FIELD: aviation engineering. SUBSTANCE: system has pedals 1 and 2 for pilots mounted on the same main shaft 3 on hinges through vertical drive levers 4. Drive levers 4 have pedal position regulators 5. System has control wiring 6 for rudder 7 and control wiring 8 for nose-wheel 9. Horizontal transit shaft 10 has levers 11. Clips 12 are connected by hinges with levers 11 and with lower arms of drive levers 4 which are connected in hinges on the main shaft 3. Control winding 6 for rudder 7 is made from upper arms of drive levers 4 of different pedals 1 and 2 for both pilots. Control winding 8 for nose-wheel 9 is made from lower arms of the same levers 4. EFFECT: improved exploitation parameters; improved convenience of exploitation. 5 dwg
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Authors
Dates
1994-02-28—Published
1990-07-12—Filed