CN202314999U - Ejection type high-rise life saving dropping system - Google Patents
Ejection type high-rise life saving dropping system Download PDFInfo
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- CN202314999U CN202314999U CN2011204412110U CN201120441211U CN202314999U CN 202314999 U CN202314999 U CN 202314999U CN 2011204412110 U CN2011204412110 U CN 2011204412110U CN 201120441211 U CN201120441211 U CN 201120441211U CN 202314999 U CN202314999 U CN 202314999U
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- life saving
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Abstract
The utility model discloses an ejection type high-rise life saving dropping system, which comprises an ejection frame and a seat which a parachute is installed on. A guide rail in sliding match with the seat is arranged on the ejection frame, the guide rail is provided with an elevation on a horizontal plane, a boosting device for driving the seat to move along the guide rail and enable the seat to break away from the guide rail and to be ejected at high speed towards the inclined upward side is arranged between the seat and the ejection frame, and a safety belt is arranged on the seat. When the ejection type high-rise life saving dropping system is in use, the seat for bearing escape personnel is ejected towards the inclined upward side along the guide rail on the ejection frame through the boosting device. On one hand, the parachute opening height is increased, and the problem of insufficient height of parachute opening at low altitude in the prior art is solved; on the other hand, the horizontal distance generated by the ejection can enable the escape personnel to be far away from buildings, prevent the parachute in dropping from meeting flame sprayed out of buildings and prevent the parachute from being disturbed by fire airflows and building wind. Therefore, the safety of the escape personnel is effectively improved.
Description
Technical field
The utility model relates to a kind of high-rise building life saving system, and definite saying so relates to a kind of ejection type high-rise building life saving parachuting system.
Background technology
What existing high building lifesaving parachute mainly adopted is hook parachute-opening mode, promptly utilizes fixing hook on the wall when jumping, to force to draw back parachute.But because that human body jumps is limited in one's ability, can't be when therefore landing away from the exterior wall of high building, inevitable very near apart from the external wall in building after parachute is opened, if when high building lower floor fire is violent, flare is scurried out outside the building, and the parachute that ignites easily causing the escape failure.Chinese patent open file CN100402112C discloses a kind of parachute rescue system of skyscraper; This rescue system comprises parachute and seat; Seat is suspended on the guide rail that is obliquely installed; Seat makes the escape personnel who is sitting on the seat obtain bigger second cosmic velocity through escape personnel's the weight and the acceleration of gravity of self gravitation formation in slip on the guide rail, thereby makes the escape personnel away from building.But this parachute rescue system is to guarantee to have enough speed when the escape personnel breaks away from, and it need be at the long guide rail of indoor setting, and volume is bigger; Therefore need take bigger space, be inappropriate in the less building in spaces such as office tower, residential building and using, and adopt this guide rail to quicken to cast aside mode; Need use at higher floor, it uses at lower floor can quicken escape personnel's falling speed on the contrary, reduces deployment time; Increase the difficulty of escape; In addition, if run into bigger contrary wind when casting aside, speed when this mode of utilizing acceleration of gravity to glide is easy to reduce the escape personnel and glides; Reduce escape personnel's the distance of casting aside, influence escape personnel's safe escape.
The utility model content
The purpose of the utility model is: a kind of ejection type high-rise building life saving parachuting system with elevation angle is provided; Through assist device is that escape compartment provides bigger initial velocity and the opening altitude of launching; Existing high building parachute is low because of opening altitude to solve, second cosmic velocity is little is caused the problem of escape failure easily by the influence of bottom flame, thereby improves the success rate of high-rise building life saving.
The technical scheme of the utility model is: a kind of ejection type high-rise building life saving parachuting system; Comprise launching cradle and escape compartment; Escape compartment is provided with seat and is equipped with the parachuting device, and seat is provided with safety belt, on said launching cradle, is provided with the guide rail that is slidingly matched with this escape compartment guiding; This guide rail has the elevation angle on horizontal plane, between escape compartment and launching cradle, be equipped with to drive escape compartment along guide rail moves and final getaway ejects at a high speed to oblique upper assist device.
Described escape compartment is made up of seat that cooperates with the guide rail guiding and the protection hatchcover that is located at outside the seat, and described parachute is installed on seat or the protection hatchcover.
