System for airborne launch of an aircraft from a larger...

Aeronautics and astronautics – Composite aircraft

Reexamination Certificate

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Details

C244S00400R, C244S063000, C244S11000H, C244S13500B, C244S137400

Reexamination Certificate

active

06869042

ABSTRACT:
A system for launching, refuelling and recovering in flight an aircraft (10) such as an unmanned aerial vehicle (UAV) from a larger carrier aircraft (16) comprising a holder (22) on the carrier aircraft (16) to which the UAV (10) is detachably connectable and an extendable and retractable refuelling device (23, 24) on the carrier aircraft (16) detachably connectable to the UAV (10) whereby to launch the UAV it is disconnected from the holder (22), the refuelling device (23, 24) is extended with the UAV connected thereto to cause the UAV to trail behind the carrier aircraft and the UAV is then disconnected from the refuelling device.

REFERENCES:
patent: 4678141 (1987-07-01), Sarrantonio
patent: 4757959 (1988-07-01), Schroder et al.
patent: 5000398 (1991-03-01), Rashev
patent: 5131438 (1992-07-01), Loucks
patent: 5465923 (1995-11-01), Milner
patent: 5906336 (1999-05-01), Eckstein
patent: 6540179 (2003-04-01), Henderson
patent: 911457 (1949-07-01), None
patent: 472 927 (1992-03-01), None
patent: 676430 (1952-07-01), None
patent: 1821428 (1993-06-01), None
patent: WO 0054433 (2000-09-01), None

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