FIELD: aircraft engineering.
SUBSTANCE: invention relates to aircraft engineering, particularly to aircraft take-off-and-landing systems. Main telescopic leg of aircraft carriage with wheel semilevered suspension that is pivoted to airframe, bell-crank with wheel attachment axle rigid device, torque link and undercarriage leg release-and-retract device. Note that lower end of aforesaid rigid device is coupled with front arm of bell crank, while its upper end is pivoted to airframe at the point located outside rotational axis of shock-absorber strut in undercarriage retraction and release.
EFFECT: reduced length of undercarriage leg.
3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| FLYING VEHICLE RETRACTABLE LANDING GEAR | 1995 |
|
RU2088478C1 |
| SEMI-LEVERAGE UNDERCARRIAGE AND ITS UNDERCARRIAGE BEAM ARRANGEMENT | 2011 |
|
RU2564277C2 |
| AIRCRAFT LANDING GEAR WELL FRONT FLAP DRIVE | 2010 |
|
RU2427502C1 |
| AIRCRAFT RETRACTABLE LANDING GEAR | 2007 |
|
RU2389650C2 |
| DETECTION OF LOAD AT AIRCRAFT UNDERCARRIAGE | 2008 |
|
RU2478525C2 |
| AIRCRAFT RETRACTABLE LANDING GEAR | 2007 |
|
RU2415778C2 |
| AIRCRAFT UNDERCARRIAGE STRUT | 2005 |
|
RU2307046C2 |
| CHASSIS WITH FUSELAGE INSTALLATION | 2012 |
|
RU2617295C2 |
| DEVICE TO DECREASE AIRCRAFT UNDERCARRIAGE LENGTH | 2009 |
|
RU2488523C2 |
| AIRCRAFT RETRACTABLE LANDING GEAR | 2007 |
|
RU2415777C2 |
