CN206485578U - A kind of high-altitude intelligent escape device - Google Patents
A kind of high-altitude intelligent escape device Download PDFInfo
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- CN206485578U CN206485578U CN201720136632.XU CN201720136632U CN206485578U CN 206485578 U CN206485578 U CN 206485578U CN 201720136632 U CN201720136632 U CN 201720136632U CN 206485578 U CN206485578 U CN 206485578U
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- sealed compartment
- manned
- ejection
- manned sealed
- automatic control
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Abstract
A kind of high-altitude intelligent escape device, aircraft is arranged on including on aircraft, helicopter, skyscraper, high mountain climb the mountain work high above the ground environmentally, when there is emergency risks state, including aircraft it is out of control, blast, skyscraper, high tower occur fire, earthquake and decayed, in the case of high landslide snow, quick ejection departs from aircraft body or high vacant building, personal safety landing ground or the water surface are reached, the utility model device is made up of manned sealed compartment, parachute, driver, automatic control system and external ejection system.
Description
Technical field
The utility model is related to a kind of escape device skill of use under aircraft, skyscraper, the aerial precarious position of high mountain
Art.
Background technology
Current aircarrier aircraft is no launch escape system in high-altitude flight, only military aircraft particularly fighter flight
Just escape device is launched in configuration to member.
The content of the invention
The utility model can independently launch the overhead escape device of separation by a kind of, and being arranged on aircraft includes flying
On machine, helicopter, environmentally, when there is emergency risks state, including aircraft loses for the work high above the ground climbed the mountain in skyscraper, high mountain
Control, blast, skyscraper, high tower occur fire, earthquake and decayed, and in the case of high landslide snow, quick ejection departs from aircraft body
Or high vacant building, reach personal safety landing ground or the water surface.
In order to solve the above-mentioned technical problem, the utility model employs following technical scheme：
A kind of high-altitude intelligent escape device, by manned sealed compartment 1, parachute 2, driver 3, automatic control system 4 and outer
Ejection system 5 is put to constitute；
The utility model device is arranged in aircraft 6, and its manned sealed compartment 1 is explosion-proof, waterproof alloy shell, is matched somebody with somebody
Pressure-adjustable in hatch door 11, built-in inversion-prevention, shock proof seat 12, cabin, temperature adjustment, weightless balance are put, bottom sets driver 3, top
External parachute 2, the shell shape of the manned sealed compartment 1 can design various shapes, including spheroidal, cone as needed
Or it is oval spherical, its volume can designed size as needed, the seat of one people of loading or many people can be set in the manned sealed compartment 1
Chair 12；In the secure state, the utility model device is fixedly installed on cabin in aircraft 6 and not started, and when there is state of necessity, leads to
Cross automatic control system 4 and start external ejection system 5, ejected by departing from outlet 61, depart from the main body of aircraft 6, in manned sealing
While cabin 1 is ejected, automatic control system 4 starts driver 3 simultaneously；The parachute 2 shrinks folding when safety is not opened
At the manned top of sealed compartment 1；
The driver 3 is arranged on the manned bottom of sealed compartment 1, is fixedly connected all the time with manned sealed compartment 1, the driver
3 configurations include cabin seat 31, engine 32, hydraulically extensible bar 33, generator 34, compressor 35, battery and Bunker equipment；
The driver 3 can use storage battery power supply, fuel oil, or be used as power raw material using cooling liquid hydrogen, oxygen, nitrogen；It is described from
Autocontrol system 4 is arranged on the manned inner bottom part of sealed compartment 1, under precarious position, passes through the automatic sensing device of automatic control system 4
Send distress signal, after escape personnel, which enters manned sealed compartment 1, is closing hatch door 11, automatic control system 4 starts external
Ejection system promotes manned sealed compartment 1 to be ejected safely in optimal orientation, angle and speed within 5,20 seconds, stretched while opening hydraulic pressure
Contracting bar 33, start engine 32, and according to ground, water surface elevation distance, open parachute 2 automatically in good time, constantly regulate is driven
Dynamic device 3, makes manned sealed compartment 1 remain at safe uniform descent, and avoids the barrier that is run into when declining, at 1,000 meter
The high space-time of the above, automatic control system 4 adjusts engine by inductor and keeps manned sealed compartment 1 with the speed of 15 meter per seconds
Drop, the high space-time within 5,000 meters, parachute 2 opens, keep manned sealed compartment 1 with the speed within 11 meter per seconds it is steady under
Drop, and ground obstacle safe landing or safe falling are avoided on the water surface；The automatic control system 4, while auto-control
Stall, pressure, temperature, gravity balance and the landing of manned sealed compartment 1, and keep the wireless communication with ground to contact；It is described from
Autocontrol system 4 is provided with positioning signal instrument, can be carried out by GPS, the Big Dipper, Galileo or GLONASS satellite system comprehensive
Monitoring, tracking, regulation and control；
The external ejection system 5 is arranged on the manned outer bottom of sealed compartment 1, former using cooling liquid state nitrogen as ejection power
Material, sets multigroup canned cooling liquid state nitrogen 5A, and temperature reaches -195.8 DEG C, and normality natural heating is at -20---+30 DEG C during startup
Cooling liquid state nitrogen is discharged, impulsive force of the allowance for expansion moment more than more than 600 times is formed, by multigroup jet 5B around opposite
The manned base injcction of sealed compartment 1, produces reaction force and ejects manned sealed compartment 1, separated with the main body of aircraft 6；Described is outer
Putting ejection system 5 can be using cooling liquid hydrogen, oxygen as ejection power raw material；
The aircraft 6 includes that civil aviaton is large-scale, baby plane, helicopter.
