CN103979110A - Ballistic parachute life-saving system - Google Patents
Ballistic parachute life-saving system Download PDFInfo
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- CN103979110A CN103979110A CN201410232222.6A CN201410232222A CN103979110A CN 103979110 A CN103979110 A CN 103979110A CN 201410232222 A CN201410232222 A CN 201410232222A CN 103979110 A CN103979110 A CN 103979110A
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- parachute
- umbrella
- canopy
- saving system
- life saving
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Abstract
A ballistic parachute life-saving system comprises a parachute system, a rocket engine system and a handing system, wherein the parachute system comprises a parachute-opening pull rope, a parachute cover, a parachute rope and a connecting belt. One end of the parachute-opening pull rope is connected with the top of the parachute cover, the bottom edge of the parachute cover is connected with one end of the parachute rope, the other end of the parachute rope is connected with one end of the connecting belt, and the other end of the connecting belt is connected with the upper end of hanging belts. The rocket engine system comprises a rocket barrel and an ignition device, wherein the other end of the parachute-opening pull rope is connected with the rocket barrel. The hanging system comprises multiple hanging belts, wherein the lower ends of the hanging belts are connected with hanging points on an aircraft. The system can be started through an engine of the rocket barrel and can be used for life-saving of flight crew and the aircraft. For example, the life-saving system can be used for 1-2 seat hung glider, a motor driven paraglider, an ultra-light aircraft, an ultra-light glider and experimental type and small light-duty aircrafts.
Description
Technical field
The present invention relates to life saving system field, particularly, relate to a kind of ballistic parachute life saving system.
Background technology
In the ZL200820233272 of bulletin on October 7th, 2009, a kind of parachute that low altitude lifesaving is used that is applicable to is disclosed, this low altitude lifesaving parachute comprises canopy and is connected in the umbrella rope on canopy, be characterised in that and uniformly on canopy be attached with multiple column gas bundles, multiple column gas bundles provide source of the gas by the high-pressure aerated cylinder being communicated with it, between column gas bundle and high-pressure aerated cylinder, are communicated with by the high-pressure aerated pipe with unidirectional charge valve.It is rational in infrastructure, safety of operation is reliable, has solved under low empty condition the method for parachute-opening fast and stable landing, provides a kind of new mode for crowd in the time that the disaster scenarios it such as earthquake, fire occurs escapes to be rescued on high-rise building.This mean of escape is also suitable for field and is landed by the low latitude at crag place.But this life-saving para chute can only carry less weight, cannot Application Example as large-sized objects such as aircraft.
But, modern aircraft is more and more, the development of the gliding parachute especially driving at 1-2 seat hang glider, motor, the aspect such as aircraft, aerodone, test-type and the small-sized light-duty flying toy of microlight-type of microlight-type is maked rapid progress especially, but in the time there is emergency in aircraft or aviator, cannot escape danger, occur fatal crass's situation.Be below several emergency situations that easily occur:
1) above rugged landform time, the engine has gone wrong, when impossible safe landing;
2) aircraft get out of hand: i) because technological deficiency; Ii) weather condition is severe, loses pilotage control; Iii) because other reasons loses pilotage control;
3), because of aviator's health problem, make it can not continue safe flight (for example, heart attack etc.);
4) lose sense of direction because severe meteorological conditions makes aviator, may bump against with certain obstacle, visbility reduces, lack of fuel to be to arrive at safe landing site;
5) mechanical defect causes continuing safe flight and safe landing.
In view of as above reason, be necessary to study a kind of ballistic parachute life saving system, to solve problems of the prior art.
Summary of the invention
Considers at least one the problems referred to above and completed the present invention, and one object of the present invention is to provide a kind of ballistic parachute life saving system, it is characterized in that comprising:
Parachute system, it comprises parachute lanyard, canopy, umbrella rope and connecting band, parachute lanyard one end is connected with canopy top, Connectable umbrella rope one end, canopy base, the umbrella rope other end is connected with connecting band one end, and the connecting band other end is connected with the upper end of following straphanger;
Rocket engine system, it comprises rocket socket and ignition device, wherein the other end of parachute lanyard is connected with rocket socket; And
Hangar system, it comprises many straphangers, the lower end of wherein said straphanger connects carry-on sling point.
That is to say, this system can be by the engine start of rocket socket, can be used for crew's (comprising aircraft) to carry out lifesaving.For example this life saving system can be used for 1-2 seat hang glider, the gliding parachute of motor driving, the aircraft of microlight-type, aerodone, test-type and the small-sized light-duty flying toy of microlight-type.
