WO2018172812A1 - Device for the soft landing of an aeroplane when the use of landing gear is not possible - Google Patents
Device for the soft landing of an aeroplane when the use of landing gear is not possible Download PDFInfo
- Publication number
- WO2018172812A1 WO2018172812A1 PCT/IB2017/051629 IB2017051629W WO2018172812A1 WO 2018172812 A1 WO2018172812 A1 WO 2018172812A1 IB 2017051629 W IB2017051629 W IB 2017051629W WO 2018172812 A1 WO2018172812 A1 WO 2018172812A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- landing
- platform
- aeroplane
- aircraft
- shock
- Prior art date
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Definitions
- the device is a shock-absorbing platform consisting of elastic cells that are filled with air or a gaseous mixture. The cells are gently bonded to each other.
- the device is intended for the safety of the aircraft and the lives of passengers during the emergency landing.
- the aircraft can land in the following way: the plane hovering over the runway during landing (take-off and landing lane) or some other place on which the shock-absorbing platform is laid out, and then, turning off the engines, carries out
- the safety of the aircraft will be ensured by the cushioning properties of the platform.
- the height at which the aircraft will fall should be as low as possible, but nevertheless, with a sufficient height of the platform, the height of the fall can be different.
- the shock impulse arising from the dead weight of the aircraft and the height of the fall that the platform can withstand is limited only by the dimensions of the platform itself (height) and the properties of the elastic cell. Depreciation qualities ("softness") of the platform can be increased to almost any level. That is, the platform, in principle, can take and withstand any weight, any aircraft.
Landscapes
- Braking Arrangements (AREA)
Abstract
The invention relates to an aircraft braking landing device and to the emergency landing of an aeroplane. The device comprises a shock-absorbing platform consisting of elastic cells fastened to each other and filled with a gaseous mixture. The platform is intended to soften and neutralize the impact of an aeroplane upon landing when the use of landing gear is not possible. The invention achieves easy and reliable use of the platform and mobility of same.
Description
УСТРОЙСТВО ДЛЯ ОСУЩЕСТВЛЕНИЯ мягкой ПОСАДКИ САМОЛЕТА В УСЛОВИЯХ НЕВОЗМОЖНОСТИ ПОСАДКИ НА ШАССИ DEVICE FOR IMPLEMENTING A PLANE SOFT PLANE UNDER CONDITIONS OF IMPOSSIBILITY OF LANDING ON THE CHASSIS
Устройство представляет собой амортизирующую платформу , состоящую из эластичных ячеек , которые заполнены воздухом или газообразной смесью .Ячейки мягко скреплены между собой . The device is a shock-absorbing platform consisting of elastic cells that are filled with air or a gaseous mixture. The cells are gently bonded to each other.
Устройство предназначено для сохранности самолета и жизни пассажиров при осуществлении аварийной посадки . The device is intended for the safety of the aircraft and the lives of passengers during the emergency landing.
Сохранность самолета ,а также жизней пассажиров при аварийной посадке самолета достигается только одним способом : The safety of the aircraft, as well as the lives of passengers during an emergency landing, is achieved in only one way:
нейтрализацией ударного воздействия внешней среды . neutralization of the impact of the external environment.
При невозможности посадить самолет на шасси , в случае аварии или когда невозможна посадка в штатном режиме например , сложные погодные метеоусловия (сильный ветер , шторм , снежный буран )— посадка самолета может быть осуществлена так : самолет ,при посадке зависает над ВПП (взлетно-посадочная полоса ) или каким либо другим местом на котором раскладывается амортизирующая платформа , и потом , выключив двигатели— осуществляет If it is impossible to land the aircraft on the chassis, in the event of an accident or when normal landing is impossible, for example, difficult weather conditions (strong wind, storm, snowstorm) - the aircraft can land in the following way: the plane hovering over the runway during landing (take-off and landing lane) or some other place on which the shock-absorbing platform is laid out, and then, turning off the engines, carries out
свободное падение на платформу .Сохранность самолета будет обеспечена амортизационными свойствами платформы .Высота с которой самолет будет осуществлять падение должна быть по возможности ниже , но тем не менее , при достаточной высоте платформы высота падения может быть различна . free fall on the platform. The safety of the aircraft will be ensured by the cushioning properties of the platform. The height at which the aircraft will fall should be as low as possible, but nevertheless, with a sufficient height of the platform, the height of the fall can be different.
Ударный импульс возникающий из собственного веса самолета и высоты падения , который может выдержать платформа ограничен только размерами самой платформы ( высотой ) и свойствами эластичной ячейки . Амортизационные качества ( «мягкость ») платформы можно увеличивать практически до любого уровня .То есть платформа в принципе может принять и выдержать любой вес , любого самолета . The shock impulse arising from the dead weight of the aircraft and the height of the fall that the platform can withstand is limited only by the dimensions of the platform itself (height) and the properties of the elastic cell. Depreciation qualities ("softness") of the platform can be increased to almost any level. That is, the platform, in principle, can take and withstand any weight, any aircraft.
Простота и низкая стоимость подобной платформы позволяет многократно повышать ее надежность просто увеличивая ее The simplicity and low cost of such a platform allows you to repeatedly increase its reliability by simply increasing it
размеры . Быстро монтируется в любом , удобном месте.
sizes. It is quickly mounted in any convenient place.
Claims
ФОРМУЛА ИЗОБРЕТЕНИЯ CLAIM
УСТРОЙСТВО ДЛЯ ОСУЩЕСТВЛЕНИЯ МЯГКОЙ ПОСАДКИ САМОЛЕТА В УСЛОВИЯХ НЕВОЗМОЖНОСТИ ПОСАДКИ НА ШАССИ DEVICE FOR CARRYING OUT THE SOFT PLANE OF THE AIRPLANE IN THE CONDITIONS OF IMPOSSIBILITY OF LANDING ON THE CHASSIS
Амортизирующая платформа , состоящая из эластичных ячеек .шарообразной или квадратной формы .мягко скрепленных между собой .заполненных воздухом или газообразной Shock-absorbing platform, consisting of elastic cells. Spherical or square. Softly bonded to each other. Filled with air or gaseous
смесью , предназначенная для смягчения и нейтрализации ударного импульса самолета в момент его приземления при невозможности посадки в штатном режиме , на шасси.
a mixture designed to mitigate and neutralize the shock pulse of the aircraft at the time of its landing, if it is impossible to land normally, on the landing gear.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PCT/IB2017/051629 WO2018172812A1 (en) | 2017-03-21 | 2017-03-21 | Device for the soft landing of an aeroplane when the use of landing gear is not possible |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PCT/IB2017/051629 WO2018172812A1 (en) | 2017-03-21 | 2017-03-21 | Device for the soft landing of an aeroplane when the use of landing gear is not possible |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| WO2018172812A1 true WO2018172812A1 (en) | 2018-09-27 |
Family
ID=63585109
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/IB2017/051629 WO2018172812A1 (en) | 2017-03-21 | 2017-03-21 | Device for the soft landing of an aeroplane when the use of landing gear is not possible |
Country Status (1)
| Country | Link |
|---|---|
| WO (1) | WO2018172812A1 (en) |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2850252A (en) * | 1952-08-06 | 1958-09-02 | Goodyear Tire & Rubber | Inflatable mat structure |
| US6092763A (en) * | 1998-12-01 | 2000-07-25 | David John Hemes | Aircraft crash damage limitation system |
| US20080308673A1 (en) * | 2006-04-19 | 2008-12-18 | Yuen Liu | Secure System and Method for Aircraft Emergency Landing |
-
2017
- 2017-03-21 WO PCT/IB2017/051629 patent/WO2018172812A1/en active Application Filing
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2850252A (en) * | 1952-08-06 | 1958-09-02 | Goodyear Tire & Rubber | Inflatable mat structure |
| US6092763A (en) * | 1998-12-01 | 2000-07-25 | David John Hemes | Aircraft crash damage limitation system |
| US20080308673A1 (en) * | 2006-04-19 | 2008-12-18 | Yuen Liu | Secure System and Method for Aircraft Emergency Landing |
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