CN1629040A - Airplane forced landing device - Google Patents
Airplane forced landing device Download PDFInfo
- Publication number
- CN1629040A CN1629040A CN 200310109543 CN200310109543A CN1629040A CN 1629040 A CN1629040 A CN 1629040A CN 200310109543 CN200310109543 CN 200310109543 CN 200310109543 A CN200310109543 A CN 200310109543A CN 1629040 A CN1629040 A CN 1629040A
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- aircraft
- forced landing
- landing device
- platform
- protective cover
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- 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.)
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Abstract
This invention relates to an airplane safe landing device when the landing chassis is damaged, which can avoid the aviation accidents due to the chassis damage.
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 unmanned machinery 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 |
|---|---|---|---|
| CN 200310109543 CN1629040A (en) | 2003-12-19 | 2003-12-19 | Airplane forced landing device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200310109543 CN1629040A (en) | 2003-12-19 | 2003-12-19 | Airplane forced landing device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN1629040A true CN1629040A (en) | 2005-06-22 |
Family
ID=34843085
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 200310109543 Pending CN1629040A (en) | 2003-12-19 | 2003-12-19 | Airplane forced landing device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN1629040A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| ES2325974A1 (en) * | 2007-05-03 | 2009-09-25 | Fco. Javier Porras Vila | Truck-forced landing platform (Machine-translation by Google Translate, not legally binding) |
| CN103646602A (en) * | 2013-12-09 | 2014-03-19 | 河南师范大学 | Simulated ship-bone aircraft take-off and landing training platform |
| CN105752351A (en) * | 2016-04-27 | 2016-07-13 | 武汉大学 | Auxiliary device for safe landing of aircraft and safe landing method |
| CN111792054A (en) * | 2020-06-15 | 2020-10-20 | 成都飞机工业（集团）有限责任公司 | Safe test flight method based on airplane airborne sliding forced landing capability |
| CN112711268A (en) * | 2020-12-01 | 2021-04-27 | 一飞智控(天津)科技有限公司 | Forced landing path planning method and system, unmanned aerial vehicle, processing terminal and storage medium |
-
2003
- 2003-12-19 CN CN 200310109543 patent/CN1629040A/en active Pending
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| ES2325974A1 (en) * | 2007-05-03 | 2009-09-25 | Fco. Javier Porras Vila | Truck-forced landing platform (Machine-translation by Google Translate, not legally binding) |
| CN103646602A (en) * | 2013-12-09 | 2014-03-19 | 河南师范大学 | Simulated ship-bone aircraft take-off and landing training platform |
| CN105752351A (en) * | 2016-04-27 | 2016-07-13 | 武汉大学 | Auxiliary device for safe landing of aircraft and safe landing method |
| CN111792054A (en) * | 2020-06-15 | 2020-10-20 | 成都飞机工业（集团）有限责任公司 | Safe test flight method based on airplane airborne sliding forced landing capability |
| CN111792054B (en) * | 2020-06-15 | 2021-06-08 | 成都飞机工业（集团）有限责任公司 | Safe test flight method based on airplane airborne sliding forced landing capability |
| CN112711268A (en) * | 2020-12-01 | 2021-04-27 | 一飞智控(天津)科技有限公司 | Forced landing path planning method and system, unmanned aerial vehicle, processing terminal and storage medium |
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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 |