FIELD: aircraft engineering.
SUBSTANCE: proposed ejector comprises the spring contracted at initial position to be retained in said as-contracted position between airframe and cargo bed with the help of locking mechanism. Locking mechanism comprises self-releasing screw pair fitted on rod, sleeve being secured to cargo bed while sleeve can turn about said rod and to press the cargo bed against contracted spring. Lever is rigidly secured to said sleeve, lever end being connected with retainer. Locking mechanism comprises the appliance which can destruct said retainer.
EFFECT: simplified design.
10 cl, 3 dwg
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