CN101823559A - Lifting rescue cabin of military aircraft - Google Patents
Lifting rescue cabin of military aircraft Download PDFInfo
- Publication number
- CN101823559A CN101823559A CN200910025293A CN200910025293A CN101823559A CN 101823559 A CN101823559 A CN 101823559A CN 200910025293 A CN200910025293 A CN 200910025293A CN 200910025293 A CN200910025293 A CN 200910025293A CN 101823559 A CN101823559 A CN 101823559A
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- rescue cabin
- rescue
- cabin
- hawser
- motor
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Abstract
The invention discloses a lifting rescue cabin of a military aircraft, a motor and a rope pulley are mounted on the aircraft which can be hovered, the motor drives the rope pulley to rotate, one end of a cable rope is fixed at the rope pulley, the rescue cabin is fixedly arranged at the other end of the cable rope, the rescue cabin can accommodate a plurality of people, an entrance is formed on the rescue cabin, a door which can be closed is arranged on the entrance, the rope pulley can wind up the cable rope, the length of the cable rope is 2000-10000m, when the motor rotates to one direction, the rope pulley winds up the cable rope, the cable rope lifts the rescue cabin, when the motor rotates to the other direction, the rope pulley pays off the cable rope, and the cable rope puts down the rescue cabin. The lifting rescue cabin of the military aircraft can be ascended or descended through the cable rope, safely send rescue personnel and required rescue objects to the accident scene and help the rescue personnel and the wounded flee the accident scene.
Description
Technical field
But the present invention relates to a kind of Liftable type rescue cabin that is installed on the floating type aircraft.
Background technology
When contingency takes place (as earthquake, fire, flood, freezing, mud-rock flow or war etc.), because captive self is difficult to even can't flees from the scene of the accident, the rescue group also is difficult to enter field conduct and rescues, often need this moment to implement to rescue in the air, the rescue group generally enters the scene by rope ladder on the aircraft or hawser and rescues, but the climbing rope ladder makes rescue action slow and dangerous, and rope ladder or hawser often fall short of, making the rescue group enter on-the-spot difficulty increases, and the rescue group rescues the wounded and the collaborative wounded are just bigger by the difficulty that aircraft upper cable or rope ladder break away from the scene of the accident; Sometimes also adopt the mode of paraoperation or air-drop article to implement rescue, but complicated landform makes the difficulty of rescue increase, paratrooper's life security is difficult to guarantee that the article of air-drop damage easily.
Summary of the invention
In order to overcome above-mentioned defective, the invention provides lifting rescue cabin of military aircraft, this lifting rescue cabin of military aircraft can hold some people, rescue cabin can rise or descend by hawser, safe delivers to the scene of the accident with rescue group and required rescue article, and can help the rescue group and the wounded to flee from the scene of the accident.
The present invention for the technical scheme that solves its technical matters and adopt is:
A kind of lifting rescue cabin of military aircraft, motor and rope sheave are installed on the aircraft that can hover, the rotation of motor-driven rope sheave, hawser one end is fixed in rope sheave, the hawser other end is fixed with rescue cabin, rescue cabin can hold some people, offers inlet on the rescue cabin, and inlet is provided with closable door, the rope sheave hawser of can reeling, the length of hawser is 2000～ten thousand metres, when motor rotates towards a direction, and rope sheave coiling hawser, hawser promotes rescue cabin to the cabin of aircraft, when motor rotated to another way, rope sheave was emitted hawser, and hawser is transferred rescue cabin to the destination.
Further technical scheme of the present invention is:
Described rescue cabin adopts the high-strength light material.
Be provided with controller in the cabin of aircraft, controller control rotating speed of motor and hand of rotation.
Be provided with apparatus of oxygen supply, light equipment, food and water in the rescue cabin, can be used for rescuing the wounded, the bulkhead of rescue cabin is provided with opal, is convenient to the rescue group and observes the outer environment of rescue cabin.
Rescue cabin is provided with the infrared inductor of perception rescue cabin ground clearance.
