CN202464132U - Electronic controlled vehicle-mounted parachute - Google Patents
Electronic controlled vehicle-mounted parachute Download PDFInfo
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- CN202464132U CN202464132U CN2012200467833U CN201220046783U CN202464132U CN 202464132 U CN202464132 U CN 202464132U CN 2012200467833 U CN2012200467833 U CN 2012200467833U CN 201220046783 U CN201220046783 U CN 201220046783U CN 202464132 U CN202464132 U CN 202464132U
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- umbrella
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- parachute
- grain
- circular storage
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Abstract
An electronic controlled vehicle-mounted parachute relates to the field of airborne devices. A main parachute (21) is arranged in a circular parachute storing vacuum bin (11), a powder flask (1) is arranged in the top end of the circular parachute storing vacuum bin (11), a rubber sealing cover (5) is arranged at the top end of the powder flask (1), a moving parachute (4) is arranged in the powder flask (1), powders (2) are arranged on the outer walls of the two sides of the powder flask (1), a detonator (3) is arranged in the powders (2), air exhaust nozzles (8) are symmetrically arranged on the outer walls of the two sides of the powder flask (1) and are all connected with one end of an air pipe (7) by an electromagnetic valve (6), the other end of the air pipe (7) is connected with the circular parachute storing vacuum bin (11), a rope fixing ring (9) is arranged at the bottom end of the powder flask (1) by a parachute line (10), the parachute line (10) is connected with the moving parachute (4), and a connecting rod (20) is arranged in the bottom end of the circular parachute storing vacuum bin (11). According to the electronic controlled vehicle-mounted parachute, remote control powders, vehicle-mounted parachutes and the like are adopted, so that the purpose of safety control of people and airplanes can be achieved.
Description
Technical field:
The utility model relates to airborne device field, is specifically related to a kind of automatically controlled airborne parachute.
Background technology:
Along with the level raising of industry and social life, aviette will become family and function in an acting capacity of instrument, becomes a reality in the near future.Driving an airplane is everyone dream, but the danger that drives an airplane is greatly, vacates existing shutdown because in a single day aircraft flies up into the sky, mechanical breakdown, and during problems such as line fault, its various reasons all can cause the air crash accident.
The utility model content:
The purpose of the utility model provides a kind of automatically controlled airborne parachute, and it can provide aircraft and personal security safety method.
In order to solve the existing problem of background technology; The utility model is to adopt following technical scheme: it comprises grain 1, gunpowder 2, detonator 3, moves and draw umbrella 4, rubber closing cap 5, electromagnetic valve 6, breather pipe 7, the mouthpiece 8 of bleeding, rope set collar 9, umbrella line 10, circular storage umbrella vacuum storehouse 11, lead 12, attaching plug 13, circular storage battery 14, circular keying line plate 15, relay indicating light 16, storage battery indicator lamp 17, remote controller antenna 18, battery charge socket 19, pipe link 20 and main chute 21; Be provided with main chute 21 in the circular storage umbrella vacuum storehouse 11; The inside, top in circular storage umbrella vacuum storehouse 11 is provided with grain 1; The top of grain 1 is provided with rubber closing cap 5; And be provided with in the grain 1 to move and draw umbrella 4, the both sides outer wall of grain 1 is equipped with gunpowder 2, is provided with detonator 3 in the gunpowder 2; The both sides outer wall of grain 1 is arranged with the mouthpiece 8 of bleeding; The mouthpiece 8 of bleeding of both sides all is connected with an end of breather pipe 7 through electromagnetic valve 6, and the other end of breather pipe 7 is connected with circular storage umbrella vacuum storehouse 11, and the bottom of grain 1 is provided with rope set collar 9 through umbrella line 10; Umbrella line 10 draws umbrella 4 and is connected with moving; The inside, bottom in circular storage umbrella vacuum storehouse 11 is provided with pipe link 20, and the bilateral symmetry of pipe link 20 is provided with circular storage battery 14, and the below correspondence of the circular storage battery 14 of both sides is provided with circular keying line plate 15; And circular storage battery 14 is connected with circular storage umbrella vacuum storehouse 11 inboard attaching plugs 13 through lead 12; Attaching plug 13 is connected with electromagnetic valve 6 with detonator 3 respectively through lead 12, and one outside, bottom in circular storage umbrella vacuum storehouse 11 is respectively equipped with remote controller antenna 18 and relay indicating light 16, and its another outside correspondence is respectively equipped with battery charge socket 19 and storage battery indicator lamp 17.
