CN203865005U - Ballistic-trajectory-type parachute lifesaving system - Google Patents
Ballistic-trajectory-type parachute lifesaving system Download PDFInfo
- Publication number
- CN203865005U CN203865005U CN201420280648.4U CN201420280648U CN203865005U CN 203865005 U CN203865005 U CN 203865005U CN 201420280648 U CN201420280648 U CN 201420280648U CN 203865005 U CN203865005 U CN 203865005U
- Authority
- CN
- China
- Prior art keywords
- parachute
- umbrella
- canopy
- ballistic
- aircraft
- 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.)
- Active
Links
Abstract
A ballistic-trajectory-type parachute lifesaving system comprises a parachute system, a rocket engine system and a hanging system, wherein the parachute system comprises a parachute opening pull cord, a parachute canopy, a parachute cord and a connecting band, one end of the parachute opening pull cord is connected with the top of the parachute canopy, the bottom side of the parachute canopy is connected with one end of the parachute cord, the other end of the parachute cord is connected with one end of the connecting band, and the other end of the connecting band is connected with the upper ends of hanging bands; the rocket engine system comprises a rocket launcher and an igniting device, and the other end of the parachute opening pull cord is connected with the rocket launcher; the hanging system comprises the multiple hanging bands, and the lower ends of the hanging bands are connected to an aircraft. The system can be used for lifesaving of flight crew and aircraft through an engine starter of the rocket launcher. For example, the lifesaving system can be used for a hang glider with one to two seats, a paraglider driven by a motor, a super-light aircraft, a super-light glider, and an experimental-type, small-size and light movement aircraft.
Description
Technical field
The utility model relates to life saving system field, particularly, relates 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 a plurality of column gas bundles, a plurality of 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, by the high-pressure aerated pipe with unidirectional charge valve, are communicated with.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, for crowd when the disaster scenarios it such as earthquake, fire occur escapes to be rescued on high-rise building, provides a kind of new mode.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.
Yet, modern aircraft is more and more, especially the gliding parachute driving at 1-2 seat hang glider, motor, the aircraft of microlight-type, the development of the aspects such as the aerodone of microlight-type, test-type and small-sized light-duty flying toy are maked rapid progress especially, but when there is emergency in aircraft or aviator, cannot escape danger, occur fatal crass's situation.Be below several emergency situations that easily occur:
1) in the time of above rugged landform, the engine has gone wrong, during impossible safe landing;
2) aircraft get out of hand: i) because technological deficiency; Ii) weather condition is severe, loses pilotage and controls; Iii) because losing pilotage, other reasons controls;
3), because of aviator's health problem, make it can not continue safe flight (for example, heart attack etc.);
4) because severe meteorological conditions makes aviator, lose sense of direction, 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.
Utility model content
Considers at least one the problems referred to above and completed the utility model, and an object of the present utility model 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 on aircraft.
That is to say, this system can, 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 gliding parachute, the aircraft of microlight-type, the aerodone of microlight-type, test-type and the small-sized light-duty flying toy of 1-2 seat hang glider, motor driving.
According to the utility model on the other hand, described system also comprises umbrella cabin, and described canopy and umbrella rope are arranged in umbrella cabin.
According to the utility model on the other hand, also comprise the dress umbrella cover being arranged in umbrella cabin, described canopy and umbrella rope are arranged in dress umbrella cover.
According to the utility model on the other hand, 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 the utility model on the other hand, described ignition device is connected with the engine of described rocket socket.
According to the utility model on the other hand, the upper end of described straphanger is converged and is a bit connected with the other end of described connecting band.
According to the utility model on the other hand, 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 the utility model on the other hand, rocket engine system is arranged on the sidewall in umbrella cabin.
According to the utility model on the other hand, described umbrella cabin is provided with openable protecgulum.
According to the utility model on the other hand, described canopy is arranged on the top of described umbrella rope.
Compared with prior art, the beneficial effects of the utility model are: when 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.
Accompanying drawing explanation
Fig. 1 is according to the structural representation of the ballistic parachute life saving system of the utility model preferred embodiment.
Fig. 2 is according to the ballistic parachute life saving system of the utility model preferred embodiment and the connection diagram of aircraft.
Fig. 3-10th, according to real work flow process and the view of the ballistic parachute life saving system of the utility model preferred embodiment.
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
The specific embodiment
Below in conjunction with accompanying drawing; by preferred embodiment, preferred forms of the present utility model is described; the specific embodiment is here to explain the utility model; and should not be construed as restriction of the present utility model; in the situation that not departing from spirit of the present utility model and essential scope; can make various changes and modifications, within these all should be included in protection domain of the present utility model.
Referring to Fig. 1-2, wherein show the ballistic parachute life saving system of the utility model preferred embodiment.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 on aircraft 11.
Be understandable that, this system can start by the engine 5 of rocket socket, can be used for crew's (comprising aircraft 11) to carry out lifesaving.For example this life saving system can be used for gliding parachute, the aircraft 11 of microlight-type, the aerodone of microlight-type, test-type and the small-sized light-duty flying toy 11 of 1-2 seat hang glider, motor driving.
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.
When 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 transmittings, by parachute lanyard 7, progressively pull out canopy 3, umbrella rope 9 and straphanger 12 (being hoist cable), 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 comprised 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.When aircraft is in an emergency, aviator starts the ignition device of rocket engine, the solid fuel of rocket engine takes fire, rocket engine transmitting, by parachute lanyard, progressively pull out canopy, umbrella rope and hoist cable, hoist cable connects aircraft, and parachute is all opened, and parachute carries aircraft security landing.
In sum, the beneficial effects of the utility model are: when 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 utility model is not limited to above-mentioned specific embodiment.These are understandable that, in the situation that not departing from spirit of the present utility model and essential scope, can make various changes and modifications, within all should be included in protection domain of the present utility model.
Claims (9)
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 on aircraft.
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 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 3, 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 4, 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 5, is characterized in that described canopy is arranged on the top of described umbrella rope.
7. ballistic parachute life saving system according to claim 6, 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 7, is characterized in that rocket engine system is arranged on the sidewall in umbrella cabin.
9. ballistic parachute life saving system according to claim 8, is characterized in that described umbrella cabin is provided with openable protecgulum.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420280648.4U CN203865005U (en) | 2014-05-29 | 2014-05-29 | Ballistic-trajectory-type parachute lifesaving system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420280648.4U CN203865005U (en) | 2014-05-29 | 2014-05-29 | Ballistic-trajectory-type parachute lifesaving system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203865005U true CN203865005U (en) | 2014-10-08 |
Family
ID=51645985
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420280648.4U Active CN203865005U (en) | 2014-05-29 | 2014-05-29 | Ballistic-trajectory-type parachute lifesaving system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203865005U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103979110A (en) * | 2014-05-29 | 2014-08-13 | 襄阳宏伟航空器有限责任公司 | Ballistic parachute life-saving system |
| 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 |
| CN104691788A (en) * | 2015-01-23 | 2015-06-10 | 北京空间机电研究所 | Pop-up parachute capable of realizing self-adaptive equilibrium |
-
2014
- 2014-05-29 CN CN201420280648.4U patent/CN203865005U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103979110A (en) * | 2014-05-29 | 2014-08-13 | 襄阳宏伟航空器有限责任公司 | Ballistic parachute life-saving system |
| 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 |
| CN104691788A (en) * | 2015-01-23 | 2015-06-10 | 北京空间机电研究所 | Pop-up parachute capable of realizing self-adaptive equilibrium |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN103979110A (en) | Ballistic parachute life-saving system | |
| CN203865005U (en) | Ballistic-trajectory-type parachute lifesaving system | |
| CN104890851A (en) | Near space balloon system safety release method | |
| US10005559B2 (en) | Crash-resistant aircraft and crash-resistant control method | |
| CN108163179B (en) | Near space aerostat issuing method and apparatus | |
| CN1962362A (en) | Light airplane safe life-saving system | |
| CN101767651A (en) | Low altitude lifesaving parachute | |
| CN101148198A (en) | Danger preventing airborne escaping method in civil airline passenger cabin ejected out the plane | |
| WO2010127562A2 (en) | Escaping cabin aeroplane | |
| CN106043710A (en) | Aerial pilotless manned escaping device | |
| CN209126987U (en) | Platform-type jet runway | |
| CN206485578U (en) | A kind of high-altitude intelligent escape device | |
| CN206984402U (en) | A kind of multirotor helicopter security system | |
| CN104071339A (en) | Rocket backpack for realizing landing by using jet propulsion system | |
| CN205044935U (en) | Emergent air bleeder of aerostatics and aerostatics | |
| CN203567936U (en) | Flight anchor-hanging rescue device | |
| RU2021164C1 (en) | Airbus | |
| CN204096089U (en) | Helicopter escape system and escape employment are with rushing umbrella big gun and helicopter with rushing umbrella big gun | |
| CN202657248U (en) | secape system | |
| CN111589016A (en) | High-altitude aviation fire extinguishing and disaster relief system | |
| CN218288140U (en) | Multi-state aerial emergency ejection life-saving parachute device | |
| RU163251U1 (en) | DEVICE FOR HELICOPTER EXTERNAL SUSPENSION FOR MOUNTING AN UNMANNED AIRPLANE | |
| CN202896868U (en) | Direction controllable lowering device | |
| RU2753735C1 (en) | Amphibious life raftcomplexes | |
| CN102068765A (en) | High-rise lifesaving method |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |