to description tool
The purpose of the embodiment of body, it is not intended that in the limitation present invention.
Fig. 1 to Fig. 8 is refer to, is the disconnected oar test device 10 of unmanned plane of a preferred embodiment of the present invention, the unmanned plane breaks
Oar test device 10 includes support 20, the governor motion 30 being installed on support 20, the supporting mechanism being connected with governor motion 30
40, in use, installing corresponding tester respectively on the bottom of governor motion 30 and top, tester detects unmanned plane in difference
Data under flight progress.
Reference picture 1, the support 20 include drum portion 21, the connecting rod 22 being installed in drum portion 21 and fastener 23,
Fastener 23 is connected with drum portion 21 and connecting rod 22 respectively, ensures that connecting rod 22 will not tilt.In use, drum portion 21
Both ends can bleed off pressure some weights to improve the support strength of support 20, ensure test be normally carried out.
Reference picture 2 base 31 that the governor motion 30 includes being installed in connecting rod 21, is installed on base 31 to Fig. 8
On support column 32, be placed on support column 32 adjusting set 33, protrude out and rotatable spherical support inside self-regulation set 33
Bar 34, the damping adjusting knob 35 being installed in adjusting set 33, reclining lock knob 36 and limited screw 37.Its center base 31 exists
Tester is put during test, one end of spherical support bar 34 abuts with support column 32, the other end of spherical support bar 34 and support
Mechanism 40 connects, and damping adjusting knob 35 is horizontally through adjusting set 33 and abutted with support column 32, and reclining lock knob 36 is laterally worn
Overregulate set 33 to abut with spherical support bar 34, limited screw 37 is horizontally through adjusting set 33 and abutted with support column 32.
Further, the support column 32 is provided with deep-slotted chip breaker 321, regulating tank 322 and holding groove 323, deep-slotted chip breaker 321
Abutted in the top of support column 32 with spherical support bar 34, regulating tank 322 is oppositely arranged to form regulation with damping adjusting knob 35
Space, holding groove 323 accept base 31.There is inclined plane 324, inclined plane 324 is supported with damping adjusting knob 35 on regulating tank 322
Connect, the inclination angle of specific inclined plane 324 is 45 degree, and the inclination angle of the touch surface at the touching end of damping adjusting knob 35 is also 45
It degree, can move support column 32 by damping the shake-up extruding of adjusting knob 35.
The inside of adjusting set 33 is provided with socket passage 331, and socket passage 331 is used to house support column 32 and spherical support
Bar 34, support column 32, spherical support bar 34 can move in socket passage 331.The first receiving hole is offered in adjusting set 33
332nd, the second receiving hole 333 and the 3rd receiving hole 334, the first receiving hole 332 is adapted to damping adjusting knob 35 is easy to damping to adjust
The regulation of knob 35 is saved to rotate, the second receiving hole 333 is adapted to angle locking knob 36 is easy to the regulation of angle locking knob 36 to rotate,
3rd receiving hole 334 is adapted to limited screw 37 is easy to the regulation of limited screw 37 to rotate.
The spherical support bar 34 includes ball-type portion 341, the adjustment portion 342 protruded out from ball-type portion 341 and supporting part
343, adjustment portion 342 abuts with deep-slotted chip breaker 321, and supporting part 343 is connected with supporting mechanism 40 and is used to install test in test
Instrument.Wherein the diameter in ball-type portion 341 is more than bore of the socket passage 331 close to supporting mechanism 40, and spherical support bar 34 will not be from
Come off, abutted from below by the deep-slotted chip breaker 321 of support column 32 in conjunction with adjustment portion 342, frictional force can uniformly divide in adjusting set 33
Cloth.Spherical support bar 34 forms similar spherical pan head structure, Ke Yishi by damping adjusting knob 35 and angle locking knob 36
Existing horizontal 360-degree rotation, each 45 degree of inclinations in left and right.