As the further improvement of above-mentioned technical proposal, a kind of high-altitude intelligent escape device, except may be provided at flight
Outside device 6, it can also be provided on skyscraper 7, high tower, overpass or high mountain, the utility model device can be set multigroup, can return
Receive multiple Reusability.
As the further improvement of above-mentioned technical proposal, a kind of high-altitude intelligent escape device may be selected to be nobody and drive
Sail, escape personnel manipulates in manned sealed compartment 1, or ground staff's remote control；Can be without using parachute 2 and external ejection system 5, directly
Connect and complete ejection lift-off, flight, decline process using driver 3.
The beneficial effects of the utility model are：Before aircraft air crash, skyscraper decay before, collapse mountain, floods dangerous situation occur
When, use the even whole people's safe escapes of present apparatus implementation section personnel.
Brief description of the drawings
Fig. 1 is the utility model schematic device.
Fig. 2 is manned sealed compartment and activation configuration schematic diagram.
Fig. 3 is external ejection system structural representation.
Fig. 4 is that the utility model device is arranged on carry-on ejection schematic diagram.
Fig. 5 is that the utility model device is arranged on the architectural schematic diagram in high-altitude.
Embodiment
Refering to Fig. 1-Fig. 5, a kind of high-altitude intelligent escape device, by manned sealed compartment 1, parachute 2, driver 3, automatic control
System 4 processed and external ejection system 5 are constituted；
The utility model device is arranged in aircraft 6, and its manned sealed compartment 1 is explosion-proof, waterproof alloy shell, is matched somebody with somebody
Pressure-adjustable in hatch door 11, built-in inversion-prevention, shock proof seat 12, cabin, temperature adjustment, weightless balance are put, bottom sets driver 3, top
External parachute 2, the shell shape of the manned sealed compartment 1 can design various shapes, including spheroidal, cone as needed
Or it is oval spherical, its volume can designed size as needed, the seat of one people of loading or many people can be set in the manned sealed compartment 1
Chair 12；In the secure state, the utility model device is fixedly installed on cabin in aircraft 6 and not started, and when there is state of necessity, leads to
Cross automatic control system 4 and start external ejection system 5, ejected by departing from outlet 61, depart from the main body of aircraft 6, in manned sealing
While cabin 1 is ejected, automatic control system 4 starts driver 3 simultaneously；The parachute 2 shrinks folding when safety is not opened
At the manned top of sealed compartment 1；
The driver 3 is arranged on the manned bottom of sealed compartment 1, is fixedly connected all the time with manned sealed compartment 1, the driver
3 configurations include cabin 31, engine 32, hydraulically extensible bar 33, generator 34, compressor 35, battery and Bunker equipment；Institute
Storage battery power supply, fuel oil can be used by stating driver 3, or be used as power raw material using cooling liquid hydrogen, oxygen, nitrogen；It is described automatic
Control system 4 is arranged on the manned inner bottom part of sealed compartment 1, under precarious position, is sent out by the automatic sensing device of automatic control system 4
Go out danger signal, after escape personnel, which enters manned sealed compartment 1, is closing hatch door 11, automatic control system 4 starts external bullet
System, which is penetrated, within 5,20 seconds promotes manned sealed compartment 1 to orient safe ejection, while opening hydraulically extensible bar 33, starting engine
32, and according to ground, water surface elevation distance, open parachute 2 automatically in good time, constantly regulate driver 3 makes manned sealed compartment
1 remains at safe uniform descent, and avoids the barrier that is run into when declining, and the high space-time more than 1,000 meter is automatically controlled
System 4 is adjusted engine 32 by inductor and keeps manned sealed compartment 1 to be declined with the speed of 15 meter per seconds, high within 5,000 meters
Space-time, parachute 2 opens, and keeps manned sealed compartment 1 steadily to decline with the speed within 11 meter per seconds, and avoid ground obstacle
Safe landing or safe falling are on the water surface；The automatic control system 4, while the stall of the manned sealed compartment 1 of auto-control, pressure
Power, temperature, gravity balance and landing, and keep the wireless communication with ground to contact；The automatic control system 4 is provided with positioning
Bashertron, can carry out conduct monitoring at all levels, tracking, regulation and control by GPS, the Big Dipper, Galileo or GLONASS satellite system；
The external ejection system 5 is arranged on the manned outer bottom of sealed compartment 1, former using cooling liquid state nitrogen as ejection power
Material, sets multigroup canned cooling liquid state nitrogen 5A, and temperature reaches -195.8 DEG C, and normality natural heating is at -20---+30 DEG C during startup
Cooling liquid state nitrogen is discharged, impulsive force of the allowance for expansion moment more than more than 600 times is formed, by multigroup jet 5B around opposite
The manned base injcction of sealed compartment 1, produces reaction force and ejects manned sealed compartment 1, separated with the main body of aircraft 6；Described is outer
Putting ejection system 5 can be using cooling liquid hydrogen, oxygen as ejection power raw material；
The aircraft 6 includes that civil aviaton is large-scale, baby plane, helicopter.
