Inventors:
Alan Buitekant - Kent WA
David M. Dolliver - Bellevue WA
Assignee:
The Boeing Company - Seattle WA
International Classification:
B64D 112
Abstract:
The inner end of a hollow shaft (12) is releasably attached to a flight vehicle (2) by a ball-plunger type quick release mechanism. A rod (22) is axially slidable in the shaft (12) to release the shaft (12) from the vehicle (2). A plate (34) extends radially from the outer end (16) of the shaft (12) and abuts an outwardly facing surface of an external store (4) through which the shaft (12) and the rod (22) extend. The rim (48) of a cup-shaped retainer (42) interlocks with plate (34) to rotatably secure retainer (42) to plate (34). A solenoid (52) engages an arm (44) on retainer (42) to rotate retainer (42), release the interlocking engagement, and allow a spring (68) to move the retainer (42) axially outwardly. Retainer (42) contacts a shoulder (74) on rod (22) to move rod (22) axially outwardly. This releases shaft (12) from vehicle (2) and allows shaft (12) and store (4) to be separated from vehicle (2).