发明名称 |
AIRCRAFT UNDERCARRIAGE STRUT |
摘要 |
FIELD: aviation industry; aircraft takeoff and landing gears. ^ SUBSTANCE: aircraft undercarriage strut contains shock absorber 1 with piston connected with fulcrum 2 by braces 3, folding strut with down position lock and up position lock lug. Eyes are formed on lower part of piston in which cardan is installed hinge connected with lug whose upper part gets into up position lock. Stops made on cardan and on lug limit deflection of lug relative to longitudinal and lateral axes. ^ EFFECT: improved reliability of undercarriage in operation and closing of lock. ^ 3 dwg |
申请公布号 |
RU2307046(C2) |
申请公布日期 |
2007.09.27 |
申请号 |
RU20050128053 |
申请日期 |
2005.09.09 |
申请人 |
OTKRYTOE AKTSIONERNOE OBSHCHESTVO "AVIATSIONNYJ KOMPLEKS IM. S.V. IL'JUSHINA" |
发明人 |
SMIRNOV EVGENIJ IVANOVICH;DOLGOV VLADIMIR IL'ICH |
分类号 |
B64C25/10 |
主分类号 |
B64C25/10 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|