The invention has the beneficial effects as follows: when the needs air rescue, aircraft flight hovers to the place that needs rescue, rescue group on the aircraft is entered in the rescue cabin by the inlet on the rescue cabin, starter motor, by controller control rotating speed of motor and hand of rotation, the motor-driven rope sheave rotates towards a direction, rope sheave is emitted hawser, hawser is transferred rescue cabin to the named destination, the rescue group comes out from rescue cabin and implements rescue action then, the rescue group was communicated with the wounded and enters rescue cabin after rescue action was finished, starter motor, the hand of rotation and the rotating speed of controller control motor, the motor-driven rope sheave rotates to another way, rope sheave coiling hawser, hawser promote rescue cabin to the cabin of aircraft, make the rescue group and the wounded escape with life and limb.
Description of drawings
Fig. 1 is a structural representation of the present invention.
The specific embodiment
Embodiment: a kind of lifting rescue cabin of military aircraft, motor 1 and rope sheave 2 are installed on the aircraft that can hover, the rotation of motor-driven rope sheave, hawser 3 one ends are fixed in rope sheave, the hawser other end is fixed with rescue cabin 4, rescue cabin can hold some people, offers inlet on the rescue cabin, and inlet is provided with closable door, the rope sheave hawser of can reeling, the length of hawser is 2000～ten thousand metres, when motor rotates towards a direction, and rope sheave coiling hawser, hawser promotes rescue cabin to the cabin of aircraft, when motor rotated to another way, rope sheave was emitted hawser, and hawser is transferred rescue cabin to the destination.
Described rescue cabin adopts the high-strength light material.
Be provided with controller in the cabin of aircraft, controller control rotating speed of motor and hand of rotation.
Be provided with apparatus of oxygen supply, light equipment, food and water in the rescue cabin, can be used for rescuing the wounded, the bulkhead of rescue cabin is provided with opal, is convenient to the rescue group and observes the outer environment of rescue cabin.
Rescue cabin is provided with the infrared inductor of perception rescue cabin ground clearance.
Operating process of the present invention is as follows:
When the needs air rescue, aircraft flight is to the place that needs rescue, rescue group on the aircraft is entered in the rescue cabin by the inlet on the rescue cabin, starter motor, by controller control rotating speed of motor and hand of rotation, the motor-driven rope sheave rotates towards a direction, rope sheave is emitted hawser, hawser is transferred rescue cabin to the named destination, the rescue group comes out from rescue cabin and implements rescue action then, the rescue group was communicated with the wounded and enters rescue cabin after rescue action was finished, starter motor, the hand of rotation and the rotating speed of controller control motor, the motor-driven rope sheave rotates to another way, rope sheave coiling hawser, hawser promote rescue cabin to the cabin of aircraft, make the rescue group and the wounded escape with life and limb.
Claims (5)
1. lifting rescue cabin of military aircraft, it is characterized in that: motor (1) and rope sheave (2) are installed on the aircraft that can hover, the rotation of motor-driven rope sheave, hawser (3) one ends are fixed in rope sheave, the hawser other end is fixed with rescue cabin (4), rescue cabin can hold some people, offers inlet on the rescue cabin, and inlet is provided with closable door, the rope sheave hawser of can reeling, the length of hawser is 2000～ten thousand metres, when motor rotates towards a direction, and rope sheave coiling hawser, hawser promotes rescue cabin, when motor rotated to another way, rope sheave was emitted hawser, and hawser is transferred rescue cabin.
2. a kind of lifting rescue cabin of military aircraft according to claim 1 is characterized in that: described rescue cabin adopts the high-strength light material.
3. a kind of lifting rescue cabin of military aircraft according to claim 1 is characterized in that: be provided with controller in the cabin of aircraft, controller control rotating speed of motor and hand of rotation.
4. a kind of lifting rescue cabin of military aircraft according to claim 1 is characterized in that: be provided with apparatus of oxygen supply, light equipment, food and water in the rescue cabin, the bulkhead of rescue cabin is provided with opal.
