FIELD: aviation. SUBSTANCE: control column has case, onto which guides of carriage are mounted, carriage, provided with support and rotatable handle, which is kinematically connected with in roll and in pitch position transducers. Axis of rotation of the handle is aligned with axis of guide of the carriage. Kinematical coupling with in roll position transducer is made in form of spring-loaded carrier, connected with case of the detector and mounted onto the arm-piece, which is rigidly connected with the carriage. Gear transmission of kinematical coupling has gear fixed onto input unit of the transducer, and wheel of gear transmission is fixed to edge of support of rotatable handle. Kinematical coupling with in pitch position transducer is made in form of spring-loaded carrier, mounted onto the case, lever, which is connected with carriage through link, and transmission gear, which has gear, attached to input shaft of the transducer, and gear sector, mounted onto the lever. The lever is connected by hinges with load pitch cylinder, which is mounted by hinges onto the case. Support of rotatable handle is spring-loaded. EFFECT: improved convenience of control; improved safety of flight. 6 dwg
Title | Year | Author | Number |
---|---|---|---|
AIRCRAFT LANDING GEAR FRONT LEG CONTROL DEVICE | 2009 |
|
RU2395428C1 |
DEVICE FOR CONTROL OF SENSOR SHAFT OF AIRCRAFT UNDERCARRIAGE LEG CONTROL SYSTEM | 1992 |
|
RU2097271C1 |
LOAD-BEARING LOCK OF AIRCRAFT LANDING GEAR | 1993 |
|
RU2068799C1 |
AIRCRAFT CREW CABIN WINDOW LEAF | 2011 |
|
RU2475413C1 |
AIRCRAFT SIDE-STICK CONTROL | 2014 |
|
RU2571992C1 |
AIRCRAFT NOSE UNDERCARRIAGE CONTROL SYSTEM | 1992 |
|
RU2070140C1 |
AIRCRAFT MANUAL CONTROL DEVICE | 2016 |
|
RU2652284C1 |
AIRCRAFT LANDING GEAR FRONT SUPPORT CONTROL UNIT (VERSIONS) | 2018 |
|
RU2695967C1 |
AIRCRAFT NOSE UNDERCARRIAGE LEG | 1997 |
|
RU2123961C1 |
ADAPTIVE LOAD SIMULATOR FOR CONTROL LEVERS OF AIRCRAFT SIMULATOR | 2002 |
|
RU2231127C1 |
Authors
Dates
1994-08-30—Published
1991-06-28—Filed