CN2668511Y - Aircraft forced landing device - Google Patents
Aircraft forced landing device Download PDFInfo
- Publication number
- CN2668511Y CN2668511Y CNU2003201226093U CN200320122609U CN2668511Y CN 2668511 Y CN2668511 Y CN 2668511Y CN U2003201226093 U CNU2003201226093 U CN U2003201226093U CN 200320122609 U CN200320122609 U CN 200320122609U CN 2668511 Y CN2668511 Y CN 2668511Y
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- CN
- China
- Prior art keywords
- aircraft
- forced landing
- landing device
- platform
- protective cover
- 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.)
- Expired - Fee Related
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Abstract
The utility model relates to an aircraft forced landing device which can make an aircraft land safely when the landing gear of the aircraft is damaged. The aircraft forced landing device can avoid some aviation accidents caused by the failure of the landing gear.
Description
Technical field:
Involved in the present invention is a kind of lifesaving appliance of aviation field, is used for forced landing.
Background technology:
Be that aircraft was born for 100 anniversaries this year, and aircraft has become the indispensable vehicle in people's routine in the period of 100, because the shortcoming of aircraft itself, so still suitable protrusion of safety problem.For example when aircraft aloft because that alighting gear damages is former thereby can't land the time, have only emergency landing usually.In case the generation emergency landing, the possibility that personal casualty takes place is very big.
Summary of the invention:
In order to overcome the above-mentioned aircraft accident that takes place owing to the undercarriage problem, the invention provides a kind of approach that can lifesaving, can allow aircraft safety land.
The technical solution adopted for the present invention to solve the technical problems is: one than aircraft bigger unmanned machinery control under the platform one group of wheel be installed, and can direct drive and control wheel turns.Controlling at unmanned machinery has one to receive protective cover on the platform, it has flame resistance and flexibility.In the time of can't landing when aircraft discovery alighting gear et out of order, the aviator on the aircraft informs airport nearby at once, and the aspect, airport starts this forced landing device, and waits for that aircraft arrives.When aircraft is wanted land; the ground staff controls the forced landing device and accelerates to the speed identical with aircraft, and talk down, and aircraft landing is on the reception protective cover of forced landing device; have fire-retardant and soft characteristic owing to receive protective cover, so aircraft landing is foolproof in the above.Last forced landing device is decelerated to safety zone with aircraft, finishes the forced landing task.
Accident when generation of the present invention can effectively reduce aircraft landing improves the safety of flight greatly, the vehicle that aircraft become really transport safely.
Description of drawings
The present invention is further described below in conjunction with drawings and Examples.
Fig. 1 is a fundamental diagram of the present invention.
Fig. 2 is a constructional drawing of the present invention
Among Fig. 11, airstrip, 2, the forced landing device, 3, aircraft
5, one groups of wheels among Fig. 2,6, unmanned machinery controls platform, 7, receive protective cover
The specific embodiment
In Fig. 1, control platform one than aircraft 3 bigger unmanned machineries and 6 times one group of wheel 5 is installed, and can direct drive and control wheel turns.Controlling at unmanned machinery has one to receive protective cover 7 on the platform 6, it is made by fire-retardant asbestos.In the time of can't landing when aircraft 3 alighting gear et out of orders, the aviator on the aircraft 3 informs airport nearby at once, and the aspect, airport starts this forced landing device, waits for that on airstrip 1 aircraft arrives.When aircraft 3 is wanted land; the ground staff controls forced landing device 2 and accelerates to the speed identical with aircraft 3; and notice aircraft 3 landing; aircraft 3 drops on the reception protective cover 7 of forced landing device 2; because asbestos layer has fire-retardant and soft characteristic, so aircraft 3 is foolproof above dropping to.Last forced landing device 2 is decelerated to safety zone with aircraft 3, finishes the forced landing task.
Claims (3)
1, forced landing device is controlled platform and received protective cover by one group of wheel, unmanned machinery and forms, it is characterized in that: one group of wheel is installed and unmanned machinery is controlled on the platform, and unmanned machinery is controlled the reception protective cover is installed on the platform.
2, forced landing device according to claim 1 is characterized in that not having the machinery of going into and controls dynamic device of platform tool and wireless receiving control setup, can drive and control wheel turns.
3, forced landing device according to claim 1, it is characterized in that receiving protective cover is to be made by fire-retardant flexible asbestos.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2003201226093U CN2668511Y (en) | 2003-12-19 | 2003-12-19 | Aircraft forced landing device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2003201226093U CN2668511Y (en) | 2003-12-19 | 2003-12-19 | Aircraft forced landing device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN2668511Y true CN2668511Y (en) | 2005-01-05 |
Family
ID=34439217
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNU2003201226093U Expired - Fee Related CN2668511Y (en) | 2003-12-19 | 2003-12-19 | Aircraft forced landing device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN2668511Y (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102470921A (en) * | 2009-07-27 | 2012-05-23 | 贝尔直升机泰克斯特龙公司 | Aircraft occupant protection system |
| CN102530257A (en) * | 2012-02-10 | 2012-07-04 | 南京航空航天大学 | Forced landing device for civil aircrafts |
-
2003
- 2003-12-19 CN CNU2003201226093U patent/CN2668511Y/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102470921A (en) * | 2009-07-27 | 2012-05-23 | 贝尔直升机泰克斯特龙公司 | Aircraft occupant protection system |
| CN102470921B (en) * | 2009-07-27 | 2015-03-04 | 贝尔直升机泰克斯特龙公司 | Aircraft occupant protection system |
| CN102530257A (en) * | 2012-02-10 | 2012-07-04 | 南京航空航天大学 | Forced landing device for civil aircrafts |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C19 | Lapse of patent right due to non-payment of the annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |