FIELD: aircraft engineering.
SUBSTANCE: landing gear comprises two bobs to carry wheels. said bobs turn on common pivot shafts. Landing gear comprises also a damper with two connection rods, each being connected with appropriate bob. One connection rod, a telescoping component, makes the damper. Two connection rods are connected with swinging lever arranged to turn on central pivot shaft. Common pivot shaft of bobs if rigidly jointed with airframe and locked thereat. Central pivot shaft of swinging lever can displace between first position whereat bobs stay in aircraft landing position and second position whereat swinging lever is pulled to connection rods to make bobs turn to retracted position.
EFFECT: reliable and simplified design.
5 cl, 6 dwg
Title | Year | Author | Number |
---|---|---|---|
AIRCRAFT UNDERCARRIAGE WITH BALANCE BEAM AND DEFORMING PARALLELOGRAM | 2011 |
|
RU2549580C2 |
DEVICE TO DECREASE AIRCRAFT UNDERCARRIAGE LENGTH | 2009 |
|
RU2488523C2 |
AIRCRAFT RETRACTABLE LANDING GEAR | 2007 |
|
RU2389650C2 |
DETECTION OF LOAD AT AIRCRAFT UNDERCARRIAGE | 2008 |
|
RU2478525C2 |
PIRAMIDAL UNDERCARRIAGE OF AIRCRAFT RETRACTABLE SKI LANDING GEAR | 0 |
|
SU593400A1 |
AIRCRAFT RETRACTABLE LANDING GEAR LEG | 2014 |
|
RU2545239C1 |
AIRCRAFT UNDERCARRIAGE INCORPORATING DRIVE WITH BRACE, AND AIRCRAFT WITH SUCH UNDERCARRIAGE | 2006 |
|
RU2424948C2 |
MAIN LEG OF AIRCRAFT UNDERCARRIAGE | 2007 |
|
RU2371353C2 |
AIRCRAFT RETRACTABLE LANDING GEAR | 2013 |
|
RU2539623C1 |
AIRCRAFT | 1992 |
|
RU2023628C1 |
Authors
Dates
2014-06-20—Published
2011-06-16—Filed