According to a further aspect of the invention, described system also comprises umbrella cabin, and described canopy and umbrella rope are arranged in umbrella cabin.
According to a further aspect of the invention, also comprise the dress umbrella cover being arranged in umbrella cabin, described canopy and umbrella rope are arranged in dress umbrella cover.
According to a further aspect of the invention, described canopy top is sewed with umbrella top loop, and canopy connects one end of described parachute lanyard by described umbrella top loop.
According to a further aspect of the invention, described ignition device is connected with the engine of described rocket socket.
According to a further aspect of the invention, the upper end of described straphanger is converged and is a bit connected with the other end of described connecting band.
According to a further aspect of the invention, parachute lanyard and connecting band are arranged on umbrella out of my cabin and are positioned on the opposite side in umbrella cabin.
According to a further aspect of the invention, rocket engine system is arranged on the sidewall in umbrella cabin.
According to a further aspect of the invention, described umbrella cabin is provided with openable protecgulum.
According to a further aspect of the invention, described canopy is arranged on the top of described umbrella rope.
Compared with prior art, beneficial effect of the present invention is: in the time that aircraft is in an emergency, aviator starts the ignition device of rocket engine, the solid fuel of rocket engine takes fire, rocket engine transmitting, progressively pulls out canopy, umbrella rope and straphanger (being hoist cable) by parachute lanyard, and hoist cable connects aircraft, parachute is all opened, and parachute carries aircraft security landing.
Brief description of the drawings
Fig. 1 is the structural representation of ballistic parachute life saving system according to the preferred embodiment of the invention.
Fig. 2 is the connection diagram of ballistic parachute life saving system and aircraft according to the preferred embodiment of the invention.
Fig. 3-10th, according to the preferred embodiment of the invention real work flow process and the view of ballistic parachute life saving system.
In figure, 1, umbrella cabin, 2, protecgulum, 3, bell, 4, ignition device, 5, rocket engine, 6, connecting band, 7, parachute lanyard, 8, dress umbrella cover, 9, umbrella rope, 10, umbrella top loop, 11, aircraft, 12, straphanger
Detailed description of the invention
Below in conjunction with accompanying drawing; by preferred embodiment, preferred forms of the present invention is described; the detailed description of the invention is here to explain the present invention; and should not be construed as limitation of the present invention; in the situation that not departing from spirit of the present invention and essential scope; can make various changes and modifications, within these all should be included in protection scope of the present invention.
Referring to Fig. 1-2, wherein show the ballistic parachute life saving system of the preferred embodiment of the present invention.This ballistic parachute life saving system comprises:
Parachute system, it comprises parachute lanyard 7, canopy 3, umbrella rope 9 and connecting band 6, and parachute lanyard 7 one end are connected with canopy 3 tops, canopy 3 Connectable umbrella rope 9 one end, base, umbrella rope 9 other ends are connected with connecting band 6 one end, and connecting band 6 other ends are connected with the upper end of following straphanger 12;
Rocket engine 5 systems, it comprises rocket socket and ignition device 4, wherein the other end of parachute lanyard 7 is connected with rocket socket; And
Hangar system, it comprises many straphangers 12, the lower end of wherein said straphanger 12 connects the sling point on aircraft 11.
Be understandable that, this system can start by the engine of rocket socket 5, can be used for crew's (comprising aircraft 11) to carry out lifesaving.For example this life saving system can be used for 1-2 seat hang glider, the gliding parachute of motor driving, the aircraft 11 of microlight-type, aerodone, test-type and the small-sized light-duty flying toy 11 of microlight-type.
Preferably, described system also comprises umbrella cabin 1, and described canopy 3 and umbrella rope 9 are arranged in umbrella cabin 1.
Preferably, also comprise the dress umbrella cover 8 being arranged in umbrella cabin 1, described canopy 3 and umbrella rope 9 are arranged in dress umbrella cover 8.
Preferably, described canopy 3 tops are sewed with umbrella top loop 10, and canopy 3 connects one end of described parachute lanyard 7 by described umbrella top loop 10.
Preferably, described ignition device 4 is connected with the engine 5 of described rocket socket.
Preferably, the upper end of described straphanger 12 is converged and is a bit connected with the other end of described connecting band 6.
Preferably, parachute lanyard 7 and connecting band 6 are arranged on outside umbrella cabin 1 and are positioned on the opposite side in umbrella cabin 1.
Preferably, rocket engine 5 systems are arranged on the sidewall in umbrella cabin 1.
Preferably, described umbrella cabin 1 is provided with openable protecgulum 2.
