JET PROPULSION POWERPLANTS
Assignee
BRITISH AEROSPACE PLC, 100 PALL MALL, LONDON, SW1Y 5HR, U.K. A BRITISH COMPANY
Filed
Dec 20, 1984
Granted
Dec 21, 1993
Location
PRESTON GB
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.
Source: Google Patents
35 USC §181 Secrecy Order
Imposed
Mar 11, 1986
Rescinded
Oct 22, 1992
Duration
6 years, 7 months
Inventor
- 1RONALD COE
Record Details
- Patent number
- US 5271222
- Application
- 06702407
- Aerospace match
- Yes
- Dataset source
- 35 USC §181 SO records
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