CN201604799U - Anti-falling self-rescue device for airplanes - Google Patents

Anti-falling self-rescue device for airplanes Download PDF

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Publication number
CN201604799U
CN201604799U CN2010201080392U CN201020108039U CN201604799U CN 201604799 U CN201604799 U CN 201604799U CN 2010201080392 U CN2010201080392 U CN 2010201080392U CN 201020108039 U CN201020108039 U CN 201020108039U CN 201604799 U CN201604799 U CN 201604799U
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CN
China
Prior art keywords
hot gas
parachute
umbrella
platform
rescue device
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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
CN2010201080392U
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Chinese (zh)
Inventor
孙磊
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.)
Sun Lei
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Individual
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Publication date
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Priority to CN2010201080392U priority Critical patent/CN201604799U/en
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Publication of CN201604799U publication Critical patent/CN201604799U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

The utility model discloses a device for traffic and transportation safety, and particularly relates to an anti-falling self-rescue device for airplanes. The anti-falling self-rescue device adopts the structure that a hot gas parachute pillar (2) is connected to an airplane body (1); a parachute sending table (3) is connected to the upper end of the hot gas parachute pillar (2); a hot gas parachute (4) and a plurality of hot gas tables (5) used for supplying hot gas energy for the hot gas parachute (4) are arranged in the parachute sending table (3); and a controller (6) controlling the parachute sending table (3) to open is mounted on the parachute sending table (3). The utility model has simple structure, and adopts the principle of hot gas balloon. When an airplane has an accident, the controller is started to open the parachute sending table, the hot gas parachute in the parachute sending table rises upwards after being started by a heat source so as to provide the airplane with upward force to ensure that the airplane falls slowly and land safely. Therefore, the utility model can effectively prevent the airplane from crashing down during air disaster.

Description

Aircraft falling-prevention self-rescue device
Technical field
The utility model relates to a kind of traffic safety device, relates in particular to a kind of aircraft falling-prevention self-rescue device.
Background technology
Along with development of science and technology, aircraft has become the important vehicle of people's trip gradually.Trip has characteristics easily and efficiently by air, by plane.The people that civil aircraft is taken is many, in case aircraft faces a danger, is difficult to sue and labour with the mode of parachute jumping.Because the influence of factors such as weather, the accident that airplane crash appears in aircraft happens occasionally.When aircraft runs into the accident that can not get rid of, will cause that machine is ruined, the people dies, according to statistics, 1500 people on average there is every year owing to aircraft accident is died in an accident.This brings massive losses for people's life and property.Can safe falling ground when how to solve aircraft and meeting with an accidet, be the technical matters that those skilled in the art are badly in need of solving.
The utility model content
The utility model is exactly in order to solve the problems of the technologies described above, and a kind of aircraft falling-prevention self-rescue device is provided, and it is simple in structure, can safe falling ground when aircraft is met with an accidet.
In order to solve the problems of the technologies described above, the utility model is achieved by the following technical solution.
Aircraft falling-prevention self-rescue device, its structure is as follows: be connected with hot gas umbrella post on the airframe, hot gas umbrella post upper end is connected with sends out a umbrella platform, sends out to be provided with the hot gas parachute in the umbrella platform and for the hot gas parachute provides a plurality of hot gas platforms of the hot gas energy, sends out control is installed on the umbrella platform sends out a umbrella platform control of turning device.
Aircraft falling-prevention self-rescue device, its structure is as follows: be connected with on the airframe and send out the umbrella platform, sending out the umbrella platform is connected with airframe by connecting band, send out and to be provided with the hot gas parachute in the umbrella platform and, send out and control is installed on the umbrella platform sends out a umbrella platform control of turning device for the hot gas parachute provides a plurality of hot gas platforms of the hot gas energy.
Described hot gas platform is 3-10.
The height of described hot gas umbrella post is 10-40mm.
The belly of described airframe is provided with air bag.
Described air bag is higher than aircraft return pulley 20mm.
Advantage of the present utility model and effect are as follows:
The utility model is simple in structure, adopt the fire balloon principle, work as emergency chute, opening controller starts and sends out the umbrella platform, the hot gas parachute of sending out in the umbrella platform starts through thermal source, upwards rise, give power that makes progress of aircraft, aircraft is slowly descended, and the safety landing, prevent that effectively aircraft from running into airplane crash and crashing.
Description of drawings
Fig. 1 is the structural representation of the utility model embodiment 1.
Fig. 2 is the structural representation of the utility model embodiment 2.
Among the figure, 1, airframe, 2, hot gas umbrella post, 3, send out the umbrella platform, 4, the hot gas parachute, 5, the hot gas platform, 6, controller, 7, connecting band.
The specific embodiment
Below in conjunction with accompanying drawing the utility model is described in further detail, but protection domain of the present utility model is not limit by embodiment.
Embodiment 1:
As shown in Figure 1, the utility model aircraft falling-prevention self-rescue device, its structure is as follows: be connected with hot gas umbrella post 2 on the airframe 1, hot gas umbrella post 2 upper ends are connected with sends out umbrella platform 3, send out and to be provided with hot gas parachute 4 in the umbrella platform 3 and, send out and control is installed on the umbrella platform 3 sends out umbrella platform 3 control of turning devices 6 for hot gas parachute 4 provides a plurality of hot gas platforms 5 of the hot gas energy.
Above-mentioned hot gas platform 5 is 3-10.The height of hot gas umbrella post 2 is 10-40mm.
Be provided with the air bag of cushioning effect at the belly of airframe, air bag is higher than aircraft return pulley 20mm.
Embodiment 2:
As shown in Figure 2, the utility model aircraft falling-prevention self-rescue device, its structure is as follows: be connected with on the airframe 1 and send out umbrella platform 3, sending out umbrella platform 3 is connected with airframe 1 by connecting band 7, send out and to be provided with hot gas parachute 4 in the umbrella platform 3 and, send out and control is installed on the umbrella platform 3 sends out umbrella platform 3 control of turning devices 6 for hot gas parachute 4 provides a plurality of hot gas platforms 5 of the hot gas energy.Other structure is with embodiment 1.
Principle of work of the present utility model is as follows:
[0024] work as emergency chute, opening controller starts and sends out the umbrella platform, and the hot gas parachute in the umbrella platform starts through thermal source, upwards rises, and gives power that makes progress of aircraft, and aircraft is slowly descended, and the safety landing, prevents that effectively aircraft from running into airplane crash and crashing.