Described assist device comprises the ejection guns that is fixed on the launching cradle and is installed in the bullet that launches in the ejection guns that the front end and the seat that launch bullet are connected, and are provided with in the bottom of ejection guns to be used for launching the gases at high pressure generating means that bullet is released.
Described gases at high pressure generating means is the powder burning device that is installed in the ejection guns.
Described gases at high pressure generating means is the gas cylinder that is connected the ejection guns bottom.
Bottom at said seat also is equipped with rocket booster.
Mainly be made up of parachute and parachute opener at said parachuting device, described parachute opener is for the power parachute opener of automatic or manual switch control or by the forced parachute opening device of deciding power fixed length line traffic control.
Also be provided with by the control of automatic or manual switch or by the landing buffer unit of deciding power fixed length line traffic control in the bottom of seat; This landing buffer unit comprises aerating device and buffering pneumatic cushion, is receiving the gas bleeder valve of opening automatically after the ground shock being provided with on the buffering pneumatic cushion.
Side at said launching cradle also is provided with emergency lighting device and/or instant fire extinguishment device.
The ejection type high-rise building life saving parachuting system of the utility model in use; The escape compartment that will carry the escape personnel through assist device launches away to oblique upper along the guide rail on the launching cradle; Can increase opening altitude on the one hand; Solve the problem of prior art low-to-medium altitude parachute-opening apart from deficiency, the horizontal range of launching generation on the other hand can make the escape personnel away from building, and the parachute in avoiding descending runs into the flame of ejection in the building; Can avoid simultaneously parachute to be upset, effectively raise escape personnel's security by scene of a fire air-flow and housing-group wind.The utility model volume is little, simple in structure, and it is less to take up room, and can be installed in indoorly near position of window, safe and convenient to use, is effective rescue tool of high-rise life saving.
Description of drawings
Fig. 1 is the structural representation of the utility model ejection type high-rise building life saving parachuting system embodiment one;
Fig. 2 is the structural representation of the utility model ejection type high-rise building life saving parachuting system embodiment two;
Fig. 3 is the structural representation of the utility model ejection type high-rise building life saving parachuting system embodiment three.
The specific embodiment
Embodiment one: the ejection type high-rise building life saving parachuting system implementation example one of the utility model is as shown in Figure 1; Be provided with launching cradle 1 in this lifesaving parachute landing system and be installed in the escape compartment that is used to carry the escape personnel on the launching cradle 1; This escape compartment is made up of seat 2 and the protection hatchcover 6 that is located on the seat 2; Launching cradle 1 is provided with a guide rail 1-1; Have an elevation angle between this guide rail 1-1 and the horizontal plane, seat 2 is directed on the guide rail 1-1 that is installed in launching cradle 1 of slip, is provided with the mounting strap 4 that is used to protect the escape personnel in the front portion of seat 2; At seat 2 rear portions parachuting device 3 is installed; Between the bottom of seat 2 and launching cradle 1, be equipped with and drive seat 2 and move and finally break away from the assist device that this guide rail 1-1 launches away to oblique upper along guide rail 1-1, this assist device is included in the fixing ejection guns 7 of incline direction of launching cradle 1 upper edge guide rail 1-1, in ejection guns 7, is provided with one and launches bullet 8; This launches bullet 8 and is fixedly connected with the bottom of seat 2; In ejection guns 7, be positioned at the rear portion of launching bullet 8 and be provided with and be used for taking for making things convenient for the escape personnel launching the gases at high pressure generating means that bullet 8 is launched, its side at launching cradle 1 also is provided with is convenient to the ladder that the escape personnel climbs up seat.In the present embodiment, the elevation angle of guide rail 1-1 is between 10 ° to 50 °; The gases at high pressure generating means adopts the gunpowder emitter, and it is in the ejection guns 7 that launches bullet 8 rear portions, to be provided with a powder storehouse 9, on powder storehouse 9, is connected with igniter 10.Simultaneously, the ejection switch 5 that is used to control igniter 10 igniting is installed in seat 2 bottoms.
