RU95103116A - Flying vehicle retractable landing gear - Google Patents

Flying vehicle retractable landing gear

Info

Publication number
RU95103116A
RU95103116A RU95103116/11A RU95103116A RU95103116A RU 95103116 A RU95103116 A RU 95103116A RU 95103116/11 A RU95103116/11 A RU 95103116/11A RU 95103116 A RU95103116 A RU 95103116A RU 95103116 A RU95103116 A RU 95103116A
Authority
RU
Russia
Prior art keywords
landing gear
articulated
strut
rod
arm
Prior art date
Application number
RU95103116/11A
Other languages
Russian (ru)
Other versions
RU2088478C1 (en
Inventor
Э.А. Дубовский
В.Б. Фокин
Original Assignee
Акционерное общество открытого типа "ОКБ Сухого"
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 Акционерное общество открытого типа "ОКБ Сухого" filed Critical Акционерное общество открытого типа "ОКБ Сухого"
Priority to RU95103116A priority Critical patent/RU2088478C1/en
Publication of RU95103116A publication Critical patent/RU95103116A/en
Application granted granted Critical
Publication of RU2088478C1 publication Critical patent/RU2088478C1/en

Links

Landscapes

  • Fluid-Damping Devices (AREA)
  • Steering-Linkage Mechanisms And Four-Wheel Steering (AREA)

Abstract

FIELD: aeronautical engineering. SUBSTANCE: landing gear has leg 2 with breaker strut 7, wheeled bogie 5 with shock absorber 9. Wheeled bogie is articulated to strut by means of lever 11. Landing gear is provided with bogie turning mechanism which consists of system of articulated bell cranks 12 and 13 and rods 3 and 14. Double-arm bell crank 13 is articulated on strut; one arm of bell crank 13 is connected with rod 3 and other arm is connected to bell crank 12 by means of rod 14. EFFECT: enhanced efficiency of retracting the landing gear in fuselage. 3 cl, 7 dwg

Claims (1)

Изобретение относится к области авиационной техники. Изобретение решает задачу по укладыванию шасси в органическом объеме фюзеляжа. Шасси содержит стойку 2 со складывающимся подкосом 7, колесную тележку 5 с пяточным амортизатором 9. Колесная тележка шарнирно соединена со стойкой посредством рычага 11. Шасси снабжено механизмом разворота тележки, состоящим из системы шарнирных качалок 12 и 13 и тяг 3 и 14. Качалка 13 выполнена двуплечей, шарнирно закреплена на стойке и одним плечом соединена с тягой 3, а другим плечом посредством тяги 14 подсоединена к качалке 12.The invention relates to the field of aviation technology. The invention solves the problem of laying the chassis in the organic volume of the fuselage. The chassis contains a rack 2 with a folding brace 7, a wheeled trolley 5 with a heel shock absorber 9. The wheeled trolley is pivotally connected to the strut by a lever 11. The chassis is equipped with a trolley pivot mechanism consisting of a system of articulated rocking chairs 12 and 13 and rods 3 and 14. The rocking chair 13 is made two shoulders, pivotally mounted on the rack and with one shoulder connected to the rod 3, and the other shoulder through the rod 14 is connected to the rocking chair 12.
RU95103116A 1995-02-28 1995-02-28 Flying vehicle retractable landing gear RU2088478C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU95103116A RU2088478C1 (en) 1995-02-28 1995-02-28 Flying vehicle retractable landing gear

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU95103116A RU2088478C1 (en) 1995-02-28 1995-02-28 Flying vehicle retractable landing gear

Publications (2)

Publication Number Publication Date
RU95103116A true RU95103116A (en) 1996-12-20
RU2088478C1 RU2088478C1 (en) 1997-08-27

Family

ID=20165337

Family Applications (1)

Application Number Title Priority Date Filing Date
RU95103116A RU2088478C1 (en) 1995-02-28 1995-02-28 Flying vehicle retractable landing gear

Country Status (1)

Country Link
RU (1) RU2088478C1 (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ITRM20080043A1 (en) * 2008-01-24 2009-07-25 Magnaghi Aeronautica S P A AIRCRAFT CART
US8448900B2 (en) * 2010-03-24 2013-05-28 The Boeing Company Semi-levered landing gear and associated method
GB2510412C (en) * 2013-02-04 2021-08-25 Messier Dowty Ltd Aircraft landing gear pitch trimmer actuator with variable damping
CN110683062B (en) * 2019-09-29 2023-04-18 中国直升机设计研究所 Helicopter tail protection device

Also Published As

Publication number Publication date
RU2088478C1 (en) 1997-08-27

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Legal Events

Date Code Title Description
PD4A Correction of name of patent owner
PC43 Official registration of the transfer of the exclusive right without contract for inventions

Effective date: 20130527