CN205837207U - A kind of whereabouts, high reliability aircraft high-altitude slow-descending system - Google Patents
A kind of whereabouts, high reliability aircraft high-altitude slow-descending system Download PDFInfo
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- CN205837207U CN205837207U CN201620790172.8U CN201620790172U CN205837207U CN 205837207 U CN205837207 U CN 205837207U CN 201620790172 U CN201620790172 U CN 201620790172U CN 205837207 U CN205837207 U CN 205837207U
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Abstract
The utility model discloses a kind of whereabouts, high reliability aircraft high-altitude slow-descending system, relate to unmanned plane apparatus field, including control unit, power drive module, motor, power module and slow descending device, described control unit respectively with power drive module, slow descending device and power module connect, described power drive module and motor connect, described it is also associated with wireless remote control transceiver module for control unit, this utility model can monitor the flight attitude of unmanned plane in real time, and contingent abnormal conditions are judged, and send slow fall order, make the unmanned plane can safe landing, guarantee the safety of unmanned plane.
Description
Technical field
This utility model relates to unmanned plane apparatus field, is specifically related to a kind of high reliability aircraft high-altitude and falls to delaying fall system
System.
Background technology
Unmanned plane (english abbreviation: Unmanned Aerial Vehicle) is a kind of with wireless remotecontrol or by self journey
Sequence controls to be the most manned main aircraft.Current aircraft slow-descending system has use servomechanism manual intervention to dish out parachute or make
By the technology that spring energy-storage launches, gunpowder fuel launches, the excessively complexity but its mechanism works, efficiency is on the low side, without the flight of intelligence
Real-time monitoring system for state, the umbrella rope discharged directly crashes easily occurring to be wound around with rotor the most at work, behaviour
Make to start crash rate higher.It addition, existing scheme versatility is the strongest, it is impossible to carry out seamless link use for multiple aircraft.
Utility model content
The purpose of this utility model is to provide a kind of whereabouts, high reliability aircraft high-altitude slow-descending system, existing to solve
The above-mentioned multinomial defect caused in technology.
A kind of whereabouts, high reliability aircraft high-altitude slow-descending system, mechanical, electrical including control unit, power drive module, electricity
Source module and slow descending device, described control unit is connected with power drive module, slow descending device and power module respectively, described dynamic
Power drives module and motor to connect, and described is also associated with wireless remote control transceiver module for control unit.
Preferably, described control unit is specially the flight control system of unmanned plane, including gyroscope, accelerometer,
Magnetic inductor, baroceptor, GPS module, microprocessor and control circuit, microprocessor respectively with gyroscope, accelerometer,
Earth inductor, baroceptor and GPS module connect, microprocessor by control circuit respectively with power drive module, slow
Falling unit and power module connect.
Preferably, described power module is rechargeable battery, and powers for whole system.
Preferably, described slow descending device includes parachute actuator and parachute, parachute actuator respectively with control
Unit processed and parachute connect.
The utility model has the advantage of:
1, flight sensor is monitored in real time is that flight state avoids maloperation to start slow-descending system；
2, state of flight computer control system stop in advance rotor work effectively prevent rotor and twining that umbrella rope occurs
Around；
3, independent electric power supply, even if unmanned plane does not has electricity, also ensures that the whole slow-descending system of support is run；
4, rolling protection: flight sensor once monitors aircraft fuselage aloft more than state of flight meter behind 90 ° of angles
The work of closedown rotor is automatically releasable out slow descending device by calculation machine control system；
5, simple in construction, compatible different types of machines are installed and used.
Accompanying drawing explanation
Fig. 1 is the theory diagram of whereabouts, a kind of high reliability aircraft high-altitude described in the utility model slow-descending system.
Detailed description of the invention
For the technological means making this utility model realize, creation characteristic, reach purpose and be easy to understand with effect, below
In conjunction with detailed description of the invention, this utility model is expanded on further.
As it is shown in figure 1, a kind of whereabouts, high reliability aircraft high-altitude slow-descending system, including control unit, power drive mould
Block, motor, power module and slow descending device, described control unit respectively with power drive module, slow descending device and power module
Connecting, described power drive module and motor connect, and described are also associated with wireless remote control transceiver module for control unit.
In the present embodiment, described control unit is specially the flight control system of unmanned plane, including gyroscope, acceleration
Meter, earth inductor, baroceptor, GPS module, microprocessor and control circuit, microprocessor respectively with gyroscope, acceleration
Degree meter, earth inductor, baroceptor and GPS module connect, microprocessor pass through control circuit respectively with power drive mould
Block, slow descending device and power module connect, and gyroscope, accelerometer, earth inductor, baroceptor and GPS module are constituted
The flight sensor part of native system.