The parachuting device of installing on the seat 3 is mainly formed by parachute and by the power parachute opener of automatic or manual switch control or by the forced parachute opening device of deciding power fixed length line traffic control; Wherein, The power parachute opener adopts bullet power parachute opener; Be connected with the sensing apparatus that falls that is used for sensing escape compartment state on this bullet power parachute opener, this falls sensing apparatus and adopts 3-axis acceleration sensor to connect the extension digital-control circuit, and itself and bullet power parachute opener are prior art; Can be the Chinese patent open file of ZL2011200655857 specifically, repeat no more here referring to the patent No..
During use, the escape personnel opens protection hatchcover 6, closes this protection hatchcover 6 again after accomplishing on the seat 2; And fix position and attitude through safety belt 4, and open ejection switch 5, igniter 10 starts lights the gunpowder in the powder storehouse 9; Gunpowder violent burning in ejection guns 7 produces high pressure and will launch bullet 8 and penetrate at a high speed, launches bullet 8 and promotes seats 2 and launch away to oblique upper along the guide rail 1-1 on the launching cradle 1, can be elevated to the height of a safe enough parachute-opening when making the escape personnel away from building; Make parachute that enough opening altitudes arranged, protection hatchcover 6 adopts opaque material to process, and also can on protection hatchcover 6, an observation window be set; Like this can be when comprising the survivor; The escape personnel can't be looked down, thereby overcome survivor's probably high psychology, it is effective equally to hypertension, cardiac.After launching; The aerial statue that falls the sensing device senses escape compartment in the parachuting device 3; When escape compartment begins to fall; Through falling weightless the recurring the time of sensing device senses, control bullet power parachute opener ejects and releases a parachute when the complete agravity time arrives setting value, accomplishes escape.
Further; For reducing the impulsive force that produces when seat 2 lands; Protect escape personnel's health safety fully, in the present embodiment, its bottom at seat 2 also is provided with the landing buffer unit; This landing buffer unit mainly is made up of aerating device that is installed in centre position, seat 2 bottom 12 and the buffering pneumatic cushion 11 that is installed in around seat 2 bottoms, and on each buffering pneumatic cushion 11, is provided with gas bleeder valve.This landing buffer unit is connected with control device in the parachuting device 3, and it triggers the aerating device 12 in the buffer unit when falling when sensing apparatus starts parachute, and aerating device 12 be that each buffering pneumatic cushion 11 is inflated; When seat 2 lands; Each buffering pneumatic cushion 11 receives the impulsive force on ground, and the gas power effect that is hit is compressed in the buffering pneumatic cushion 11, under the gas pressure effect, opens gas bleeder valve; Gas in the buffering pneumatic cushion 11 is discharged through gas bleeder valve; Thereby reach buffering effect, avoid buffering pneumatic cushion 11 under the effect of ground shock power, to produce bounce-back, prevent that unnecessary damages from appearring in the escape personnel.
Further; In order to guarantee that the escape personnel also can find this lifesaving parachute landing system to escape rapidly rapidly in the dark at night; Its rear side at launching cradle 1 also is equipped with emergency lighting device 14 through a vertically fixing support bar 13, and in addition, it can also be provided with an instant fire extinguishment device 15 that is used to protect this lifesaving parachute landing system on this support bar 13; So that when fire spread, protect this lifesaving parachute landing system; Avoid it to be burnt, and prolong the stand-by period as much as possible, make the escape personnel that enough times arranged by big fire.
Embodiment two: as shown in Figure 2, present embodiment two is that with the difference of embodiment one the gases at high pressure generating means that is provided with in the ejection guns 7 adopts gas cylinder 19, and this gas cylinder 19 is provided with magnetic valve 20 towards the exit of launching bullet 8.During use, open magnetic valve 20 through gauge tap 5, the spraying high-pressure gas in the gas cylinder 19 and going out is launched away together with seat 2 launching bullet 8.
It falls sensing apparatus and adopts 3-axis acceleration sensor to connect time-delay relay; Start time-delay relay when escape compartment is in the complete agravity state when 3-axis acceleration sensor senses, launch the parachute opener ejection and release a parachute through time-delay relay control power bullet and accomplish escape.
Embodiment three: as shown in Figure 3; Present embodiment three is with the difference of embodiment one and embodiment two; Its bottom at seat 2 also is fixed with rocket booster 30; The prior art of this rocket booster 30 for using on the aircraft; Thereby can further improve the ejection speed and the catapulting distance of seat 2, can avoid when making seat 2 landing that complicated situation drops to open field at a distance on the ground, and parachute winding accident takes place because of mutual spacing is less can prevent that a plurality of users from using this escape parachute falling unit simultaneously the time.
