CN206265338U - A kind of multi-rotor unmanned aerial vehicle test and training unified platform - Google Patents
A kind of multi-rotor unmanned aerial vehicle test and training unified platform Download PDFInfo
- Publication number
- CN206265338U CN206265338U CN201621264904.6U CN201621264904U CN206265338U CN 206265338 U CN206265338 U CN 206265338U CN 201621264904 U CN201621264904 U CN 201621264904U CN 206265338 U CN206265338 U CN 206265338U
- Authority
- CN
- China
- Prior art keywords
- aerial vehicle
- unmanned aerial
- rotor unmanned
- aircraft
- connecting rod
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Withdrawn - After Issue
Links
Landscapes
- Toys (AREA)
Abstract
The utility model discloses a kind of test of multi-rotor unmanned aerial vehicle and training unified platform, including aircraft and test box, several vertical support bars are provided with below aircraft fuselage, the top center of test box offers a circular open, activity is equipped with a connecting rod on circular open, connecting rod is connected by a universal joint with fuselage, a dismountable mode conversion plate coordinated with circular open is provided with the middle part of connecting rod, the limiting plate greater diameter than circular open is fixedly installed below connecting rod, mode conversion plate is arranged on outside test box, limiting plate is arranged in test box.A kind of multi-rotor unmanned aerial vehicle test of the utility model and training unified platform, by the release and fixation of mode conversion plate, allow hand over different mode, complete the test to multi-rotor unmanned aerial vehicle or the training to operating personnel.In addition, aircraft limits the angle of inclination of aircraft by the mode conversion plate and limiting plate in connecting rod, aircraft is effectively protected.
Description
Technical field
The utility model is related to unmanned air vehicle technique field, more particularly to a kind of test of multi-rotor unmanned aerial vehicle and training integration
Platform.
Background technology
With unmanned air vehicle technique continue to develop and multi-rotor unmanned aerial vehicle in recent years extensive use, market to many rotors without
The demand of the human-machine operation talent constantly expands.When multi-rotor unmanned aerial vehicle is in high-altitude flight, by complicated built-in system and outer
Portion's ambient influnence, sometimes in state out of control, once there is operational error, nearly ten thousand yuan even unmanned plane of hundreds of thousands unit are just
This scraps.Operating personnel should be clear how to avoid air crash before as a veteran flight operation person, first.One
Since straight, the training of multi-rotor unmanned aerial vehicle operating personnel start all be since flight simulator, then to small-sized many rotors nobody
Machine, is finally directly trained using nobody of multi-functional heavy load.But multi-rotor unmanned aerial vehicle operating personnel are ripe to energy from introduction
White silk operates with multi-rotor unmanned aerial vehicle, during to pass through a large amount of damages caused due to error, progressively accumulate experience, ability
Make operating personnel skillfully, therefore, the cost for carrying out flight training using existing training platform is very high.
Multi-rotor unmanned aerial vehicle system is mainly made up of dynamical system and flight control system two major parts, in practical operation this two
The stability of block system determines the reliability of whole unmanned plane.At present, system reliability is being carried out to multi-rotor unmanned aerial vehicle system
Property test and debug when, mainly tested and debugged using easy cable traction or other easy fixed forms, it is difficult to
The actual conditions of true reflection multi-rotor unmanned aerial vehicle system, the fault rate of system is higher when this may result in actually used, often
Cause to fall machine.
Utility model content
In order to overcome the above-mentioned deficiencies of the prior art, the utility model provides a kind of multi-rotor unmanned aerial vehicle and tests and train
Unified platform, can complete the test and training to multi-rotor unmanned aerial vehicle, low more reliable with test data with spoilage
Advantage.
The utility model solve technical scheme that its technical problem used for：A kind of multi-rotor unmanned aerial vehicle test and training
Unified platform, including aircraft and test box, the aircraft include fuselage and some propellers, the lower section side of the fuselage
Edge is evenly arranged with several vertical support bars, and the support bar is fixedly connected with fuselage, the top center of the test box
A circular open is offered, activity is equipped with a connecting rod on the circular open, and the connecting rod passes through a universal joint
It is connected with fuselage, a mode conversion plate coordinated with circular open, the mode conversion plate is provided with the middle part of the connecting rod
It is detachably combined to the top of test box, be fixedly installed greater diameter than the spacing of circular open below the connecting rod
Plate, the mode conversion plate is arranged on outside test box, and the limiting plate is arranged in test box.
Further, the mode conversion plate is arranged on the top of test box by screw.
Further, be further fixedly arranged on below the test box one for load Different Weight load counter-balanced carriage.
Further, it is provided with for mobile wheel below the counter-balanced carriage.
Further, the aircraft also includes power supply, motor, electron speed regulator and flight control system, and the propeller passes through
Motor drives, and the power supply is used to provide electric energy for motor and electron speed regulator, and the electron speed regulator is connected and controls with motor
The rotation of motor processed, the flight control system is connected with aircraft and controls flying up, turn to, accelerate, slow down and shutting down for aircraft
Action.
Further, the power supply uses battery or D.C. regulated power supply.
Further, the flight control system is connected by wired or wireless mode with aircraft.
Further, switch, testing current unit, voltage tester unit, tensile test unit are provided with the test box
And instrument board, the testing current unit and voltage tester unit be connected with electron speed regulator respectively, the tensile test unit
It is connected with connecting rod, the instrument board is used to show the test data of electric current, voltage and pulling force.
Further, a limit casing is fixedly installed at the circular open, the limit casing is arranged in test box
Portion, the connecting rod is set in limit casing, and the mode conversion plate is arranged on the upper end outside of limit casing, described spacing
Plate is arranged on the lower end outside of limit casing.
Further, the support bar is provided with 6.
The beneficial effects of the utility model have：A kind of multi-rotor unmanned aerial vehicle test of the utility model and training integration are flat
Platform, by the release and fixation of mode conversion plate, allows hand over different mode, completes to the test of multi-rotor unmanned aerial vehicle or to behaviour
Make the training of personnel.In addition, aircraft limits the inclination angle of aircraft by the mode conversion plate and limiting plate in connecting rod
Degree, prevents aircraft over-tilting, effectively protects aircraft.
Brief description of the drawings
Below in conjunction with the accompanying drawings and specific embodiment the utility model is described in further detail, wherein：
Fig. 1 is the structural representation of the utility model test and training unified platform；
Fig. 2 is the structural representation of the utility model connecting rod and universal joint.
Specific embodiment
Referring to Fig. 1, Fig. 1 is the structural representation of the utility model test and training unified platform.The utility model one
Plant multi-rotor unmanned aerial vehicle test and training unified platform, including aircraft 1, test box 2 and counter-balanced carriage 3.
Aircraft 1 includes fuselage 11 and some propellers 12, and the balance of propeller 12 is arranged on around fuselage 11, specifically,
Propeller 12 is provided with 6.Aircraft 1 also includes power supply, motor, electron speed regulator and flight control system, and the propeller 12 leads to
Motor driving is crossed, the power supply is used to provide electric energy for motor and electron speed regulator, and the electron speed regulator is connected simultaneously with motor
The rotation of controlled motor, the flight control system is connected by wired or wireless mode aircraft 1.Motor is according to different power
Corresponding propeller 12 is configured, motor is connected with electron speed regulator, using on battery or D.C. regulated power supply connection aircraft 1
Electron speed regulator, the signal receiver of flight control system is connected with the reinforcing holding wire of electron speed regulator, by flight control system control
Aircraft 1 such as flies up, turns to, accelerates, slows down and shuts down at the action.It is vertical that the lower edge of fuselage 11 is evenly arranged with several
Support bar 13, the support bar 13 is fixedly connected with fuselage 11, when being trained, aircraft 1 drive support bar 13 leave
The top of test box 2；When training terminates or tested, aircraft 1 rests on the upper of test box 2 by support bar 13
Side.Specifically, the support bar 13 is provided with 6, and the effect of support bar 13 is to support aircraft 1.
