FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to retractable landing gear. Proposed landing gear comprises leg 1 secured by suspension 2 to fuselage and articulated with folding brace 4 articulated with landing gear retraction drive 9, gear truck 3, damping cylinder 5, as well as gear truck turn mechanism with tie rod articulated with fuselage and damping cylinder 5. Said tie rod 6 is articulated with damping cylinder via ring 10 with lever 7 arranged on damping cylinder to rotate thereon and jointed with top link of splined hinge. Lever 7 is rigidly secured on ring 10 and has its free end pivoted to tie rod 6 of gear truck turn mechanism.
EFFECT: simplified design of landing gear.
2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIRCRAFT RETRACTABLE LANDING GEAR | 2007 |
|
RU2389650C2 |
| FLYING VEHICLE RETRACTABLE LANDING GEAR | 1995 |
|
RU2088478C1 |
| PIRAMIDAL UNDERCARRIAGE OF AIRCRAFT RETRACTABLE SKI LANDING GEAR | 0 |
|
SU593400A1 |
| AIRCRAFT RETRACTABLE LANDING GEAR | 2007 |
|
RU2415778C2 |
| 0 |
|
SU305633A1 | |
| AIRCRAFT LANDING GEAR WELL FRONT FLAP DRIVE | 2010 |
|
RU2427502C1 |
| METHOD OF FLYING VEHICLE CLEARANCE CHANGE AT PARKING AND ACTUATING STRUT (VERSIONS) | 2016 |
|
RU2628002C1 |
| RETRACTABLE SKI LANDING GEAR FOR FLYING VEHICLE | 1984 |
|
RU1213659C |
| CHASSIS WITH FUSELAGE INSTALLATION | 2012 |
|
RU2617295C2 |
| AIRCRAFT RETRACTABLE SKI UNDERCARRIAGE MAIN SUPPORT | 0 |
|
SU575839A1 |