The utility model is not limited to the foregoing description; It is in concrete the application; The parachuting device can also adopt manual control bullet power parachute opener to realize parachute-opening; Or adopt by the disclosed a kind of electronic automatic opening controller for parachute control bullet power parachute opener of Chinese patent open file CN1645278A and realize parachute-opening, it can also adopt the power fixed length line of deciding that is connected between launching cradle and the bell to force parachute-opening or adopt the disclosed parachute auromatic unlocking device of Chinese patent open file CN200988579Y to force parachute-opening or adopt manually parachute-opening of escape personnel oneself; The landing buffer unit that is installed in seat bottom also can adopt to be decided power fixed length line and triggers, perhaps with fall sensing apparatus and be connected by digital-control circuit or time-delay relay and trigger, also can adopt installation hand switch triggering in the escape cabin; The assist device that is used to drive seat fire can also adopt the compression spring as boosting power; Rocket booster both can with the gases at high pressure generating means maybe this compression spring assist device use, also can independently use; The buffer unit of seat bottom setting can also adopt other buffering methods such as high-pressure injection streamer mode; But the technical scheme of above various equivalent substitutions is all within the protection domain of the utility model.
Claims (9)
1. ejection type high-rise building life saving parachuting system; It is characterized in that, comprise launching cradle and escape compartment, escape compartment is provided with seat and is equipped with the parachuting device; Seat is provided with safety belt; On said launching cradle, be provided with the guide rail that is slidingly matched with this escape compartment guiding, this guide rail has the elevation angle on horizontal plane, between escape compartment and launching cradle, is equipped with to drive escape compartment along guide rail moves and final getaway ejects at a high speed to oblique upper assist device.
2. ejection type high-rise building life saving parachuting according to claim 1 system is characterized in that, described escape compartment is by the seat that cooperates with the guide rail guiding and be located at the outer protection hatchcover of seat and form, and described parachute is installed in seat or protects on the hatchcover.
3. ejection type high-rise building life saving parachuting according to claim 1 system; It is characterized in that; Described assist device comprises the ejection guns that is fixed on the launching cradle and is installed in the bullet that launches in the ejection guns; The front end and the seat that launch bullet are connected, and are provided with in the bottom of ejection guns to be used for launching the gases at high pressure generating means that bullet is released.
4. ejection type high-rise building life saving parachuting according to claim 2 system is characterized in that, described gases at high pressure generating means is the powder burning device that is installed in the ejection guns.
5. ejection type high-rise building life saving parachuting according to claim 2 system is characterized in that, described gases at high pressure generating means is the gas cylinder that is connected the ejection guns bottom.
6. ejection type high-rise building life saving parachuting according to claim 2 system is characterized in that, in the bottom of said seat rocket booster is installed also.
7. according to any described ejection type high-rise building life saving parachuting system of claim 1 to 6; It is characterized in that; Mainly be made up of parachute and parachute opener at said parachuting device, described parachute opener is for the power parachute opener of automatic or manual switch control or by the forced parachute opening device of deciding power fixed length line traffic control.
8. ejection type high-rise building life saving parachuting according to claim 7 system; It is characterized in that; Also be provided with by the control of automatic or manual switch or by the landing buffer unit of deciding power fixed length line traffic control in the bottom of seat; This landing buffer unit comprises aerating device and buffering pneumatic cushion, is receiving the gas bleeder valve of opening automatically after the ground shock being provided with on the buffering pneumatic cushion.
