SUPESONIC NOZZLE, IN PARTICULAR FOR A TURBOJET ENGINE
Assignee
SOCIETE NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION, S.N.E.C.M.A.
Filed
Nov 24, 1982
Granted
Aug 6, 1996
Location
SAINTRY SUR SEI FR
Abstract
A turbojet engine has an outlet duct to which an annular array of actuating cylinders for nozzle flaps are hinged. The housings for the cylinders are connected together by transverse members to form a rigid structure coaxial with the outlet duct. The arrangement includes convergent flaps and slaving devices for divergent flaps, all hinged to the rigid structure and particularly to the housings.
Source: Google Patents
35 USC §181 Secrecy Order
Imposed
Aug 25, 1983
Rescinded
Oct 11, 1995
Duration
12 years, 1 month
Inventor
- 1GERARD E. A. JOURDAIN
Record Details
- Patent number
- US 5542607
- Application
- 06448528
- Aerospace match
- Yes
- Dataset source
- 35 USC §181 SO records
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