In the present embodiment, described power module is rechargeable battery, and powers for whole system, described slow descending device bag
Including parachute actuator and parachute, parachute actuator is connected with control unit and parachute respectively.
This utility model has a set of state of flight computer control system, i.e. control unit, the gyro in control unit
The flight sensor such as instrument, accelerometer can monitor whether unmanned plane runs into emergency in flight course, the most freely falls
Body, rolling etc..Emergency once occurs, and the flight sensor of slow-descending system will be sent by wireless signal after monitoring
Sending prompting to remote controller and man-machine linkage interface, operator can open button and start slow-descending system, and state of flight calculates
It is that lotus-shaped flower is opened and discharged slow fall umbrella that machine control system will stop the rotor cabin of expandable type storage subsequently that works immediately.
Based on above-mentioned, it is that flight state avoids maloperation to start slow fall that flight sensor of the present utility model is monitored in real time
System；State of flight computer control system stops rotor work in advance and effectively prevent the winding that rotor occurs with umbrella rope；Solely
Vertical power-supply system, even if unmanned plane does not has electricity, also ensures that the whole slow-descending system of support is run；Rolling protection: flight sensing
Device once monitors aircraft fuselage aloft will close rotor work certainly more than state of flight computer control system behind 90 ° of angles
Move and discharge slow descending device；Simple in construction, compatible different types of machines are installed and used.
As known by the technical knowledge, this utility model can be by other essence without departing from its spirit or the reality of essential feature
The scheme of executing realizes.Therefore, embodiment disclosed above, for each side, all it is merely illustrative, is not only
's.All in the range of this utility model or be equal to the change in the range of this utility model all by this utility model bag
Contain.
Claims (4)
1. whereabouts, high reliability aircraft high-altitude slow-descending system, it is characterised in that include control unit, power drive mould
Block, motor, power module and slow descending device, described control unit respectively with power drive module, slow descending device and power module
Connecting, described power drive module and motor connect, and described control unit is also associated with wireless remote control transceiver module.
A kind of whereabouts, high reliability aircraft high-altitude the most according to claim 1 slow-descending system, it is characterised in that: described control
Unit processed is specially the flight control system of unmanned plane, including gyroscope, accelerometer, earth inductor, baroceptor,
GPS module, microprocessor and control circuit, microprocessor respectively with gyroscope, accelerometer, earth inductor, air pressure sensing
Device and GPS module connect, and microprocessor is by control circuit respectively with power drive module, slow descending device and power module even
Connect.
A kind of whereabouts, high reliability aircraft high-altitude the most according to claim 2 slow-descending system, it is characterised in that: described electricity
Source module is rechargeable battery, and powers for whole system.
A kind of whereabouts, high reliability aircraft high-altitude the most according to claim 1 slow-descending system, it is characterised in that: described slow
Falling unit includes that parachute actuator and parachute, parachute actuator are connected with control unit and parachute respectively.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620790172.8U CN205837207U (en) | 2016-07-23 | 2016-07-23 | A kind of whereabouts, high reliability aircraft high-altitude slow-descending system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620790172.8U CN205837207U (en) | 2016-07-23 | 2016-07-23 | A kind of whereabouts, high reliability aircraft high-altitude slow-descending system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205837207U true CN205837207U (en) | 2016-12-28 |
Family
ID=57626239
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
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| CN201620790172.8U Active CN205837207U (en) | 2016-07-23 | 2016-07-23 | A kind of whereabouts, high reliability aircraft high-altitude slow-descending system |
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| CN (1) | CN205837207U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109677621A (en) * | 2019-01-25 | 2019-04-26 | 广东翼景信息科技有限公司 | A kind of unmanned plane parachute and unmanned plane parachute control system |
| CN110979647A (en) * | 2019-12-24 | 2020-04-10 | 广东电网有限责任公司 | Air fault protection device and method suitable for multi-rotor unmanned aerial vehicle |
-
2016
- 2016-07-23 CN CN201620790172.8U patent/CN205837207U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109677621A (en) * | 2019-01-25 | 2019-04-26 | 广东翼景信息科技有限公司 | A kind of unmanned plane parachute and unmanned plane parachute control system |
| CN110979647A (en) * | 2019-12-24 | 2020-04-10 | 广东电网有限责任公司 | Air fault protection device and method suitable for multi-rotor unmanned aerial vehicle |
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|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |