CN104491993A - High-altitude life-saving device - Google Patents
High-altitude life-saving device Download PDFInfo
- Publication number
- CN104491993A CN104491993A CN201410855095.5A CN201410855095A CN104491993A CN 104491993 A CN104491993 A CN 104491993A CN 201410855095 A CN201410855095 A CN 201410855095A CN 104491993 A CN104491993 A CN 104491993A
- Authority
- CN
- China
- Prior art keywords
- seat
- life
- altitude
- saving device
- main shaft
- 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.)
- Pending
Links
- 230000035939 shock Effects 0.000 claims abstract description 9
- 239000002002 slurry Substances 0.000 claims description 10
- 238000005422 blasting Methods 0.000 abstract 1
- 239000000383 hazardous chemical Substances 0.000 abstract 1
- 241000883990 Flabellum Species 0.000 description 1
- 230000001133 acceleration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
Classifications
-
- A—HUMAN NECESSITIES
- A62—LIFE-SAVING; FIRE-FIGHTING
- A62B—DEVICES, APPARATUS OR METHODS FOR LIFE-SAVING
- A62B1/00—Devices for lowering persons from buildings or the like
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D19/00—Non-canopied parachutes
- B64D19/02—Rotary-wing parachutes
Landscapes
- Health & Medical Sciences (AREA)
- General Health & Medical Sciences (AREA)
- Business, Economics & Management (AREA)
- Emergency Management (AREA)
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Emergency Lowering Means (AREA)
Abstract
The invention relates to a high-altitude life-saving device. The high-altitude life-saving device is a passive and high-reliability special life-saving device facility for high altitudes and high-rise buildings; the high-altitude life-saving device is mainly composed of a main shaft, a bearing, a propeller, a tholepin, a wind-driven paddle, a seat frame, a safety belt, a shock absorbing supporting legs, a cushion and the like. In case of air crash of high-altitude aircrafts or exceptional situations such as fire, blasting and hazardous substance leakage of high-rise buildings, people can sit in the high-altitude life-saving device quickly and then land on the ground safely, quickly and reliably to be out of danger; the worry of people working and living at high altitudes and in high-rise buildings is eliminated. In case of exceptional situations, the life safety of people is guaranteed.
Description
Technical field:
The present invention relates to a kind of high-altitude life-saving appliance, belong to high-altitude and high-rise building safe facility.
Background technology: the air crash of countries in the world at present, of common occurrence, cause great fear to the mankind, particularly cause a large amount of casualties and property loss, amazing especially.In recent years, the skyscraper in the whole world gets up more, more and more higher.Such as: our China determines to have 1318 skyscraper to rise sheer from level ground in recent years, some developed countries of the whole world then also will surpass one, but everybody ignores a bit.Namely be high altitude rescue problem, although every country takes series of measures all in various degree, also can not meet growing needs far away.Such as: the U.S. " 911 " event, see that the life of nearly 10000 people is lost one's life helplessly, but feel simply helpless.Changsha hotel fire, causes nearly 100 human lives to bury the sea of fire, and this is a how bitter lesson!
The content of invention:
The object of the invention is to be to provide a kind of high-altitude life-saving appliance.It is a kind of special high-altitude safe lifesaving appliance, it is applicable to the aircraft of all kinds and height, and the lifesaving of various differing heights skyscraper, is more suitable for the quick land of aircraft carrier, and the aspect such as spaceship associate components deceleration safe retrieving, also will play the guaranteeing role of reliability.
To the effect that of the present invention: high-altitude life-saving appliance is made up of main shaft, bearing, propeller, crutch, pneumatic slurry, seat, safety belt, shock reducing support leg, seat cushion and seat frame etc.The upper end of high-altitude life-saving appliance main shaft is set with pneumatic slurry, crutch, propeller from bottom to up successively, this crutch can be packed up at ordinary times, namely be rotated down 90 ° parallel with seat both sides, the cylindrical of main shaft and the inner ring of bearing are tight fit, outer shroud then connects as one with crutch, connects propeller above crutch, dynamic slurry of giving a dinner for a visitor from afar below, the lower end of main shaft then connects with seat jail and is integrated, and seat is equipped with safety belt, seat cushion and seat frame etc.
Shock reducing support leg is equipped with in the lower end of seat, and this leg can be packed up parallel with seat lower frame at ordinary times.
Run into emergency, escape personnel sits on rapidly on the seat cushion of seat, fastens seat belts and stresses on both hands two frames of seat, leap to sea of clouds rapidly, at this moment along with the weight of human body will be landed ground at leisure, according to acceleration of gravity and more and more faster, while landing, one wind-force upwards will be produced, this strand of wind-force then can as wind-driven generator, driving propeller rotates, and propeller rotates and just as picking-up helicopter, survivor upwards held up again, makes its landing slowly.As long as the therefore size of our suitable selection propeller flabellum, survivor be delivered to ground with the speed of safety by fixed meeting.
The invention has the advantages that:
1, volume of the present invention is little, lightweight, easy and simple to handle, safe and reliable.
2, the present invention need not power source, but relies on survivor's own wt as power source, is therefore the not complete of inexhaustible use.
3, highly versatile of the present invention, is applicable to the different aircraft in high-altitude of multiclass and the skyscraper of multiple differing heights.