Preferably, described canopy 3 is arranged on the top of described umbrella rope 9.
In the time that aircraft 11 is in an emergency, aviator starts the ignition device 4 of rocket engine 5, the solid fuel of rocket engine 5 takes fire, rocket engine 5 is launched, progressively pull out canopy 3, umbrella rope 9 and straphanger 12 (being hoist cable) by parachute lanyard 7, hoist cable connects aircraft 11, and parachute is all opened, and parachute carries aircraft 11 safe fallings.Whole system working process and state are shown in Fig. 3-10.
Preferably, this ballistic parachute life saving system comprises parachute system, rocket engine 5 systems, hangar system.Parachute system can comprise parachute umbrella cabin 1, dress umbrella cover 8, canopy 3, umbrella rope 9, connecting band 6.Rocket engine 5 systems can comprise rocket socket, ignition device 4.Hangar system can be made up of four straphangers 12.
Preferably, can be sewed with umbrella top loop in parachute system on canopy 3, umbrella top loop connects parachute lanyard 7, umbrella rope 9 one end connect canopy 3 bases, and one end is connected with connecting band 6, for example, canopy 3, umbrella rope 9, connecting band 6 can be filled in umbrella cover 8 together like a cork, then be placed in three cabins.
Preferably, in rocket engine 5 systems, the in-built medicine of setting fire of rocket socket, is excited by ignition device 4.
Preferably, four straphangers of hangar system, 12 lower ends connect 11 4 sling points of aircraft, and upper end is converged a bit and is connected with connecting band 6.
Be understandable that, bell 3 links together by umbrella top loop 10 and parachute lanyard 7, parachute lanyard and rocket engine 5 link together, umbrella rope 9 one end are connected with bell 3 bases, the other end is connected with connecting band 6, connecting band 6 is connected with the straphanger 12 that is connected, and straphanger 12 is connected with aircraft 11, and ignition device 4 is connected with rocket engine 5.In the time that aircraft is in an emergency, aviator starts the ignition device of rocket engine, the solid fuel of rocket engine takes fire, rocket engine transmitting, progressively pull out canopy, umbrella rope and hoist cable by parachute lanyard, hoist cable connects aircraft, and parachute is all opened, and parachute carries aircraft security landing.
In sum, beneficial effect of the present invention is: in the time that aircraft is in an emergency, aviator starts the ignition device of rocket engine, the solid fuel of rocket engine takes fire, rocket engine transmitting, progressively pulls out canopy, umbrella rope and straphanger (being hoist cable) by parachute lanyard, and hoist cable connects aircraft, parachute is all opened, and parachute carries aircraft security landing.
The invention is not restricted to above-mentioned specific embodiment.These are understandable that, in the situation that not departing from spirit of the present invention and essential scope, can make various changes and modifications, within all should be included in protection scope of the present invention.
Claims (10)
1. a ballistic parachute life saving system, is characterized in that comprising:
Parachute system, it comprises parachute lanyard, canopy, umbrella rope and connecting band, parachute lanyard one end is connected with canopy top, Connectable umbrella rope one end, canopy base, the umbrella rope other end is connected with connecting band one end, and the connecting band other end is connected with the upper end of following straphanger;
Rocket engine system, it comprises rocket socket and ignition device, wherein the other end of parachute lanyard is connected with rocket socket; And
Hangar system, it comprises many straphangers, the lower end of wherein said straphanger connects carry-on sling point.
2. ballistic parachute life saving system according to claim 1, characterized by further comprising umbrella cabin, and described canopy and umbrella rope are arranged in umbrella cabin.
3. ballistic parachute life saving system according to claim 1 and 2, characterized by further comprising the dress umbrella cover being arranged in umbrella cabin, and described canopy and umbrella rope are arranged in dress umbrella cover.
4. ballistic parachute life saving system according to claim 1 and 2, is characterized in that described canopy top is sewed with umbrella top loop, and canopy connects one end of described parachute lanyard by described umbrella top loop.
5. ballistic parachute life saving system according to claim 1 and 2, is characterized in that described ignition device is connected with the engine of described rocket socket.
6. ballistic parachute life saving system according to claim 1 and 2, the upper end that it is characterized in that described straphanger is converged a bit and is connected with the other end of described connecting band.
7. ballistic parachute life saving system according to claim 1 and 2, is characterized in that parachute lanyard and connecting band are arranged on umbrella out of my cabin and are positioned on the opposite side in umbrella cabin.
8. ballistic parachute life saving system according to claim 3, is characterized in that rocket engine system is arranged on the sidewall in umbrella cabin.
