FIELD: aeronautical engineering. SUBSTANCE: device includes housing where extensible shaft with control wheel is mounted; shaft is provided with gear engaged with wheel of drive shaft mounted in housing and connected with carrier which is input member of intermediate nonlinear mechanism containing bell crank articulated with carrier and output lever through trunnions movably located in slots made in carrier Output lever is rigidly connected with shaft of control system sensor through plate. Sensor is electrically connected with control unit. EFFECT: enhanced efficiency. 4 dwg
Title | Year | Author | Number |
---|---|---|---|
AIRCRAFT NOSE UNDERCARRIAGE CONTROL SYSTEM | 1992 |
|
RU2070140C1 |
LOAD-BEARING LOCK OF AIRCRAFT LANDING GEAR | 1993 |
|
RU2068799C1 |
AIRCRAFT LANDING GEAR FRONT SUPPORT CONTROL UNIT (VERSIONS) | 2018 |
|
RU2695967C1 |
DEVICE FOR CONNECTION OF SENSOR SHAFT WITH SWIVEL MEMBER OF ACTUATING MECHANISM | 1993 |
|
RU2068798C1 |
AIRCRAFT LANDING GEAR FRONT LEG CONTROL DEVICE | 2009 |
|
RU2395428C1 |
FLYING VEHICLE CARGO CABIN FOR TRANSPORTATION OF CARGO IN CONTAINERS | 1995 |
|
RU2092386C1 |
FLYING VEHICLE MANUAL CONTROL STATION | 1996 |
|
RU2122509C1 |
DEVICE FOR OPENING HATCH COVER | 1995 |
|
RU2104217C1 |
AIRCRAFT LANDING GEAR FRONT CONTROL MODES SWITCH (VERSIONS), SWITCH ASSEMBLY AND SWITCH POWER FRAME | 2018 |
|
RU2695942C1 |
FLYING VEHICLE RETRACTABLE LANDING GEAR | 1995 |
|
RU2088478C1 |
Authors
Dates
1997-11-27—Published
1992-11-27—Filed