CN105366065A - Anti-falling unmanned aerial vehicle - Google Patents
Anti-falling unmanned aerial vehicle Download PDFInfo
- Publication number
- CN105366065A CN105366065A CN201510934209.XA CN201510934209A CN105366065A CN 105366065 A CN105366065 A CN 105366065A CN 201510934209 A CN201510934209 A CN 201510934209A CN 105366065 A CN105366065 A CN 105366065A
- Authority
- CN
- China
- Prior art keywords
- air
- shatter
- unmanned vehicle
- resistant unmanned
- vehicle according
- 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.)
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D45/04—Landing aids; Safety measures to prevent collision with earth's surface
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U70/00—Launching, take-off or landing arrangements
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
Abstract
The invention discloses an anti-falling unmanned aerial vehicle. The anti-falling unmanned aerial vehicle comprises an aerial vehicle body (1), a flying wing (2), flying propellers (4) and an anti-collision air cushion. One end of the flying wing (2) is fixedly connected with the outer side wall of the aerial vehicle body (1), the other end of the flying wing (2) extends in the radial direction of the aerial vehicle body (1), and the flying propellers (4) are mounted at the other end of the flying wing (2). The anti-collision air cushion is arranged at the top end of the aerial vehicle body (1). By means of the anti-falling unmanned aerial vehicle, crash losses of the unmanned aerial vehicle can be reduced to the largest extent, and the service life of the unmanned aerial vehicle can be prolonged.
Description
Technical field
The present invention relates to unmanned vehicle field, particularly, relate to a kind of shatter-resistant unmanned vehicle.
Background technology
Unmanned vehicle is the not manned craft utilizing radio telecommand or the process controller provided for oneself to handle, along with the continuous progress of science and technology, the development of unmanned vehicle technology is more and more ripe, use more and more extensive, not only can be used for battle reconnaissance and supervision, positioning school are penetrated, injured the military missions such as assessment, electronic warfare, but also oneself is as target drone, also can be used for civilian, as border patrol, nuclear radiation detection, aerial photography, mineral exploration aviation, the condition of a disaster supervision, traffic patrolling, security monitoring etc.
But; alighting gear is the important device of unmanned vehicle landing; certain buffer action can be played when the air crash of aircraft et out of order; but current landing gear buffer action is very limited; protection can only be made to landing bottom aircraft; and when aircraft turn land top down time helpless, be therefore badly in need of providing a kind of shatter-resistant unmanned vehicle reducing unmanned vehicle air crash loss to greatest extent.
Summary of the invention
The object of this invention is to provide a kind of shatter-resistant unmanned vehicle, this shatter-resistant unmanned vehicle can reduce unmanned vehicle air crash loss to greatest extent, extends aircraft service life.
To achieve these goals, the invention provides a kind of shatter-resistant unmanned vehicle, this shatter-resistant unmanned vehicle comprises aircraft body, flying wing, flight oar and anti-collision air-bed; One end of flying wing is fixed on the lateral wall of aircraft body, and the other end stretches out along the radial direction of aircraft body and is provided with flight oar; Wherein, the anti-collision air-bed top being arranged on aircraft body.
Preferably, anti-collision air-bed is type inflatable air cushion, and the top of aircraft body is provided with inflatable appliance, and the air-filled pore of type inflatable air cushion is connected with the air extractor duct of inflatable appliance inflatable appliance can be inflated in type inflatable air cushion.
Preferably, inflatable appliance is inflation pump.
Preferably, inflatable appliance is a box body with cavity, and the top of box body offers an air gate, and the air-filled pore of type inflatable air cushion seals mutually with air gate and is communicated with; Wherein, sodium azide or ammonium nitrate is loaded with in cavity.
Preferably, the air gate on box body has multiple and is evenly distributed on the top surface of box body; The quantity of type inflatable air cushion is equal with the quantity of air gate.
Preferably, flying wing is flexible flying wing and can stretches along the radial direction of aircraft body.
Preferably, the oar that flies is double bladed paddle or three leaf oars.
Preferably, this shatter-resistant unmanned vehicle also comprises at least two feets, and feet is disposed on the bottom face of aircraft body.
According to technique scheme; the present invention arrange on aircraft top one anti-collision air-bed; when this aircraft aloft flown break down turn head downward air crash time; when colliding surface, the anti-collision air-bed hard hit that can be good between buffering aircraft and ground is hit; protect its top injury-free, substantially prolongs the service life of aircraft.
Other features and advantages of the present invention are described in detail in detailed description of the invention part subsequently.
Accompanying drawing explanation
Accompanying drawing is used to provide a further understanding of the present invention, and forms a part for specification sheets, is used from explanation the present invention, but is not construed as limiting the invention with detailed description of the invention one below.In the accompanying drawings:
Fig. 1 is the structural representation according to the shatter-resistant unmanned vehicle in a kind of embodiment provided by the invention.
Description of reference numerals
1-aircraft body 2-flying wing
3-type inflatable air cushion 4-flies oar
5-box body 6-air gate
7-feet
Detailed description of the invention
Below in conjunction with accompanying drawing, the specific embodiment of the present invention is described in detail.Should be understood that, detailed description of the invention described herein, only for instruction and explanation of the present invention, is not limited to the present invention.
In the present invention, when not doing contrary explanation, the nouns of locality be included in term such as " top, bottoms " only represents the orientation of this term under normal service condition, or being commonly called as those skilled in the art's understanding, and should not be considered as the restriction to this term.
See Fig. 1, the invention provides a kind of shatter-resistant unmanned vehicle, this shatter-resistant unmanned vehicle comprises aircraft body 1, flying wing 2, flight oar 4 and anti-collision air-bed; One end of flying wing 2 is fixed on the lateral wall of aircraft body 1, and the other end stretches out along the radial direction of aircraft body 1 and is provided with flight oar 4; Wherein, the anti-collision air-bed top being arranged on aircraft body 1.
Pass through technique scheme; arrange on aircraft top one anti-collision air-bed; when this aircraft aloft flown break down turn head downward air crash time; when colliding surface, the anti-collision air-bed hard hit that can be good between buffering aircraft and ground is hit; protect its top injury-free, substantially prolongs the service life of aircraft.
In order to make the anti-collision air-bed injury that can alleviate aircraft better, the secondary injury of upspringing after avoiding colliding surface, preferably, anti-collision air-bed is type inflatable air cushion 3, the top of aircraft body 1 is provided with inflatable appliance, and the air-filled pore of type inflatable air cushion 3 is connected with the air extractor duct of inflatable appliance inflatable appliance can be inflated in type inflatable air cushion 3.
Above-mentioned inflatable appliance can be that any one common in this area can the mechanical equipment of fast aeration, but from alleviating aircraft overall weight and the angle of controlling cost is considered, preferably, inflatable appliance is inflation pump.
Further, in order to alleviate the load of aircraft, increase its particle carrying capacity, preferred inflatable appliance is a box body 5 with cavity, and the top of box body 5 offers an air gate 6, and the air-filled pore of type inflatable air cushion 3 seals with air gate 6 phase and is communicated with; Wherein, sodium azide or ammonium nitrate is loaded with in cavity.Like this, when clashing into generation, can there is decomposition reaction rapidly in sodium azide or ammonium nitrate, produce a large amount of gas, is full of type inflatable air cushion 3.
In addition, in order to increase the protected area to aircraft top end face, preferably, the air gate 6 on box body 5 has multiple and is evenly distributed on the top surface of box body 5; The quantity of type inflatable air cushion 3 is equal with the quantity of air gate 6.
In present embodiment, in order to the flight that can adjust unmanned vehicle easily according to flight space size takes up room, make it can free flight in different spaces, preferably, flying wing 2 be flexible flying wing and can stretches along the radial direction of aircraft body 1.
In addition, in order to obtain pulsation-free up current when flying oar 4 High Rotation Speed, keep the stability of aircraft, preferably, flight oar 4 is double bladed paddle or three leaf oars.
When aircraft drop to rugged jump area, in order to avoid aircraft body 1 or flying wing 2 collide with ground, extend the service life of aircraft, preferably, this shatter-resistant unmanned vehicle also comprises at least two feets 7, and feet 7 is disposed on the bottom face of aircraft body 1.
Below the preferred embodiment of the present invention is described in detail by reference to the accompanying drawings; but; the present invention is not limited to the detail in above-mentioned embodiment; within the scope of technical conceive of the present invention; can carry out multiple simple variant to technical scheme of the present invention, these simple variant all belong to protection scope of the present invention.
It should be noted that in addition, each concrete technical characteristic described in above-mentioned detailed description of the invention, in reconcilable situation, can be combined by any suitable mode, in order to avoid unnecessary repetition, the present invention illustrates no longer separately to various possible array mode.
In addition, also can carry out combination in any between various different embodiment of the present invention, as long as it is without prejudice to thought of the present invention, it should be considered as content disclosed in this invention equally.
Claims (8)
1. a shatter-resistant unmanned vehicle, is characterized in that, described shatter-resistant unmanned vehicle comprises aircraft body (1), flying wing (2), flight oar (4) and anti-collision air-bed; One end of described flying wing (2) is fixed on the lateral wall of described aircraft body (1), and the other end stretches out along the radial direction of described aircraft body (1) and is provided with described flight oar (4); Wherein, the described anti-collision air-bed top being arranged on described aircraft body (1).
2. shatter-resistant unmanned vehicle according to claim 1, it is characterized in that, described anti-collision air-bed be type inflatable air cushion (3), the top of described aircraft body (1) is provided with inflatable appliance, and the air-filled pore of described type inflatable air cushion (3) is connected with the air extractor duct of described inflatable appliance described inflatable appliance can be inflated in described type inflatable air cushion (3).
3. shatter-resistant unmanned vehicle according to claim 2, is characterized in that, described inflatable appliance is inflation pump.
4. shatter-resistant unmanned vehicle according to claim 2, it is characterized in that, described inflatable appliance is a box body (5) with cavity, the top of described box body (5) offers an air gate (6), and the air-filled pore of described type inflatable air cushion (3) seals mutually with described air gate (6) and is communicated with; Wherein, sodium azide or ammonium nitrate is loaded with in described cavity.
5. shatter-resistant unmanned vehicle according to claim 4, is characterized in that, the air gate (6) on described box body (5) has multiple and is evenly distributed on the top surface of described box body (5); The quantity of described type inflatable air cushion (3) is equal with the quantity of described air gate (6).
6. shatter-resistant unmanned vehicle according to claim 1, is characterized in that, described flying wing (2) is flexible flying wing and can stretches along the radial direction of described aircraft body (1).
7. shatter-resistant unmanned vehicle according to claim 1, is characterized in that, described flight oar (4) is double bladed paddle or three leaf oars.
8. shatter-resistant unmanned vehicle according to claim 1, it is characterized in that, described shatter-resistant unmanned vehicle also comprises at least two feets (7), and described feet (7) is disposed on the bottom face of described aircraft body (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510934209.XA CN105366065A (en) | 2015-12-14 | 2015-12-14 | Anti-falling unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510934209.XA CN105366065A (en) | 2015-12-14 | 2015-12-14 | Anti-falling unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105366065A true CN105366065A (en) | 2016-03-02 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510934209.XA Pending CN105366065A (en) | 2015-12-14 | 2015-12-14 | Anti-falling unmanned aerial vehicle |
Country Status (1)
| Country | Link |
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| CN (1) | CN105366065A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106005451A (en) * | 2016-08-03 | 2016-10-12 | 安徽钰龙信息科技有限公司 | Water travel protection system for shipborne unmanned aerial vehicle based on Internet of Things |
| CN106428549A (en) * | 2016-11-21 | 2017-02-22 | 苏州曾智沃德智能科技有限公司 | Carrying device for unmanned aerial vehicle |
| CN113135297A (en) * | 2021-05-17 | 2021-07-20 | 宜宾职业技术学院 | Unmanned aerial vehicle anti-falling device |
-
2015
- 2015-12-14 CN CN201510934209.XA patent/CN105366065A/en active Pending
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106005451A (en) * | 2016-08-03 | 2016-10-12 | 安徽钰龙信息科技有限公司 | Water travel protection system for shipborne unmanned aerial vehicle based on Internet of Things |
| CN106005451B (en) * | 2016-08-03 | 2018-10-26 | 安徽钰龙信息科技有限公司 | A kind of boat-carrying unmanned plane based on Internet of Things traveling waterborne protects system |
| CN106428549A (en) * | 2016-11-21 | 2017-02-22 | 苏州曾智沃德智能科技有限公司 | Carrying device for unmanned aerial vehicle |
| CN113135297A (en) * | 2021-05-17 | 2021-07-20 | 宜宾职业技术学院 | Unmanned aerial vehicle anti-falling device |
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| C06 | Publication | ||
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| WD01 | Invention patent application deemed withdrawn after publication | ||
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Application publication date: 20160302 |