RU95103116A - Flying vehicle retractable landing gear - Google Patents
Flying vehicle retractable landing gearInfo
- 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
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)
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)
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 |
-
1995
- 1995-02-28 RU RU95103116A patent/RU2088478C1/en active
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 |