4, when after the setting of propeller fan blade size, then decrease speed will adjust automatically.
Accompanying drawing illustrates:
Accompanying drawing 1: a kind of embodiment of the present invention.
Accompanying drawing 2: structural representation of the present invention.
Detailed description of the invention:
Embodiment as shown in Figure 1 and Figure 2.High-altitude life-saving appliance of the present invention is made up of main shaft 1, bearing 2, propeller 3, crutch 4, pneumatic slurry 5, seat 6, safety belt 7, shock reducing support leg 8, seat cushion 9, seat frame 10 etc.It is characterized in that: main shaft 1 is actively coupled by bearing 2 and crutch 4, the top fixed installation propeller 3 of crutch 4, install pneumatic slurry 5 below, its crutch 5 can be rotated down 90 °, overlaps the surrounding of seat 6.
The lower end of main shaft 1 then connects with seat 6 jail and is integrated, seat 6 is provided with safety belt 7, seat cushion 9, seat frame 10, in the bottom of seat 6, shock reducing support leg 8 is housed, frightens to eliminate when survivor lands from shake.Shock reducing support leg 8 can make it parallel with the base of seat 6 to direction, the inner side half-twist of seat 6, is beneficial to carry and collect.
Claims (4)
1. a high-altitude life-saving appliance, comprises main shaft, bearing, propeller, crutch, pneumatic slurry, seat, safety belt, shock reducing support leg, seat cushion, seat frame.It is characterized in that: the upper end of main shaft is provided with pneumatic slurry, crutch and propeller successively by bearing.The lower end of main shaft connects with seat one, and seat is equipped with safety belt, seat cushion and seat frame, the lower end of seat is equipped with shock reducing support leg, and this shock reducing support leg can be packed up parallel below with seat at ordinary times.
2. according to claim 1, described high-altitude life-saving appliance, is characterized in that: the lower end that propeller is positioned on above crutch, pneumatic slurry is positioned on crutch.
3. according to claim 1, described high-altitude life-saving appliance, is characterized in that: seat jail is connected on the bottom of main shaft and pneumatic slurry.
4. according to claim 1, described high-altitude life-saving appliance, is characterized in that: pneumatic slurry also can substitute with DC brushless motor.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410855095.5A CN104491993A (en) | 2014-12-25 | 2014-12-25 | High-altitude life-saving device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410855095.5A CN104491993A (en) | 2014-12-25 | 2014-12-25 | High-altitude life-saving device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104491993A true CN104491993A (en) | 2015-04-08 |
Family
ID=52933498
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410855095.5A Pending CN104491993A (en) | 2014-12-25 | 2014-12-25 | High-altitude life-saving device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104491993A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105169577A (en) * | 2015-10-13 | 2015-12-23 | 曾令太 | Sliding device for high-rise escape |
| CN105730689A (en) * | 2016-04-14 | 2016-07-06 | 天津京东智联科技发展有限公司 | Double-rotor high-rise escape aircraft |
| CN110077584A (en) * | 2019-05-16 | 2019-08-02 | 贵州大学 | A kind of DCB Specimen high-rise life saving aircraft |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2451473Y (en) * | 2000-04-27 | 2001-10-03 | 苗永林 | Airborne lifesaving umbrella |
| CN2616473Y (en) * | 2003-05-16 | 2004-05-19 | 项小峰 | Safety airborne device |
| CN201516247U (en) * | 2009-11-03 | 2010-06-30 | 吴万象 | Descent control device for sky escape |
| CN201537325U (en) * | 2009-09-11 | 2010-08-04 | 长春理工大学光电信息学院 | High-altitude escape slow descent device |
| CN102019045A (en) * | 2010-11-25 | 2011-04-20 | 大连海洋大学 | Cushion for emergency escape on lower floors |
| CN103028206A (en) * | 2012-12-20 | 2013-04-10 | 刘晓冰 | Parachute high altitude escape device |
-
2014
- 2014-12-25 CN CN201410855095.5A patent/CN104491993A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2451473Y (en) * | 2000-04-27 | 2001-10-03 | 苗永林 | Airborne lifesaving umbrella |
| CN2616473Y (en) * | 2003-05-16 | 2004-05-19 | 项小峰 | Safety airborne device |
| CN201537325U (en) * | 2009-09-11 | 2010-08-04 | 长春理工大学光电信息学院 | High-altitude escape slow descent device |
| CN201516247U (en) * | 2009-11-03 | 2010-06-30 | 吴万象 | Descent control device for sky escape |
| CN102019045A (en) * | 2010-11-25 | 2011-04-20 | 大连海洋大学 | Cushion for emergency escape on lower floors |
| CN103028206A (en) * | 2012-12-20 | 2013-04-10 | 刘晓冰 | Parachute high altitude escape device |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105169577A (en) * | 2015-10-13 | 2015-12-23 | 曾令太 | Sliding device for high-rise escape |
| CN105730689A (en) * | 2016-04-14 | 2016-07-06 | 天津京东智联科技发展有限公司 | Double-rotor high-rise escape aircraft |
| CN110077584A (en) * | 2019-05-16 | 2019-08-02 | 贵州大学 | A kind of DCB Specimen high-rise life saving aircraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20150408 |