5. according to the described a kind of lifting rescue cabin of military aircraft of one of claim 1 to 4, it is characterized in that: rescue cabin is provided with the infrared inductor of perception rescue cabin ground clearance.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN200910025293A CN101823559A (en) | 2009-03-02 | 2009-03-02 | Lifting rescue cabin of military aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN200910025293A CN101823559A (en) | 2009-03-02 | 2009-03-02 | Lifting rescue cabin of military aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN101823559A true CN101823559A (en) | 2010-09-08 |
Family
ID=42687783
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN200910025293A Pending CN101823559A (en) | 2009-03-02 | 2009-03-02 | Lifting rescue cabin of military aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN101823559A (en) |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105658519A (en) * | 2013-08-26 | 2016-06-08 | 谷歌公司 | Mechanisms for lowering payload to ground from uav |
| CN107952181A (en) * | 2017-12-27 | 2018-04-24 | 重庆金瓯科技发展有限责任公司 | Family fire rescue system |
| CN108159579A (en) * | 2017-12-27 | 2018-06-15 | 重庆金瓯科技发展有限责任公司 | Fire rescue system based on unmanned plane |
| CN108778927A (en) * | 2015-09-23 | 2018-11-09 | 沃尔玛阿波罗有限责任公司 | The system and method for delivering product with unmanned delivery aircraft |
| CN109987225A (en) * | 2019-04-03 | 2019-07-09 | 阙文新 | A kind of air rescue device and rescue mode |
| CN111204453A (en) * | 2020-03-26 | 2020-05-29 | 长春师范大学 | Large-load unmanned aerial vehicle rescue device |
| WO2020139307A1 (en) * | 2018-12-29 | 2020-07-02 | Андрей Павлович ЛИТВИНЕНКО | Convertible flying machine (variants), method of using a convertible flying machine (variants), transport device |
| CN113135291A (en) * | 2021-06-04 | 2021-07-20 | 何立峰 | Helicopter rescue equipment |
| DE102016224479B4 (en) | 2015-12-11 | 2021-08-05 | Disco Corporation | Transport drone for people |
-
2009
- 2009-03-02 CN CN200910025293A patent/CN101823559A/en active Pending
Cited By (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US10106257B2 (en) | 2013-08-26 | 2018-10-23 | X Development Llc | Mechanisms for lowering a payload to the ground from a UAV |
| US9783297B2 (en) | 2013-08-26 | 2017-10-10 | X Development Llc | Mechanisms for lowering a payload to the ground from a UAV |
| CN105658519A (en) * | 2013-08-26 | 2016-06-08 | 谷歌公司 | Mechanisms for lowering payload to ground from uav |
| US9957046B2 (en) | 2013-08-26 | 2018-05-01 | X Development Llc | Mechanisms for lowering a payload to the ground from a UAV |
| CN108778927A (en) * | 2015-09-23 | 2018-11-09 | 沃尔玛阿波罗有限责任公司 | The system and method for delivering product with unmanned delivery aircraft |
| US11053006B2 (en) | 2015-09-23 | 2021-07-06 | Walmart Apollo, Llc | Systems and methods of delivering products with unmanned delivery aircrafts |
| DE102016224479B4 (en) | 2015-12-11 | 2021-08-05 | Disco Corporation | Transport drone for people |
| CN108159579A (en) * | 2017-12-27 | 2018-06-15 | 重庆金瓯科技发展有限责任公司 | Fire rescue system based on unmanned plane |
| CN107952181A (en) * | 2017-12-27 | 2018-04-24 | 重庆金瓯科技发展有限责任公司 | Family fire rescue system |
| WO2020139307A1 (en) * | 2018-12-29 | 2020-07-02 | Андрей Павлович ЛИТВИНЕНКО | Convertible flying machine (variants), method of using a convertible flying machine (variants), transport device |
| CN109987225A (en) * | 2019-04-03 | 2019-07-09 | 阙文新 | A kind of air rescue device and rescue mode |
| CN111204453A (en) * | 2020-03-26 | 2020-05-29 | 长春师范大学 | Large-load unmanned aerial vehicle rescue device |
| CN113135291A (en) * | 2021-06-04 | 2021-07-20 | 何立峰 | Helicopter rescue equipment |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20100908 |