NOZZLE FOR A JET ENGINE CONTANING AN ADJUSTABLE CONVERGENT-DIVERGENT PORTION
Assignee
SOCIETE NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION, S.N.E.C.M.A.
Filed
Jan 13, 1981
Granted
May 28, 1996
Location
ROCK CREEK MD US
Abstract
A nozzle comprises: a set of first flaps articulated to a rigid structure, and forming a convergent; a set of second flaps each articulated to a corresponding first flap, and forming a divergent; a set of third flaps each of which is connected at a position between two adjacent second flaps and which is, on the one hand, articulated to the rigid structure and, on the other hand, linked to each of the two adjacent second flaps by carrier linked to the aforesaid third flap by a ball joint.
Source: Google Patents
35 USC §181 Secrecy Order
Imposed
Sep 21, 1983
Rescinded
Jun 28, 1995
Duration
11 years, 9 months
Inventor
- 1GERARD E. A. JOURDAIN
Record Details
- Patent number
- US 5520336
- Application
- 06237399
- Aerospace match
- Yes
- Dataset source
- 35 USC §181 SO records
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