FIELD: aviation and rocket technology; docking units of aircraft compartments.
SUBSTANCE: multi-lever compartment docking system, including flanges of joined compartments, wherein the flange of one of the compartments is made removable, and the flange of the other compartment is presented in the form of a power frame. There are fixing grips that may rest with the other end on the abutting shelves, made on the flange of the opposite compartment, and distributed along its periphery. The system is equipped with clamping brackets. The contact surfaces of the fixing grips are made at an angle to the plane of connection of the flanges of the joined compartments.
EFFECT: design is simplified.
1 cl, 5 dwg
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RU2764879C1 |
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SU557557A1 |
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Authors
Dates
2023-03-29—Published
2022-05-06—Filed