9. ejection type high-rise building life saving parachuting according to claim 1 system is characterized in that, also is provided with emergency lighting device and/or instant fire extinguishment device in a side of said launching cradle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011204412110U CN202314999U (en) | 2011-09-28 | 2011-11-09 | Ejection type high-rise life saving dropping system |
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201120371963 | 2011-09-28 | ||
| CN201120371963.4 | 2011-09-28 | ||
| CN2011204412110U CN202314999U (en) | 2011-09-28 | 2011-11-09 | Ejection type high-rise life saving dropping system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202314999U true CN202314999U (en) | 2012-07-11 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2011204412110U Expired - Fee Related CN202314999U (en) | 2011-09-28 | 2011-11-09 | Ejection type high-rise life saving dropping system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202314999U (en) |
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104007451A (en) * | 2014-05-27 | 2014-08-27 | 曹宇 | Wrecking position recording reporting device |
| CN104568370A (en) * | 2014-12-11 | 2015-04-29 | 中国航天空气动力技术研究院 | Rapid parachute-opening wind tunnel test device of supersonic lander |
| CN104941088A (en) * | 2015-06-11 | 2015-09-30 | 华北科技学院 | Escape capsule |
| CN107050693A (en) * | 2017-06-01 | 2017-08-18 | 张力敏 | Residential building safe escape cabin |
| CN108482686A (en) * | 2018-05-24 | 2018-09-04 | 南京航空航天大学 | A kind of heavy helicopter ejection escape device |
| CN110898344A (en) * | 2019-12-20 | 2020-03-24 | 彭鑫乾 | High-rise escape equipment |
| CN110935113A (en) * | 2019-11-21 | 2020-03-31 | 康定市和宏房地产开发有限公司 | Auto-induction parachute-opening escape device in weightless state |
| CN111569280A (en) * | 2020-06-01 | 2020-08-25 | 东阳督凡安防科技有限公司 | Escape capsule capable of safely falling from high-rise building |
| CN112569488A (en) * | 2021-01-06 | 2021-03-30 | 南京花桂颜贸易有限公司 | High-rise earthquake escape device capable of breaking French window |
| CN114506459A (en) * | 2020-06-02 | 2022-05-17 | 赵润生 | Sideslip type ejection suspension seat of armed helicopter |
| US11427338B2 (en) | 2018-11-16 | 2022-08-30 | Ami Industries, Inc. | Inclining curved ejection seat assemblies |
-
2011
- 2011-11-09 CN CN2011204412110U patent/CN202314999U/en not_active Expired - Fee Related
Cited By (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104007451A (en) * | 2014-05-27 | 2014-08-27 | 曹宇 | Wrecking position recording reporting device |
| CN104007451B (en) * | 2014-05-27 | 2016-06-08 | 曹宇 | Wrecked position record report device |
| CN104568370B (en) * | 2014-12-11 | 2017-05-03 | 中国航天空气动力技术研究院 | Rapid parachute-opening wind tunnel test device of supersonic lander |
| CN104568370A (en) * | 2014-12-11 | 2015-04-29 | 中国航天空气动力技术研究院 | Rapid parachute-opening wind tunnel test device of supersonic lander |
| CN104941088B (en) * | 2015-06-11 | 2017-11-28 | 华北科技学院 | A kind of escape compartment |
| CN104941088A (en) * | 2015-06-11 | 2015-09-30 | 华北科技学院 | Escape capsule |
| CN107050693A (en) * | 2017-06-01 | 2017-08-18 | 张力敏 | Residential building safe escape cabin |
| CN108482686A (en) * | 2018-05-24 | 2018-09-04 | 南京航空航天大学 | A kind of heavy helicopter ejection escape device |
| CN108482686B (en) * | 2018-05-24 | 2023-09-26 | 南京航空航天大学 | Heavy helicopter catapulting escape device |
| US11427338B2 (en) | 2018-11-16 | 2022-08-30 | Ami Industries, Inc. | Inclining curved ejection seat assemblies |
| CN110935113A (en) * | 2019-11-21 | 2020-03-31 | 康定市和宏房地产开发有限公司 | Auto-induction parachute-opening escape device in weightless state |
| CN110898344A (en) * | 2019-12-20 | 2020-03-24 | 彭鑫乾 | High-rise escape equipment |
| CN111569280A (en) * | 2020-06-01 | 2020-08-25 | 东阳督凡安防科技有限公司 | Escape capsule capable of safely falling from high-rise building |
| CN114506459A (en) * | 2020-06-02 | 2022-05-17 | 赵润生 | Sideslip type ejection suspension seat of armed helicopter |
| CN112569488A (en) * | 2021-01-06 | 2021-03-30 | 南京花桂颜贸易有限公司 | High-rise earthquake escape device capable of breaking French window |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20120711 Termination date: 20131109 |