Jet propulsion powerplants

Power plants – Reaction motor – With thrust direction modifying means

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Details

60230, 60262, 60 60, 60 3901, F02K 100

Patent

active

052712222

ABSTRACT:
A flow diverter arrangement for an aircraft comprises a first duct 17 for receiving propulsion fluid from the powerplant 11 and delivering it to a first location 18, a second duct 19 merging with the first duct 17 at a communication aperture 23 and adapted to deliver propulsion fluid to a second location, a flap member 24 pivotted for movement between a first position in which it closes the communication aperture 23 and a second position in which it closes the first duct, and a diverter device 31 for diverting propulsion fluid into the second duct when the flap member is in its second position.

REFERENCES:
patent: 3837411 (1974-09-01), Nash
patent: 4038818 (1977-08-01), Snell
patent: 4533095 (1985-08-01), Yates

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