CN106741879A - A kind of unmanned plane with protection device - Google Patents
A kind of unmanned plane with protection device Download PDFInfo
- Publication number
- CN106741879A CN106741879A CN201611129522.7A CN201611129522A CN106741879A CN 106741879 A CN106741879 A CN 106741879A CN 201611129522 A CN201611129522 A CN 201611129522A CN 106741879 A CN106741879 A CN 106741879A
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- protection device
- generating unit
- control module
- gas generating
- 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.)
- Pending
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
- B64C25/62—Spring shock-absorbers; Springs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/54—Floats
- B64C25/56—Floats inflatable
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
- B64C25/62—Spring shock-absorbers; Springs
- B64C25/64—Spring shock-absorbers; Springs using rubber or like elements
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Professional, Industrial, Or Sporting Protective Garments (AREA)
Abstract
A kind of unmanned plane with protection device, including foot support, body, remote control, the remote control include dispensing device, and the internal body is provided with reception device, the signal that the reception device transmission and reception apparatus send.The foot support is hollow-core construction; the internal stent sets protection device; the protection device includes air bag, gas generating unit, control module; the air bag, gas generating unit are arranged on inside foot support; the output end of the reception device is connected with the input of control module; the output end of the control module is connected with the input of gas generating unit, and the air sac sealing is arranged on the exit of gas generating unit.The unmanned plane can cause unmanned plane soft landing in normal operation, and unmanned plane can protect unmanned plane in the case of out of control.
Description
Technical field
The present invention relates to unmanned plane field, more particularly to a kind of unmanned plane with protection device.
Background technology
After unmanned plane during flying lands, foot support lands, but sometimes due to jump area out-of-flatness so that unmanned plane inclines
Ramp down ground and damage the wing of unmanned plane, when controlling bad to unmanned plane speed, foot support hard landing is also easily made to fuselage
Into damage.When unmanned plane is in the case of uncontrollable, and jump area be the water surface on when, accordingly even when being the unmanned plane of waterproof
Easy submerged and lose.
So being badly in need of a kind of new unmanned plane to solve the above problems.
The content of the invention
Technical problem to be solved of the invention is due to jump area out-of-flatness or to unmanned plane when unmanned plane lands
Have damage to the fuselage of unmanned plane when speed grasps bad, and be easily lost when unmanned plane is fallen into water, the present invention use with
Lower technical scheme solves above-mentioned technical problem：
A kind of unmanned plane with protection device, including foot support, body, remote control, the remote control include sending dress
Put, the internal body is provided with reception device, the signal that the reception device transmission and reception apparatus send, it is characterised in that
The foot support is hollow-core construction, and the internal stent sets protection device, and the protection device includes that air bag, gas are filled
Put, control module, the air bag, gas generating unit be arranged on inside foot support, output end and the control of the reception device
The input connection of module, the output end of the control module is connected with the input of gas generating unit, the air sac sealing
It is arranged on the exit of gas generating unit.
Optimization, the gas generating unit includes firing circuit, gas-forming agent, the firing circuit and control module
Output end connection.
Optimization, the foot support is 4, is set with the central axis circumference array of unmanned plane.
Optimization, the bottom after the airbag aeration at away from support is plane.
Optimization, described each internal stent is provided with protection device.
Optimization, the protection device also includes gyroscope, accelerometer, the gyroscope and accelerometer respectively with control mould
The input connection of block.
Optimization, the foot support lower end is cased with U-shaped elastomeric material.
The advantage of the invention is that：
(1) present invention sets protection device inside foot support, and after unmanned plane lands, remote control transmits a signal to control
Module, control module control gas generating unit, produces gas so as to control airbag aeration, soft when being realized after unmanned plane landing
Land.
(2) gas generating unit of the present invention includes firing circuit, control module control firing circuit, when unmanned plane is normal
When unmanned plane needs to open air bag under state, remote control dispensing device transmits a signal to the reception device inside unmanned plane, receives
Device is input a signal into control module, control module control firing circuit conducting, anti-so as to cause gas-forming agent to occur
Gas should be produced.Produce the mode of gas identical with the principle of the air bag of automobile.
(3) bottom of air bag is a plane in the present invention, bigger with landing point contact area so after opening,
When falling into water, the area of floating also increases.
(4) protection device also includes gyroscope, accelerometer in the present invention, when remote control can not control unmanned plane, nobody
When machine does the rolling under the movement of falling object, non-control state, control module control airbag-releasing, so as to produce certain floating
Power, it is to avoid unmanned plane is broken.
(5) foot support lower end is cased with U-shaped elastomeric material in the present invention, so in the case where air bag is not turned on
Certain cushioning effect can be played.When air bag is opened, elastomeric material reduces the frictional force of air bag and foot support edge, so as to protect
Shield air bag.
Brief description of the drawings
Fig. 1 is the structural representation of unmanned plane in the present invention.
Fig. 2 is the structural representation of foot support of the present invention.
Specific embodiment
As shown in Figure 1-2, a kind of unmanned plane with protection device, including foot support 3, body 1, remote control, remote control
Including dispensing device, body 1 is internally provided with reception device 2, the signal that the transmission and reception apparatus of reception device 2 send.Foot support 3
It is hollow-core construction, internal stent sets protection device, and protection device includes air bag 5, gas generating unit 7, control module 6, gas
Capsule 5, gas generating unit 7 are arranged on inside foot support 3, and the output end of reception device 2 is connected with the input of control module 6,
The output end of control module 6 is connected with the input of gas generating unit 7, and air bag 5 is sealingly disposed in going out for gas generating unit 7
At mouthful.
Gas generating unit 7 includes firing circuit, gas-forming agent, and firing circuit is connected with the output end of control module 6.
Control module 6 controls firing circuit, and when unmanned plane needs to open air bag 5 to unmanned plane in normal state, remote control sends dress
Put and transmit a signal to reception device 2 inside unmanned plane, reception device 2 is input a signal into control module 6, control module 6
Control firing circuit conducting, so as to cause gas-forming agent to react generation gas.Produce the mode of gas and the peace of automobile
The principle of full air bag 5 is identical.
Optimization, foot support 3 is 4, is set with the central axis circumference array of unmanned plane.Each internal stent is respectively provided with
There is protection device.So as to increase the number of air bag 5.So as to increase the contact area with air, because an area of air bag 5 is excessive
When, in the state of the non-handstand of unmanned plane, air bag 5 may upwards be floatd and touch the wing of unmanned plane, optimization, and air bag 5 is inflated
The bottom at away from support is plane afterwards.So it is also the contact area of increase and air.
After unmanned plane lands, remote control transmits a signal to control module 6, and control module 6 controls gas generating unit 7,
Gas is produced so as to control air bag 5 to inflate, soft landing is realized after unmanned plane lands.
Optimization, protection device also includes gyroscope, accelerometer, and gyroscope and accelerometer are defeated with control module 6 respectively
Enter end connection.So when unmanned plane is uncontrolled, gyroscope and accelerometer transmit a signal to control module 6, and control module 6 is controlled
Gas generating unit 7 produces gas and is filled with air bag 5, buoyancy is so increased in the air, so as to prevent unmanned plane freedom
The damage that falling bodies are caused.In unmanned plane falls into water, can also increase buoyancy, it is not easy to lose.
Optimization, the lower end of foot support 3 is cased with U-shaped elastomeric material 4.So also realized when unmanned plane is not turned on air bag 5
A certain degree of soft landing, when air bag 5 is opened, elastomeric material reduces the frictional force of air bag 5 and foot support 3 edge, so that
Protection air bag 5.
The preferred embodiment of the invention is these are only, creation is not intended to limit the invention, it is all in the present invention
Any modification, equivalent and improvement made within the spirit and principle of creation etc., should be included in the guarantor of the invention
Within the scope of shield.
Claims (7)
1. a kind of unmanned plane with protection device, including foot support, body, remote control, the remote control include dispensing device,
The internal body is provided with reception device, the signal that the reception device transmission and reception apparatus send, it is characterised in that described
Foot support is hollow-core construction, and the internal stent sets protection device, the protection device include air bag, gas generating unit,
Control module, the air bag, gas generating unit are arranged on inside foot support, the output end and control module of the reception device
Input connection, the output end of the control module is connected with the input of gas generating unit, the air sac sealing setting
In the exit of gas generating unit.
2. a kind of unmanned plane with protection device according to claim 1, it is characterised in that the gas generating unit
Including firing circuit, gas-forming agent, the firing circuit is connected with the output end of control module.
3. a kind of unmanned plane with protection device according to claim 1, it is characterised in that the foot support is 4,
Set with the central axis circumference array of unmanned plane.
4. a kind of unmanned plane with protection device according to claim 1, it is characterised in that after the airbag aeration
It is plane away from the bottom at support.
5. a kind of unmanned plane with protection device according to claim 1, it is characterised in that described each internal stent
It is provided with protection device.
6. a kind of unmanned plane with protection device according to claim 1, it is characterised in that the protection device is also wrapped
Gyroscope, accelerometer are included, the gyroscope and accelerometer are connected with the input of control module respectively.
7. a kind of unmanned plane with protection device according to claim 1, it is characterised in that the foot support lower end set
There is U-shaped elastomeric material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611129522.7A CN106741879A (en) | 2016-12-09 | 2016-12-09 | A kind of unmanned plane with protection device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611129522.7A CN106741879A (en) | 2016-12-09 | 2016-12-09 | A kind of unmanned plane with protection device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106741879A true CN106741879A (en) | 2017-05-31 |
Family
ID=58875647
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611129522.7A Pending CN106741879A (en) | 2016-12-09 | 2016-12-09 | A kind of unmanned plane with protection device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106741879A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108482690A (en) * | 2018-04-06 | 2018-09-04 | 丁奕森 | A kind of scalable comprehensive protective device of unmanned plane |
| CN111268103A (en) * | 2020-02-14 | 2020-06-12 | 广东工业大学 | Take dual-purpose unmanned aerial vehicle in sea and air of gasbag |
| CN111591436A (en) * | 2020-04-30 | 2020-08-28 | 南京理工大学 | Pneumatic soft landing gear of small unmanned aerial vehicle |
| CN111645871A (en) * | 2020-06-18 | 2020-09-11 | 湖北金色阳光创客教育有限公司 | Be used for unmanned aerial vehicle protector that falls |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20080315037A1 (en) * | 2005-12-23 | 2008-12-25 | Airbus Deutschland Gmbh | Safety System for Reducing the Impact Energy of a Container |
| CN204606224U (en) * | 2015-04-15 | 2015-09-02 | 广州快飞计算机科技有限公司 | A kind of unmanned plane landing damping device |
| CN205499330U (en) * | 2016-02-04 | 2016-08-24 | 普宙飞行器科技（深圳）有限公司 | Unmanned aerial vehicle with gasbag of saving oneself |
-
2016
- 2016-12-09 CN CN201611129522.7A patent/CN106741879A/en active Pending
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20080315037A1 (en) * | 2005-12-23 | 2008-12-25 | Airbus Deutschland Gmbh | Safety System for Reducing the Impact Energy of a Container |
| CN204606224U (en) * | 2015-04-15 | 2015-09-02 | 广州快飞计算机科技有限公司 | A kind of unmanned plane landing damping device |
| CN205499330U (en) * | 2016-02-04 | 2016-08-24 | 普宙飞行器科技（深圳）有限公司 | Unmanned aerial vehicle with gasbag of saving oneself |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108482690A (en) * | 2018-04-06 | 2018-09-04 | 丁奕森 | A kind of scalable comprehensive protective device of unmanned plane |
| CN111268103A (en) * | 2020-02-14 | 2020-06-12 | 广东工业大学 | Take dual-purpose unmanned aerial vehicle in sea and air of gasbag |
| CN111268103B (en) * | 2020-02-14 | 2024-03-05 | 广东工业大学 | Sea-air dual-purpose unmanned aerial vehicle with air bag |
| CN111591436A (en) * | 2020-04-30 | 2020-08-28 | 南京理工大学 | Pneumatic soft landing gear of small unmanned aerial vehicle |
| CN111591436B (en) * | 2020-04-30 | 2022-03-18 | 南京理工大学 | Pneumatic soft landing gear of small unmanned aerial vehicle |
| CN111645871A (en) * | 2020-06-18 | 2020-09-11 | 湖北金色阳光创客教育有限公司 | Be used for unmanned aerial vehicle protector that falls |
| CN111645871B (en) * | 2020-06-18 | 2021-09-03 | 湖北金色阳光创客教育有限公司 | Be used for unmanned aerial vehicle protector that falls |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20170531 |
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| RJ01 | Rejection of invention patent application after publication |