GAS TURBINE ENGINE
Assignee
ROLLS-ROYCE LIMITED
Filed
Sep 12, 1983
Granted
Apr 28, 1992
Location
BRISTOL GB
Abstract
A gas turbine engine of the type comprising a first compressor 4, a second compressor 6, a combustor 8 and turbines 10 for driving the compressors 4 and 6 is provided with an air intake 16, leading to the second compressor 6. The flow from the first compressor 4 is discharged through vectorable nozzles 12,14. The nozzles 12,14 are movable between a first position where they discharge to ambient and a second position where they register with the intake 16 and the flow from the first compressor 4 discharges to the second compressor 6.
Source: Google Patents
35 USC §181 Secrecy Order
Imposed
Mar 27, 1984
Rescinded
Aug 30, 1991
Duration
7 years, 5 months
Inventor
- 1DEREK A. ROBERTS
Record Details
- Patent number
- US 5107675
- Application
- 06534573
- Aerospace match
- Yes
- Dataset source
- 35 USC §181 SO records
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