9. ballistic parachute life saving system according to claim 3, is characterized in that described umbrella cabin is provided with openable protecgulum.
10. ballistic parachute life saving system according to claim 1 and 2, is characterized in that described canopy is arranged on the top of described umbrella rope.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410232222.6A CN103979110A (en) | 2014-05-29 | 2014-05-29 | Ballistic parachute life-saving system |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410232222.6A CN103979110A (en) | 2014-05-29 | 2014-05-29 | Ballistic parachute life-saving system |
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| CN103979110A true CN103979110A (en) | 2014-08-13 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201410232222.6A Pending CN103979110A (en) | 2014-05-29 | 2014-05-29 | Ballistic parachute life-saving system |
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Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106809396A (en) * | 2017-02-28 | 2017-06-09 | 中航维拓（天津）科技有限公司 | A kind of rotor craft parachuting device of use gas generant composition in accordance |
| CN107826257A (en) * | 2017-09-08 | 2018-03-23 | 中国飞行试验研究院 | One kind penetrates umbrella big gun and parachute deployment means |
| CN107953999A (en) * | 2017-12-25 | 2018-04-24 | 襄阳宏伟航空器有限责任公司 | It is a kind of to penetrate umbrella rocket means for the quick parachute-opening of parachute |
| CN109204835A (en) * | 2018-10-18 | 2019-01-15 | 五邑大学 | A kind of sounding rocket parachute opener of burn-out proof |
| CN109398765A (en) * | 2018-11-23 | 2019-03-01 | 襄阳宏伟航空器有限责任公司 | A kind of emitter and its application method suitable for penetrating umbrella rocket |
| CN109552653A (en) * | 2018-11-29 | 2019-04-02 | 江苏鸿鹄无人机应用科技有限公司 | A kind of emission type unmanned plane |
| CN111169645A (en) * | 2018-11-12 | 2020-05-19 | 中航通飞研究院有限公司 | Reverse tail rotation device of airplane |
| CN111263723A (en) * | 2017-08-30 | 2020-06-09 | 日本化药株式会社 | Flying body |
| WO2022031377A3 (en) * | 2020-06-23 | 2022-06-09 | Boris Popov | Aircraft emergency parachute deployment system |
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| CN203865005U (en) * | 2014-05-29 | 2014-10-08 | 襄阳宏伟航空器有限责任公司 | Ballistic-trajectory-type parachute lifesaving system |
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Cited By (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106809396A (en) * | 2017-02-28 | 2017-06-09 | 中航维拓（天津）科技有限公司 | A kind of rotor craft parachuting device of use gas generant composition in accordance |
| CN111263723A (en) * | 2017-08-30 | 2020-06-09 | 日本化药株式会社 | Flying body |
| CN111263723B (en) * | 2017-08-30 | 2023-05-23 | 日本化药株式会社 | Flying body |
| CN107826257A (en) * | 2017-09-08 | 2018-03-23 | 中国飞行试验研究院 | One kind penetrates umbrella big gun and parachute deployment means |
| CN107953999A (en) * | 2017-12-25 | 2018-04-24 | 襄阳宏伟航空器有限责任公司 | It is a kind of to penetrate umbrella rocket means for the quick parachute-opening of parachute |
| CN109204835A (en) * | 2018-10-18 | 2019-01-15 | 五邑大学 | A kind of sounding rocket parachute opener of burn-out proof |
| CN109204835B (en) * | 2018-10-18 | 2023-09-08 | 五邑大学 | Anti-ablation sounding rocket parachute opening device |
| CN111169645A (en) * | 2018-11-12 | 2020-05-19 | 中航通飞研究院有限公司 | Reverse tail rotation device of airplane |
| CN111169645B (en) * | 2018-11-12 | 2023-12-01 | 中航通飞研究院有限公司 | Reverse tail-spinning device of airplane |
| CN109398765A (en) * | 2018-11-23 | 2019-03-01 | 襄阳宏伟航空器有限责任公司 | A kind of emitter and its application method suitable for penetrating umbrella rocket |
| CN109398765B (en) * | 2018-11-23 | 2024-04-19 | 襄阳宏伟航空器有限责任公司 | Launching device suitable for parachute-shooting rocket and using method thereof |
| CN109552653A (en) * | 2018-11-29 | 2019-04-02 | 江苏鸿鹄无人机应用科技有限公司 | A kind of emission type unmanned plane |
| WO2022031377A3 (en) * | 2020-06-23 | 2022-06-09 | Boris Popov | Aircraft emergency parachute deployment system |
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Application publication date: 20140813 |