The supporting mechanism 40 includes the installing plate 41 being connected with spherical support bar 34, the switching being installed on installing plate 41
Plate 42, some undertaking posts 43 being installed on pinboard 42, the bearing plate 44 accepted on post 43 is installed on, bearing plate 44 is provided with
Some mounting holes 45, unmanned plane can be fixed by mounting hole 45.Unmanned plane can pass through when carrying out disconnected oar test
Control the running status of propeller to simulate disconnected oar situation, when one of propeller other propeller rotationals when rotating
Equivalent to the running status of a disconnected oar, disconnected two oars are equivalent to during other propeller rotationals when two of which propeller does not rotate
Running status.
Above-mentioned unmanned plane breaks oar test device 10, including support 20, be installed on support 20 governor motion 30, with regulation
The supporting mechanism 40 that mechanism 30 connects, in use, installing corresponding tester respectively on the bottom of governor motion 30 and top.By
Protrude out inside the self-regulation of spherical support bar 34 set 33, and can rotate, very big pulling force can be so born, without load
Heart unmanned plane pulling force crosses havoc test device, highly reliable, rational in infrastructure.It can be changed by damping due to rotation adjusting knob 35
The position of support column 32, to change the frictional resistance of support column 32 and spherical support bar 34, so as to adapt to different flight environment of vehicle
Test；It can ensure that unmanned plane can only do horizontal rotation with the angle of inclination of locked spherical support bar 34 by reclining lock knob 36
Transhipment is dynamic, and adjustability is strong, is easy to simulate a variety of real flight environment of vehicle and flight attitude.
Each technical characteristic of embodiment described above can be combined arbitrarily, to make description succinct, not to above-mentioned reality
Apply all possible combination of each technical characteristic in example to be all described, as long as however, the combination of these technical characteristics is not deposited
In contradiction, the scope that this specification is recorded all is considered to be.
Embodiment described above only expresses the several embodiments of the present invention, and its description is more specific and detailed, but simultaneously
Can not therefore it be construed as limiting the scope of the patent.It should be pointed out that come for one of ordinary skill in the art
Say, without departing from the inventive concept of the premise, various modifications and improvements can be made, these belong to the protection of the present invention
Scope.Therefore, the protection domain of patent of the present invention should be determined by the appended claims.
Claims (10)
- The oar test device 1. a kind of unmanned plane breaks, it is characterised in that including：Support, the governor motion being installed on the support, The supporting mechanism being connected with the governor motion；The governor motion include be installed on the support base, be installed on institute The support column on base, the adjusting set being placed on the support column are stated, is protruded out from inside the adjusting set and rotatable ball Shape support bar, the damping adjusting knob being installed in the adjusting set and reclining lock knob, one end of the spherical support bar Abutted with the support column, the other end of the spherical support bar is connected with the supporting mechanism, and the damping adjusting knob is horizontal Abutted to through the adjusting set with the support column, the reclining lock knob be horizontally through the adjusting set with it is described spherical Support bar abuts.
- The oar test device 2. unmanned plane according to claim 1 breaks, it is characterised in that the support column is provided with arc Groove, regulating tank and holding groove, the top that the deep-slotted chip breaker is located at the support column abut with the spherical support bar, the regulation Groove is oppositely arranged with the damping adjusting knob, and the holding groove accepts the base.
- The oar test device 3. unmanned plane according to claim 2 breaks, it is characterised in that have on the regulating tank and tilt Face, the inclined plane abut with the damping adjusting knob.
- The oar test device 4. unmanned plane according to claim 2 breaks, it is characterised in that the spherical support bar includes ball-type Portion, the adjustment portion protruded out from the ball-type portion and supporting part, the adjustment portion abut with the deep-slotted chip breaker, the supporting part with The supporting mechanism connection.
- The oar test device 5. unmanned plane according to claim 4 breaks, it is characterised in that socket is provided with inside the adjusting set Passage, the socket passage are less than the diameter in the ball-type portion close to the bore of the supporting mechanism.
- The oar test device 6. unmanned plane according to claim 5 breaks, it is characterised in that offer first in the adjusting set Receiving hole and the second receiving hole, first receiving hole with it is described damping adjusting knob be adapted to, second receiving hole with it is described Angle locking knob fit.