The hollow casing of test box 2 substantially, is internally provided with testing current unit, voltage tester unit and pulling force
Test cell, outside is provided with switch and instrument board, and switch is used for controlling the on/off of test box, the testing current unit
It is connected with electron speed regulator respectively with voltage tester unit, the tensile test unit is connected with connecting rod 14, the instrument board
For showing electric current, voltage and the test data of pulling force, various data are shown in real time in test or training.Test box 2
Top is a level board, and the center of level board offers a circular open, and activity is equipped with a connecting rod 14 on circular open.Ginseng
See that Fig. 2, Fig. 2 are the structural representations of the utility model connecting rod 14 and universal joint 15.Connecting rod 14 passes through a universal company
Joint 15 is connected with the fuselage 11 of aircraft 1, and the middle part of connecting rod 14 is provided with a mode conversion plate coordinated with circular open
16, the mode conversion plate 16 is detachably combined to the top of test box 2, and the lower section of the connecting rod 14 is fixedly installed always
Footpath is more than the limiting plate 17 of circular open, and the mode conversion plate 16 is arranged on outside test box 2, and the limiting plate 17 is arranged on survey
In examination case 2.When being tested, mode conversion plate 16 is fixed on the top of test box 2, now aircraft 1 can only be vertical
Power is provided on direction, it is impossible to turn to；Mode conversion plate 16 is then unclamped when being trained, now aircraft 1 is in vertical and water
Square can all provide power upwards.The limiting plate 17 greater diameter than circular open is fixedly installed below connecting rod 14, is limited
Position plate 17 can limit the angle of inclination of aircraft 1, as long as the actual conditions according to aircraft 1 set the appropriate length of connecting rod 14
Degree, it is possible to after largely ensureing to unclamp mode conversion plate 16, aircraft 1 still will not over-tilting, so as to prevent spiral shell
Rotation oar 12 lands or damages.
The lower section of test box 2 be further fixedly arranged on one for load Different Weight load counter-balanced carriage 3, the counter-balanced carriage
3 lower section is provided with for mobile wheel 31.Need to increase load on aircraft 1 in test, installed on counter-balanced carriage 3
Balancing weight, one can reach the loaded purpose of increasing, and two can reduce the overall center of gravity of platform, platform is more consolidated.
In addition, if aircraft 1 uses battery power, battery can also be on counter-balanced carriage 3.
Used as preferred embodiments of the present utility model, the mode conversion plate 16 is arranged on test box 2 by screw
Top.In conversion testing or training mode, it is necessary to mode conversion plate 16 is fixed or unclamped, by key screw mode conversion
Plate 16 is arranged on the top of test box 2, has the advantages that simple structure and easy to loading and unloading.
Further, a limit casing, institute are fixedly installed as preferred embodiments of the present utility model, at circular open
State limit casing to be arranged on inside test box 2, the connecting rod 14 is set in limit casing, the mode conversion plate 16 is set
In the outside of limit casing upper end, the limiting plate 17 is arranged on the outside of limit casing lower end.The setting of limit casing, can be with
The over-tilting of aircraft 1 is further prevented, protecting effect is more preferable.
It is noted that no matter in test or when training, aircraft 1 is all without leaving ground.Flown during test
Device 1 can provide the pulling force of different numerical value, and test box 2 tests various data during different pulling force；The tested training of aircraft 1 during training
The constraint of converter plate and limiting plate 17, can only small range motion, ground can't be left, this to protection aircraft 1 it is without damage
There is great significance.In test, it is only necessary to which the data such as collected current, voltage and pulling force just can truly reflect multi-rotor unmanned aerial vehicle system
The actual conditions of system, it is not necessary to which aircraft 1 leaves ground；And for primary operation personnel, the small range motion of aircraft 1
Also it can be helped deeper into the structure and performance that understand aircraft 1, extraordinary training effect can be also brought without leaving ground.