Claims (6)

1. aircraft falling-prevention self-rescue device, it is characterized in that structure is as follows: be connected with hot gas umbrella post (2) on the airframe (1), hot gas umbrella post (2) upper end is connected with sends out umbrella platform (3), send out and to be provided with hot gas parachute (4) in the umbrella platform (3) and, send out and control is installed on the umbrella platform (3) sends out umbrella platform (a 3) control of turning device (6) for hot gas parachute (4) provides a plurality of hot gas platforms (5) of the hot gas energy.
2. aircraft falling-prevention self-rescue device, it is characterized in that structure is as follows: be connected with on the airframe (1) and send out umbrella platform (3), sending out umbrella platform (3) is connected with airframe (1) by connecting band (7), send out and to be provided with hot gas parachute (4) in the umbrella platform (3) and, send out and control is installed on the umbrella platform (3) sends out umbrella platform (a 3) control of turning device (6) for hot gas parachute (4) provides a plurality of hot gas platforms (5) of the hot gas energy.
3. aircraft falling-prevention self-rescue device according to claim 1 and 2 is characterized in that described hot gas platform (5) is 3-10.
4. aircraft falling-prevention self-rescue device according to claim 1 and 2, the height that it is characterized in that described hot gas umbrella post (2) is 10-40mm.
5. aircraft falling-prevention self-rescue device according to claim 1 and 2 is characterized in that the belly of described airframe is provided with air bag.
6. aircraft falling-prevention self-rescue device according to claim 5 is characterized in that described air bag is higher than aircraft return pulley 20mm.
CN2010201080392U 2010-02-04 2010-02-04 Anti-falling self-rescue device for airplanes Expired - Fee Related CN201604799U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2010201080392U CN201604799U (en) 2010-02-04 2010-02-04 Anti-falling self-rescue device for airplanes

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2010201080392U CN201604799U (en) 2010-02-04 2010-02-04 Anti-falling self-rescue device for airplanes

Publications (1)

Publication Number Publication Date
CN201604799U true CN201604799U (en) 2010-10-13

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN2010201080392U Expired - Fee Related CN201604799U (en) 2010-02-04 2010-02-04 Anti-falling self-rescue device for airplanes

Country Status (1)

Country Link
CN (1) CN201604799U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2013120357A1 (en) * 2012-02-17 2013-08-22 Sun Lei Airplane anti-falling and self-rescuing device
CN105056418A (en) * 2015-06-11 2015-11-18 淮南智辉装饰工程有限公司 Escape backpack for high-rise building

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2013120357A1 (en) * 2012-02-17 2013-08-22 Sun Lei Airplane anti-falling and self-rescuing device
CN105056418A (en) * 2015-06-11 2015-11-18 淮南智辉装饰工程有限公司 Escape backpack for high-rise building

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
C41 Transfer of patent application or patent right or utility model
TR01 Transfer of patent right

Effective date of registration: 20111014

Address after: Mudanjiang City, Heilongjiang Province Xinghua 157200 Dongning County District three 1 unit 201 room

Patentee after: Sun Lei

Address before: Mudanjiang City, Heilongjiang province 157200 Building 1 unit 203 Dongning county Party School

Patentee before: Sun Lei

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

Granted publication date: 20101013

Termination date: 20130204

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