EXHAUST NOZZLE COUPLED WITH REVERSER EXHAUST DOOR
Assignee
UNITED TECHNOLOGIES CORPORATION, A CORP OF DE
Filed
Nov 2, 1984
Granted
Sep 1, 1987
Location
PALM SPRINGS FL US
Abstract
A convergent/divergent gas turbine engine exhaust nozzle having reverse thrust capability includes a door which blocks a reverse flow outlet port when the nozzle convergent flap is in any forward thrust operating mode. The door is coupled to the convergent nozzle flap such that it opens as the convergent nozzle flap moves to a reverse thrust position and the flap directs the exhaust gases through the reverser outlet.
Source: Google Patents
35 USC §181 Secrecy Order
Imposed
Mar 4, 1986
Rescinded
Sep 5, 1986
Duration
6 months
Inventor
- 1WILLIAM M. MADDEN
Record Details
- Patent number
- US 4690329
- Application
- 06667707
- Aerospace match
- Yes
- Dataset source
- 35 USC §181 SO records
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