CN207482205U - Aircraft double layer security air bag - Google Patents

Aircraft double layer security air bag Download PDF

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Publication number
CN207482205U
CN207482205U CN201721599264.9U CN201721599264U CN207482205U CN 207482205 U CN207482205 U CN 207482205U CN 201721599264 U CN201721599264 U CN 201721599264U CN 207482205 U CN207482205 U CN 207482205U
Authority
CN
China
Prior art keywords
external capsule
capsula interna
air bag
aircraft
double layer
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.)
Expired - Fee Related
Application number
CN201721599264.9U
Other languages
Chinese (zh)
Inventor
李文峰
雷涛
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Yunnan Da Han Xianglong Aeronautical Science And Technology Co Ltd
Original Assignee
Yunnan Da Han Xianglong Aeronautical Science And Technology Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Yunnan Da Han Xianglong Aeronautical Science And Technology Co Ltd filed Critical Yunnan Da Han Xianglong Aeronautical Science And Technology Co Ltd
Priority to CN201721599264.9U priority Critical patent/CN207482205U/en
Application granted granted Critical
Publication of CN207482205U publication Critical patent/CN207482205U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses a kind of aircraft double layer security air bags, and including capsula interna and external capsule, the capsula interna is wrapped in inside external capsule, and the part utricule and capsula interna of the external capsule are integrated;The capsula interna is closed air bag, which is provided with an inflating port;The external capsule lower part is equipped with several aeration holes.Advantage is that the aircraft double layer security air bag of the utility model is made of two layers of air bag, closed capsula interna and open external capsule, when aircraft stall, safety device can control gas cylinder to carry out detonation inflation to capsula interna, the external capsule of its outer layer can be strutted after capsula interna detonation, then continuing during whereabouts, air is entered by the aeration hole above external capsule props up external capsule in external capsule.First time buffering is first carried out by external capsule with hitting when air bag hits ground, outer intracapsular gas can urge releasing, and capsula interna is made to carry out second and is hit.It is soft shock to hit for the first time, is next only the buffering collision of closed of capsula interna, maximumlly protects the complete and safe of aircraft.