It is further used as preferred embodiment, a kind of high-altitude intelligent escape device, except may be provided at aircraft 6
Outside, can also be provided on skyscraper 7, high tower, overpass or high mountain, the utility model device can be set it is multigroup, it is recyclable many
Secondary Reusability.
It is further used as preferred embodiment, a kind of high-altitude intelligent escape device, may be selected to be unmanned, load
Escape personnel manipulates in people's sealed compartment 1, or ground staff's remote control；Can directly it make without using parachute 2 and external ejection system 5
Ejection lift-off, flight are completed with driver 3, decline process.
Embodiment one：Refering to Fig. 1-Fig. 4, on large-scale aircarrier aircraft using multigroup parachute construction configure, apply away from
1,000 meter -10 from the ground, 000 meter of high-altitude, many people's seats built in loading sealed compartment make during for flight attendant danger and disaster in need
With.Every group of parachute construction configuration, the small-sized turbofan for the 2-4 bench-types WS500 that its driver is developed using boat group of China one
Engine, every thrust magnitude is 500KGF.
Embodiment two：Refering to Fig. 1-Fig. 4, using one group of parachute construction configuration on baby plane or helicopter, it drives
Dynamic device configures 2 bench-type WS500 engines.Apply apart from -10,000 meters of high-altitudes in 200 meters of ground.One built in manned sealed compartment
People or many people's seats, are used during danger and disaster for part or all of flight attendant.
Embodiment three：Refering to Fig. 2, Fig. 3, Fig. 5, in skyscraper more than 30 buildings, or it is more than 80 meters high empties, for example high
Use, configured using one or more groups of non-parachutes, a people built in manned sealed compartment or many people's seats, in danger and disaster on tower, high mountain
When be provided with and need people to use.Every group of manned sealed compartment, its driver uses 4 bench-type WS300-700 fanjets, and every pushes away
Strength level is 300-700KGF.
Example IV：Refering to Fig. 2, using a kind of high-altitude intelligent escape device, without using configuration parachute and external ejection
System, equivalent to a manned aircraft of frame individual small, may participate in 3,000 meter of various flight with inner height speedily carry out rescue work rescue people operation.
Although being described in conjunction with the accompanying embodiment of the present utility model, it should be noted that those skilled in the art can
So that various changes and modifications can be made within appended interest field, as long as described by not excess of export claim excessively of the present utility model
Protection domain, all should be within protection domain of the present utility model.