The utility model passes through to adopt remote control gunpowder and airborne parachute etc., thereby has reached the purpose of people and aircraft safety guarantee.
Description of drawings:
Fig. 1 is the structural representation of the utility model.
The specific embodiment:
With reference to Fig. 1; This specific embodiment adopts following technical scheme: it comprises grain 1, gunpowder 2, detonator 3, moves and draw umbrella 4, rubber closing cap 5, electromagnetic valve 6, breather pipe 7, the mouthpiece 8 of bleeding, rope set collar 9, umbrella line 10, circular storage umbrella vacuum storehouse 11, lead 12, attaching plug 13, circular storage battery 14, circular keying line plate 15, relay indicating light 16, storage battery indicator lamp 17, remote controller antenna 18, battery charge socket 19, pipe link 20 and main chute 21; Be provided with main chute 21 in the circular storage umbrella vacuum storehouse 11; The inside, top in circular storage umbrella vacuum storehouse 11 is provided with grain 1, and the top of grain 1 is provided with rubber closing cap 5, and is provided with in the grain 1 to move and draws umbrella 4; The both sides outer wall of grain 1 is equipped with gunpowder 2; Be provided with detonator 3 in the gunpowder 2, the both sides outer wall of grain 1 is arranged with the mouthpiece 8 of bleeding, and the mouthpiece 8 of bleeding of both sides all is connected with an end of breather pipe 7 through electromagnetic valve 6; The other end of breather pipe 7 is connected with circular storage umbrella vacuum storehouse 11; The bottom of grain 1 is provided with rope set collar 9 through umbrella line 10, and umbrella line 10 draws umbrella 4 and is connected with moving, and the inside, bottom in circular storage umbrella vacuum storehouse 11 is provided with pipe link 20; The bilateral symmetry of pipe link 20 is provided with circular storage battery 14; The below correspondence of the circular storage battery 14 of both sides is provided with circular keying line plate 15, and circular storage battery 14 passes through lead 12 and circular storage umbrella vacuum storehouse 11 inboard attaching plugs 13 are connected, and attaching plug 13 is connected with electromagnetic valve 6 with detonator 3 respectively through lead 12; One outside, bottom in circular storage umbrella vacuum storehouse 11 is respectively equipped with remote controller antenna 18 and relay indicating light 16, and its another outside correspondence is respectively equipped with battery charge socket 19 and storage battery indicator lamp 17.
When this specific embodiment is used; At first be installed to automatically controlled airborne parachute on the propshaft of autogyro through pipe link 20; When breaking down when driving an airplane, the computer recognition system through aircraft is cut off the oil circuit of aircraft, and the propeller of aircraft can't be rotated; Through brake gear on the aircraft propeller is stopped the rotation immediately simultaneously; Open the teleswitch in the aircraft handling storehouse simultaneously, make the remote controller antenna of outside, top, aircraft handling storehouse send remote signal, after the remote signal of at this moment sending is received by the remote controller antenna 18 on the automatically controlled airborne parachute; Be sent to signal on the circular keying line plate 15; This moment, circular keying line plate 15 was connected to attaching plug 13 to power supply through lead 12, passed through lead 12 again the detonator 3 of power delivery to 1 li of grain, made grain 1 and rubber closing cap 5 fly away from circular storage umbrella vacuum storehouse 11 simultaneously; At this moment rope set collar 9 draws umbrella 4 to moving of 1 li of grain and pulls out; When moving when drawing umbrella 4 and be about to open, circular keying line plate 15 is connected to attaching plug 13 to power supply through lead 12, forwards electromagnetic valve 6 to through lead 12 again; Electromagnetic valve 6 is opened immediately; At this moment get in the circular storage umbrella vacuum storehouses 11 through breather pipe 7, moving after opening drawn umbrella 4 and drawn back circle storage umbrella vacuum Cang11Gai, draws back the main chutes 21 in the circle storage umbrella vacuum storehouse 11 through rope set collar 9 when drawing back.This specific embodiment also is fit to the aviette of band machine wing.
This specific embodiment is passed through to adopt remote control gunpowder and airborne parachute etc., thereby has reached the purpose of people and aircraft safety guarantee.
Claims (1)
1. automatically controlled airborne parachute; It is characterized in that it comprises grain (1), gunpowder (2), detonator (3), moves and draw umbrella (4), rubber closing cap (5), electromagnetic valve (6), breather pipe (7), the mouthpiece of bleeding (8), rope set collar (9), umbrella line (10), circular storage umbrella vacuum storehouse (11), lead (12), attaching plug (13), circular storage battery (14), circular keying line plate (15), relay indicating light (16), storage battery indicator lamp (17), remote controller antenna (18), battery charge socket (19), pipe link (20) and main chute (21); Be provided with main chute (21) in the circular storage umbrella vacuum storehouse (11); The inside, top in circular storage umbrella vacuum storehouse (11) is provided with grain (1); The top of grain (1) is provided with rubber closing cap (5); And be provided with in the grain (1) to move and draw umbrella (4); The both sides outer wall of grain (1) is equipped with gunpowder (2); Be provided with detonator (3) in the gunpowder (2), the both sides outer wall of grain (1) is arranged with the mouthpiece of bleeding (8), and the mouthpiece of bleeding (8) of both sides all is connected through the end of electromagnetic valve (6) with breather pipe (7); The other end of breather pipe (7) is connected with circular storage umbrella vacuum storehouse (11); The bottom of grain (1) is provided with rope set collar (9) through umbrella line (10), and umbrella line (10) draws umbrella (4) and is connected with moving, and the inside, bottom in circular storage umbrella vacuum storehouse (11) is provided with pipe link (20); The bilateral symmetry of pipe link (20) is provided with circular storage battery (14); The below correspondence of the circular storage battery (14) of both sides is provided with circular keying line plate (15), and circular storage battery (14) passes through lead (12) and the circular inboard attaching plug (13) in umbrella vacuum storehouse (11) that stores up is connected, and attaching plug (13) is connected with electromagnetic valve (6) with detonator (3) respectively through lead (12); One outside, bottom in circular storage umbrella vacuum storehouse (11) is respectively equipped with remote controller antenna (18) and relay indicating light (16), and its another outside correspondence is respectively equipped with battery charge socket (19) and storage battery indicator lamp (17).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012200467833U CN202464132U (en) | 2012-02-14 | 2012-02-14 | Electronic controlled vehicle-mounted parachute |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012200467833U CN202464132U (en) | 2012-02-14 | 2012-02-14 | Electronic controlled vehicle-mounted parachute |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202464132U true CN202464132U (en) | 2012-10-03 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2012200467833U Expired - Fee Related CN202464132U (en) | 2012-02-14 | 2012-02-14 | Electronic controlled vehicle-mounted parachute |
Country Status (1)
| Country | Link |
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| CN (1) | CN202464132U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103693202A (en) * | 2013-08-30 | 2014-04-02 | 北京空间机电研究所 | Recovery system of helicopter |
| CN104326086A (en) * | 2014-10-22 | 2015-02-04 | 襄阳宏伟航空器有限责任公司 | Quick parachute opening device of parachute |
| CN104908953A (en) * | 2015-06-24 | 2015-09-16 | 江苏建筑职业技术学院 | Automatic life-saving protection device and method for preventing airplane from crashing and being hijacked |
| CN111038318A (en) * | 2019-12-31 | 2020-04-21 | 河北科技大学 | Charging base station of drop-in unmanned aerial vehicle |
-
2012
- 2012-02-14 CN CN2012200467833U patent/CN202464132U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103693202A (en) * | 2013-08-30 | 2014-04-02 | 北京空间机电研究所 | Recovery system of helicopter |
| CN103693202B (en) * | 2013-08-30 | 2015-11-11 | 北京空间机电研究所 | A kind of recovery system of helicopter |
| CN104326086A (en) * | 2014-10-22 | 2015-02-04 | 襄阳宏伟航空器有限责任公司 | Quick parachute opening device of parachute |
| CN104908953A (en) * | 2015-06-24 | 2015-09-16 | 江苏建筑职业技术学院 | Automatic life-saving protection device and method for preventing airplane from crashing and being hijacked |
| CN111038318A (en) * | 2019-12-31 | 2020-04-21 | 河北科技大学 | Charging base station of drop-in unmanned aerial vehicle |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20121003 Termination date: 20150214 |
|
| EXPY | Termination of patent right or utility model |