FIELD: aeronautical engineering. SUBSTANCE: articulated to tank is actuating cylinder 1 with floating piston 2 with cylindrical sleeve 3. Rod 8 is connected with door 10. On side of rod chamber piston 2 is provided with ball lock 6 with spring-loaded piston 7; on side of piston chamber A, it is provided with tab fastener engageable with lock 9 of rod 8. Fastener is made in form of sleeve 3 with inner cone divided into sectors 4 by longitudinal slots 5. Provided in bottom portion of chamber A is coaxial taper ring 21 engageable with inner cone of sleeve 2. EFFECT: reduced mass and improved service properties. 1 dwg
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0 |
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0 |
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0 |
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Authors
Dates
1995-11-27—Published
1987-05-27—Filed