Claims (3)
1. a kind of high-altitude intelligent escape device, by manned sealed compartment（1）, parachute（2）, driver（3）, automatic control system
（4）With external ejection system（5）Composition；
Described device is arranged on aircraft（6）It is interior, its manned sealed compartment（1）It is explosion-proof, waterproof alloy shell, configures hatch door
（11）, built-in inversion-prevention, shock proof seat（12）, pressure-adjustable, temperature adjustment, weightless balance in cabin, bottom sets driver（3）, top
External parachute（2）, the manned sealed compartment（1）Shell shape can design various shapes, including spheroidal, circle as needed
Taper is oval spherical, and its volume can designed size, the manned sealed compartment as needed（1）Interior settable loading one people or many
The seat of people；In the secure state, described device is fixedly installed on aircraft（6）Interior cabin does not start, and when there is state of necessity, leads to
Cross automatic control system（4）Start external ejection system（5）, manned sealed compartment（1）By departing from outlet（61）Ejection, departs from flight
Device（6）Main body, in manned sealed compartment（1）While ejection, automatic control system（4）Start driver 3 simultaneously；The parachute
（2）Shunk when safety is not opened and be folded in manned sealed compartment（1）Top；
The driver（3）It is arranged on manned sealed compartment（1）Bottom, all the time with manned sealed compartment（1）It is fixedly connected, the driving
Device（3）Configuration includes cabin seat（31）, engine（32）, hydraulically extensible bar（33）, generator（34）, compressor（35）, electric power storage
Pond and Bunker equipment；The driver（3）Storage battery power supply, fuel oil can be used, or is made using cooling liquid hydrogen, oxygen, nitrogen
For power raw material；The automatic control system（4）It is arranged on manned sealed compartment（1）Inner bottom part, under precarious position, by automatic
Control system（4）Automatic sensing device send distress signal, when escape personnel enter manned sealed compartment（1）Closing hatch door（11）
Afterwards, automatic control system（4）Start external ejection system（5）, promote manned sealed compartment 1 at optimal orientation, angle within 20 seconds
Degree and speed are ejected safely, while opening hydraulically extensible bar（33）, start engine（32）, and according to ground, water surface elevation
Distance, opens parachute automatically in good time（2）, constantly regulate driver（3）, make manned sealed compartment（1）Remain at safety even
Speed declines, and the barrier that runs into, high space-time, automatic control system more than 1,000 meter when avoiding declining（4）Pass through inductor
Adjust engine and keep manned sealed compartment（1）Declined with the speed of 15 meter per seconds, high space-time, parachute within 5,000 meters（2）
Open, keep manned sealed compartment（1）Steadily declined with the speed within 11 meter per seconds, and avoid ground obstacle safe landing or
Safe falling is on the water surface；The automatic control system（4）, while the manned sealed compartment of auto-control（1）Stall, pressure, temperature
Degree, gravity balance and landing, and keep the wireless communication with ground to contact；The automatic control system（4）There is provided positioning letter
Number instrument, can pass through GPS, the Big Dipper, Galileo or GLONASS satellite system and carry out conduct monitoring at all levels, tracking, regulate and control；
The external ejection system（5）It is arranged on manned sealed compartment（1）Outer bottom, it is former using cooling liquid state nitrogen as ejection power
Material, sets multigroup canned cooling liquid state nitrogen（5A）, temperature reaches -195.8 DEG C, and normality natural heating is in -20---+30 during startup
DEG C release cooling liquid state nitrogen, formed impulsive force of the allowance for expansion moment more than more than 600 times, pass through multigroup jet（5B）It surround
Against manned sealed compartment（1）Base injcction, produces reaction force by manned sealed compartment（1）Ejection, with aircraft（6）Main body point
From；Described external ejection system（5）Ejection power raw material can be used as using cooling liquid hydrogen, oxygen；
The aircraft（6）Including civil aviaton is large-scale, baby plane, helicopter.
2. a kind of high-altitude intelligent escape device according to claim 1, it is characterised in that：Described device, it is winged except may be provided at
Row device（6）Outside, it can also be provided at skyscraper（7）, high tower, on overpass or high mountain, described device can be set it is multigroup, it is recyclable
Multiple Reusability.
3. a kind of high-altitude intelligent escape device according to claim 1, it is characterised in that：Described device, may be selected to be nobody
Drive, manned sealed compartment（1）Interior escape personnel's manipulation, or ground staff's remote control；Can be without using parachute（2）With external ejection system
System（5）, directly using driver（3）Complete ejection lift-off, flight, decline process.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720136632.XU CN206485578U (en) | 2017-02-15 | 2017-02-15 | A kind of high-altitude intelligent escape device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720136632.XU CN206485578U (en) | 2017-02-15 | 2017-02-15 | A kind of high-altitude intelligent escape device |
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| Publication Number | Publication Date |
|---|---|
| CN206485578U true CN206485578U (en) | 2017-09-12 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720136632.XU Expired - Fee Related CN206485578U (en) | 2017-02-15 | 2017-02-15 | A kind of high-altitude intelligent escape device |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112141346A (en) * | 2019-06-28 | 2020-12-29 | 马建成 | Totally-enclosed foldable airliner air escape waiting device |
| CN113997896A (en) * | 2021-10-09 | 2022-02-01 | 易显智能科技有限责任公司 | Automobile for guaranteeing safety of passengers |
-
2017
- 2017-02-15 CN CN201720136632.XU patent/CN206485578U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112141346A (en) * | 2019-06-28 | 2020-12-29 | 马建成 | Totally-enclosed foldable airliner air escape waiting device |
| CN113997896A (en) * | 2021-10-09 | 2022-02-01 | 易显智能科技有限责任公司 | Automobile for guaranteeing safety of passengers |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170912 Termination date: 20190215 |
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| CF01 | Termination of patent right due to non-payment of annual fee |