A kind of multi-rotor unmanned aerial vehicle test of the utility model and training unified platform are a multiduty equipment, can
The training of the test and operating personnel to multi-rotor unmanned aerial vehicle is completed as needed, and its advantage is：1. effectively to many rotors without
It is man-machine to carry out reliability testing, and prolonged test flight can be done.2. display unmanned plane directly perceived under floating state electric current,
The real time values such as voltage, pulling force, motor speed.3. the dynamical system for being convenient for changing each specification is tested, and is adapted in thrust amount
Journey 0-100KG, current range 0-300A, the various multi-rotor unmanned aerial vehicle of voltage range 0-600V are used.4. easy to use, can make
Baseless primary operation personnel quickly grasp the structural principle and manipulation skill of multi-rotor aerocraft 1.
The above, simply better embodiment of the present utility model, but the utility model is not limited to above-mentioned reality
Example is applied, as long as it reaches technique effect of the present utility model with any same or similar means, should all belong to of the present utility model
Protection domain.
Claims (10)
1. a kind of multi-rotor unmanned aerial vehicle is tested and training unified platform, it is characterised in that：Including aircraft（1）And test box
（2）, the aircraft（1）Including fuselage（11）With some propellers（12）, the fuselage（11）Lower edge be uniformly arranged
There are several vertical support bars（13）, the support bar（13）With fuselage（11）It is fixedly connected, the test box（2）Top
Center offers a circular open, and activity is equipped with a connecting rod on the circular open（14）, the connecting rod（14）Pass through
One universal joint（15）With fuselage（11）It is connected, the connecting rod（14）Middle part be provided with one with circular open coordinate mould
Formula converter plate（16）, the mode conversion plate（16）It is detachably combined to test box（2）Top, the connecting rod（14）Under
Side is fixedly installed the limiting plate greater diameter than circular open（17）, the mode conversion plate（16）It is arranged on test box（2）
Outward, the limiting plate（17）It is arranged on test box（2）It is interior.
2. a kind of multi-rotor unmanned aerial vehicle according to claim 1 is tested and training unified platform, it is characterised in that：It is described
Mode conversion plate（16）Test box is arranged on by screw（2）Top.
3. a kind of multi-rotor unmanned aerial vehicle according to claim 1 is tested and training unified platform, it is characterised in that：It is described
Test box（2）Lower section be further fixedly arranged on one for load Different Weight load counter-balanced carriage（3）.
4. a kind of multi-rotor unmanned aerial vehicle according to claim 3 is tested and training unified platform, it is characterised in that：It is described
Counter-balanced carriage（3）Lower section be provided with for mobile wheel（31）.
5. a kind of multi-rotor unmanned aerial vehicle according to claim 1 is tested and training unified platform, it is characterised in that：It is described
Aircraft（1）Also include power supply, motor, electron speed regulator and flight control system, the propeller（12）Driven by motor, it is described
Power supply is used to provide electric energy for motor and electron speed regulator, and the electron speed regulator is connected the rotation of simultaneously controlled motor with motor,
The flight control system and aircraft（1）It is connected and controls aircraft（1）Fly up, turn to, accelerating, slowing down and shutdown action.
6. a kind of multi-rotor unmanned aerial vehicle according to claim 5 is tested and training unified platform, it is characterised in that：It is described
Power supply uses battery or D.C. regulated power supply.
7. a kind of multi-rotor unmanned aerial vehicle according to claim 5 is tested and training unified platform, it is characterised in that：It is described
Flight control system is by wired or wireless mode and aircraft（1）It is connected.
8. a kind of multi-rotor unmanned aerial vehicle according to claim 5 is tested and training unified platform, it is characterised in that：It is described
Test box（2）On be provided with switch, testing current unit, voltage tester unit, tensile test unit and instrument board, the electric current
Test cell and voltage tester unit are connected with electron speed regulator respectively, the tensile test unit and connecting rod（14）It is connected,
The instrument board is used to show the test data of electric current, voltage and pulling force.
9. a kind of multi-rotor unmanned aerial vehicle according to claim 1 is tested and training unified platform, it is characterised in that：It is described
A limit casing is fixedly installed at circular open, the limit casing is arranged on test box（2）Inside, the connecting rod（14）
It is set in limit casing, the mode conversion plate（16）It is arranged on the upper end outside of limit casing, the limiting plate（17）If
Put outside the lower end of limit casing.
10. a kind of multi-rotor unmanned aerial vehicle according to claim 1 is tested and training unified platform, it is characterised in that：Institute
State support bar（13）It is provided with 6.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621264904.6U CN206265338U (en) | 2016-11-22 | 2016-11-22 | A kind of multi-rotor unmanned aerial vehicle test and training unified platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621264904.6U CN206265338U (en) | 2016-11-22 | 2016-11-22 | A kind of multi-rotor unmanned aerial vehicle test and training unified platform |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206265338U true CN206265338U (en) | 2017-06-20 |
Family
ID=59041100
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621264904.6U Withdrawn - After Issue CN206265338U (en) | 2016-11-22 | 2016-11-22 | A kind of multi-rotor unmanned aerial vehicle test and training unified platform |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206265338U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106494640A (en) * | 2016-11-22 | 2017-03-15 | 珠海市双捷科技有限公司 | A kind of multi-rotor unmanned aerial vehicle test and training unified platform |
| CN109850117A (en) * | 2018-12-05 | 2019-06-07 | 中国航空工业集团公司成都飞机设计研究所 | A kind of multi-rotor aerocraft with walking function |
-
2016
- 2016-11-22 CN CN201621264904.6U patent/CN206265338U/en not_active Withdrawn - After Issue
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106494640A (en) * | 2016-11-22 | 2017-03-15 | 珠海市双捷科技有限公司 | A kind of multi-rotor unmanned aerial vehicle test and training unified platform |
| CN109850117A (en) * | 2018-12-05 | 2019-06-07 | 中国航空工业集团公司成都飞机设计研究所 | A kind of multi-rotor aerocraft with walking function |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106494640B (en) | A kind of multi-rotor unmanned aerial vehicle test and trained unified platform | |
| US11358716B2 (en) | System and method for airborne wind energy production | |
| CN105547676B (en) | A kind of arm-type rotor model.test system of multifunctional rotary | |
| CN205098464U (en) | Rotor unmanned aerial vehicle of flexible function that lands of utensil | |
| ES2379708T5 (en) | Wind Turbine Test System | |
| CN107065915A (en) | A kind of six degree of freedom rotor craft on-line debugging platform | |
| CN206265338U (en) | A kind of multi-rotor unmanned aerial vehicle test and training unified platform | |
| CN107154194A (en) | For the manipulation in paratrooper's training simulators and dynamic emulation system | |
| CN102779438B (en) | Flight simulated mechanical execution system simulating full-motion of airplane | |
| CN207191432U (en) | Rescue four rotor wing unmanned aerial vehicles in a kind of public security waters | |
| CN103318406A (en) | Composite rotor craft | |
| Raz et al. | Wind tunnel and flight evaluation of passive stabilization of a cargo container slung load | |
| CN109163874A (en) | The self-walking fan battle array that can be freely combined | |
| CN107272749A (en) | For rotary-wing flight test and the test platform and method of proof of algorithm | |
| CN106769138A (en) | Idiocratically Orly drags simulation test device and method to a kind of static balance of captive balloon Limit of Wind Speed | |
| CN104174166B (en) | Portable vertical recreation wind tunnel | |
| CN206427269U (en) | It is a kind of based on multi-rotor aerocraft can manned aerial work platform | |
| CN206384639U (en) | Unwrapping wire unmanned plane | |
| CN112109890A (en) | A folding oar presss from both sides drive assembly for unmanned aerial vehicle | |
| CN215643306U (en) | Screw negative tension demonstration device | |
| CN206437236U (en) | A kind of many rotary wind type vertical take-off and landing flying car laboratory vehicles | |
| CN106596030B (en) | A kind of full-scale helicopter tower | |
| CN205730366U (en) | A kind of wing horizontal tail full dynamic formula aircraft model plane | |
| CN107176294A (en) | A kind of overwater flight device | |
| CN211236129U (en) | Multifunctional unmanned aerial vehicle circuit test board |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20170620 Effective date of abandoning: 20181120 |
|
| AV01 | Patent right actively abandoned |