FIELD: aeronautical engineering. SUBSTANCE: cargo hatch of flying vehicle is located in tail portion of fuselage 1 and has door 2 hinged on fuselage along aircraft axis by means of fore detachment unit 3 and tail detachment unit 4. Drive 5 is located in plane of symmetry of fuselage and is hinged on the door by means of detachable unit 6 and is linked with fuselage by means of articulated joint 7. EFFECT: facilitated procedure of opening and closing the door and enhanced reliability of its operation. 4 dwg
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Authors
Dates
1996-03-20—Published
1990-04-06—Filed