Description

Aircraft double layer security air bag
Technical field
The utility model is related to unmanned vehicle field, more particularly to a kind of aircraft double layer security air bag.
Background technology
Aircraft is when accident occurs in flight, in order to reduce the damage of aircraft, needs to carry out impact protector to aircraft, Air bag is generally adopted by carry out the impact protector of aircraft, but existing air bag is all the closed gas of individual layer Capsule, it is excessive in the pressure born in a flash of shock, and only once cushioning effect, aircraft damage is may result in, even Directly air bag may be hit quick-fried, lose protective effect.
Utility model content
The technical problem to be solved by the present invention is to provide a kind of aircraft that can effectively reduce shock dynamics is double-deck Air bag.
In order to solve the above-mentioned technical problem, the technical solution of the utility model is:
A kind of aircraft double layer security air bag, including capsula interna and external capsule, the capsula interna is wrapped in inside external capsule, described outer The part utricule and capsula interna of capsule are integrated;The capsula interna is closed air bag, which is provided with an inflating port;The external capsule lower part Equipped with several aeration holes.
Further, best for the buffering effect of air bag, capsula interna and external capsule are ellipse, and oval air bag is colliding When and the contact area on ground can gradually increase so that pressure is gradually retarded.
Further, in order to increase the efficiency of air inlet, support ring can be embedded in the peritreme of aeration hole, by aeration Hole supports.
Further, it is connected with tracheae on inflating port.
The utility model is beneficial in that:
The aircraft double layer security air bag of the utility model is made of two layers of air bag, closed capsula interna and open external capsule, When aircraft stall, safety device can control gas cylinder to carry out detonation inflation to capsula interna, its outer layer can be strutted after capsula interna detonation Then external capsule is continuing during whereabouts, air is entered by the aeration hole above external capsule props up external capsule in external capsule.When Air bag first carries out first time buffering with hitting when hitting ground by external capsule, and outer intracapsular gas can urge releasing, and capsula interna is made to carry out second It hits.The open by design of external capsule so that it is soft shock to hit for the first time, is next only the buffering collision of closed of capsula interna, maximum That changes protects the complete and safe of aircraft.
Description of the drawings
FIG. 1 is a schematic structural view of the utility model.
In figure:1- capsula internas, 2- inflating ports, 3- external capsules, 31- aeration holes, 4- support rings, 5- tracheaes.
Specific embodiment
Specific embodiment of the present utility model is described further below in conjunction with the accompanying drawings.It should be noted that The explanation of these embodiments is used to help to understand the utility model, but do not form the restriction to the utility model.This Outside, technical characteristic involved in the various embodiments of the present invention described below is as long as they do not conflict with each other It can be combined with each other.
As shown in Figure 1:
A kind of aircraft double layer security air bag, including capsula interna 1 and external capsule 3, capsula interna 1 is wrapped in inside external capsule 3, described outer The part utricule and capsula interna 1 of capsule 3 are integrated;The capsula interna 1 is closed air bag, which is provided with an inflating port 2;The external capsule 3 lower parts are equipped with several aeration holes 31.
As preference, the buffering effect for air bag is best, capsula interna 1 and external capsule 3 are ellipse, and oval air bag exists The contact area on during collision and ground can gradually increase so that pressure is gradually retarded.
As preference, in order to increase the efficiency of air inlet, support ring 4 can be embedded in the peritreme of aeration hole 31, Aeration hole 31 is supported.
As preference, being connected convenient for gas cylinder, tracheae 5 is connected on inflating port 2.
The aircraft double layer security air bag of the utility model is made of two layers of air bag, closed capsula interna 1 and open external capsule 3, when aircraft stall, safety device can control gas cylinder to carry out detonation inflation to capsula interna 1, and capsula interna 1 can be strutted outside it after detonating Then the external capsule 3 of layer is continuing during whereabouts, air enters 3 inner support of external capsule by the aeration hole 31 above external capsule 3 Play external capsule 3.First time buffering is first carried out by external capsule 3 with hitting when air bag hits ground, the gas in external capsule 3 can urge releasings, make interior Capsule 1 carries out second and hits.The open by design of external capsule 3 so that it is soft shock to hit for the first time, is next only capsula interna 1 Buffering collision of closed, maximumlly protect the complete and safe of aircraft.
The embodiment of the utility model is explained in detail, but the utility model is not limited to be retouched above in association with attached drawing The embodiment stated.For a person skilled in the art, it is right in the case where not departing from the utility model principle and spirit These embodiments carry out a variety of change, modification, replacement and modification, still fall in the scope of protection of the utility model.

Claims (4)

1. a kind of aircraft double layer security air bag, it is characterised in that:Including capsula interna (1) and external capsule (3), the capsula interna (1) is wrapped It is internal to be rolled in external capsule (3), the part utricule and capsula interna (1) of the external capsule (3) are integrated;The capsula interna (1) is closed air bag, It which is provided with an inflating port (2);External capsule (3) lower part is equipped with several aeration holes (31).
2. aircraft double layer security air bag according to claim 1, it is characterised in that:The capsula interna (1) and external capsule (3) are equal For ellipse.
3. aircraft double layer security air bag according to claim 1, it is characterised in that:The peritreme of the aeration hole (31) It is upper to be embedded with support ring (4).
4. according to claim 1-3 any one of them aircraft double layer security air bags, it is characterised in that:The inflating port (2) On be connected with tracheae (5).
CN201721599264.9U 2017-11-27 2017-11-27 Aircraft double layer security air bag Expired - Fee Related CN207482205U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201721599264.9U CN207482205U (en) 2017-11-27 2017-11-27 Aircraft double layer security air bag

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201721599264.9U CN207482205U (en) 2017-11-27 2017-11-27 Aircraft double layer security air bag

Publications (1)

Publication Number Publication Date
CN207482205U true CN207482205U (en) 2018-06-12

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201721599264.9U Expired - Fee Related CN207482205U (en) 2017-11-27 2017-11-27 Aircraft double layer security air bag

Country Status (1)

Country Link
CN (1) CN207482205U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110877748A (en) * 2019-12-06 2020-03-13 湖南浩天翼航空技术有限公司 But folding double-deck gasbag of retrieving of parachute landing unmanned aerial vehicle quick replacement

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110877748A (en) * 2019-12-06 2020-03-13 湖南浩天翼航空技术有限公司 But folding double-deck gasbag of retrieving of parachute landing unmanned aerial vehicle quick replacement

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GR01 Patent grant
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20180612

Termination date: 20211127