RU94023216A - Method of landing descent vehicle - Google Patents

Method of landing descent vehicle

Info

Publication number
RU94023216A
RU94023216A RU94023216/06A RU94023216A RU94023216A RU 94023216 A RU94023216 A RU 94023216A RU 94023216/06 A RU94023216/06 A RU 94023216/06A RU 94023216 A RU94023216 A RU 94023216A RU 94023216 A RU94023216 A RU 94023216A
Authority
RU
Russia
Prior art keywords
landing
parachute
aircraft
flying vehicle
horizontal
Prior art date
Application number
RU94023216/06A
Other languages
Russian (ru)
Other versions
RU2090455C1 (en
Inventor
В.А. Ковалевский
В.А. Савичев
А.А. Туполев
А.К. Федоров
Original Assignee
В.А. Ковалевский
В.А. Савичев
А.А. Туполев
А.К. Федоров
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by В.А. Ковалевский, В.А. Савичев, А.А. Туполев, А.К. Федоров filed Critical В.А. Ковалевский
Priority to RU94023216A priority Critical patent/RU2090455C1/en
Publication of RU94023216A publication Critical patent/RU94023216A/en
Application granted granted Critical
Publication of RU2090455C1 publication Critical patent/RU2090455C1/en

Links

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  • Toys (AREA)
  • Emergency Lowering Means (AREA)

Abstract

FIELD: aeronautical engineering; alighting gears; parachute landing on unprepared surface under wind conditions. SUBSTANCE: method consists in preliminary deployment of landing parachute after which parachute is rehooked for bringing the flying vehicle in horizontal landing position and flying vehicle is oriented by tail section forward in way of horizontal motion relative to the Earth. This protects the flying vehicle against upset around the line connecting the points of contact with the Earth by one footpad of main landing gear and footpad of nose landing gear. EFFECT: higher safety of landing and prevention of upset. 5 cl, 8 dwg

Claims (1)

Изобретение относится к автокосмической технике, а именно к взлетно-посадочным устройствам летательных аппаратов, где посадка производится на парашюте на неподготовленную поверхность при наличии ветра. Целью изобретения является предотвращение опрокидывания и повышение безопасности посадки. Способ посадки спускаемого летательного аппарата состоит в том, что заблаговременно выпускают посадочный парашют, затем перецепляют парашют для приведения летательного аппарата в горизонтальное посадочное положение и ориентируют хвостовой частью вперед по направлению горизонтального перемещения летательного аппарата относительно земли. Это препятствует возможному опрокидыванию летательного аппарата вокруг линии, соединяющей точки контакта с землей одной из пят основного шасси и пяты носового шасси.The invention relates to aerospace engineering, namely to takeoff and landing devices of aircraft, where landing is carried out by parachute on an unprepared surface in the presence of wind. The aim of the invention is to prevent rollover and increase the safety of landing. The landing method of the descent aircraft is that a landing parachute is released in advance, then the parachute is retuned to bring the aircraft into a horizontal landing position and the tail part is oriented forward in the direction of horizontal movement of the aircraft relative to the ground. This prevents the aircraft from tipping over around the line connecting the contact points with the ground of one of the heels of the main landing gear and the heel of the bow landing gear.
RU94023216A 1994-06-17 1994-06-17 Method of landing descent vehicle RU2090455C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU94023216A RU2090455C1 (en) 1994-06-17 1994-06-17 Method of landing descent vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU94023216A RU2090455C1 (en) 1994-06-17 1994-06-17 Method of landing descent vehicle

Publications (2)

Publication Number Publication Date
RU94023216A true RU94023216A (en) 1997-04-10
RU2090455C1 RU2090455C1 (en) 1997-09-20

Family

ID=20157419

Family Applications (1)

Application Number Title Priority Date Filing Date
RU94023216A RU2090455C1 (en) 1994-06-17 1994-06-17 Method of landing descent vehicle

Country Status (1)

Country Link
RU (1) RU2090455C1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109774955A (en) * 2019-03-06 2019-05-21 成都飞机工业（集团）有限责任公司 Drag parachute housing structure is buried in one kind is two-door

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108058835B (en) * 2017-12-20 2021-07-27 郑州康晓科技有限公司 Unmanned aerial vehicle accident condition falling prevention and damage device

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109774955A (en) * 2019-03-06 2019-05-21 成都飞机工业（集团）有限责任公司 Drag parachute housing structure is buried in one kind is two-door
CN109774955B (en) * 2019-03-06 2022-01-25 成都飞机工业（集团）有限责任公司 Double-door embedded resistance umbrella cabin structure

Also Published As

Publication number Publication date
RU2090455C1 (en) 1997-09-20

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