FIELD: aircraft engineering. SUBSTANCE: handle disengagement mechanism 2 is made in the form of body 5 rotating relative to axle 6. The end of body 5 is pivotally connected to link 3. Pneumatic cylinder 7 with rod 8 and piston 9 is positioned inside body 5 for movement of pneumatic cylinder 7 along rod 6 connected to the other end of body 5. Link 4 is connected to pneumatic cylinder 7. EFFECT: improved flight safety. 1 dwg
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Authors
Dates
1994-06-30—Published
1991-06-03—Filed