FIELD: aeronautical engineering. SUBSTANCE: control mechanism has door lock with drive secured on flying vehicle fuselage and guide rail having pressing section with carriage connected with hatch door and its drive. Guide rail consists of two sections: one section is rigidly mounted on fuselage of flying vehicle; other section provided with retainer is articulated on fuselage by its front end; its rear end is connected with drive of lock engageable with retainer. Retainer of mechanism is made in the form of spring-loaded latch connected with double-arm lever by means of spring rod; double-arm lever is engageable with flying vehicle fuselage when door is open. EFFECT: reduction of mass.
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Authors
Dates
1996-10-27—Published
1977-03-28—Filed