- The oar test device 7. unmanned plane according to claim 1 breaks, it is characterised in that the supporting mechanism include with it is described The installing plate of spherical support bar connection, the pinboard being installed on the installing plate, some holding of being installed on the pinboard Connect post, the bearing plate being installed on the undertaking post.
- The oar test device 8. unmanned plane according to claim 7 breaks, it is characterised in that the bearing plate is provided with some peaces Fill hole.
- The oar test device 9. unmanned plane according to claim 1 breaks, it is characterised in that the support includes drum portion, peace Loaded on the connecting rod in the drum portion.
- The oar test device 10. unmanned plane according to claim 9 breaks, it is characterised in that the support also includes fastener, The fastener is connected with the drum portion and connecting rod respectively.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711130198.5A CN107839897A (en) | 2017-11-15 | 2017-11-15 | The disconnected oar test device of unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711130198.5A CN107839897A (en) | 2017-11-15 | 2017-11-15 | The disconnected oar test device of unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107839897A true CN107839897A (en) | 2018-03-27 |
Family
ID=61679506
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711130198.5A Pending CN107839897A (en) | 2017-11-15 | 2017-11-15 | The disconnected oar test device of unmanned plane |
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| CN (1) | CN107839897A (en) |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6352228B1 (en) * | 1998-08-29 | 2002-03-05 | FLM GmbH Foto-, Licht-und Messtechnisches Zubehör | Tripod head |
| CN202120022U (en) * | 2011-03-14 | 2012-01-18 | 中山市思锐摄影器材工业有限公司 | Photography monopod locking device |
| CN202205016U (en) * | 2011-07-12 | 2012-04-25 | 阙忠伟 | Holder component for tripod of video camera |
| CN105620788A (en) * | 2016-01-26 | 2016-06-01 | 上海圣尧智能科技有限公司 | Universal platform and unmanned aerial vehicle test system |
| JP2016188770A (en) * | 2015-03-30 | 2016-11-04 | 大分県 | Propeller characteristics measuring apparatus |
| CN106114903A (en) * | 2016-07-23 | 2016-11-16 | 广东容祺智能科技有限公司 | A kind of VUAV flight attitude test platform |
| CN106347704A (en) * | 2016-09-06 | 2017-01-25 | 深圳电航空技术有限公司 | Flight control testing device |
| CN206419632U (en) * | 2016-12-30 | 2017-08-18 | 深圳市众杰影视器材有限公司 | A kind of Universal active ball-shaped cloud platform with bearing positioning and locking function |
| CN207791192U (en) * | 2017-11-15 | 2018-08-31 | 深圳市科比特航空科技有限公司 | The disconnected paddle test device of unmanned plane |
-
2017
- 2017-11-15 CN CN201711130198.5A patent/CN107839897A/en active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6352228B1 (en) * | 1998-08-29 | 2002-03-05 | FLM GmbH Foto-, Licht-und Messtechnisches Zubehör | Tripod head |
| CN202120022U (en) * | 2011-03-14 | 2012-01-18 | 中山市思锐摄影器材工业有限公司 | Photography monopod locking device |
| CN202205016U (en) * | 2011-07-12 | 2012-04-25 | 阙忠伟 | Holder component for tripod of video camera |
| JP2016188770A (en) * | 2015-03-30 | 2016-11-04 | 大分県 | Propeller characteristics measuring apparatus |
| CN105620788A (en) * | 2016-01-26 | 2016-06-01 | 上海圣尧智能科技有限公司 | Universal platform and unmanned aerial vehicle test system |
| CN106114903A (en) * | 2016-07-23 | 2016-11-16 | 广东容祺智能科技有限公司 | A kind of VUAV flight attitude test platform |
| CN106347704A (en) * | 2016-09-06 | 2017-01-25 | 深圳电航空技术有限公司 | Flight control testing device |
| CN206419632U (en) * | 2016-12-30 | 2017-08-18 | 深圳市众杰影视器材有限公司 | A kind of Universal active ball-shaped cloud platform with bearing positioning and locking function |
| CN207791192U (en) * | 2017-11-15 | 2018-08-31 | 深圳市科比特航空科技有限公司 | The disconnected paddle test device of unmanned plane |
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