AXISYMMETRIC VECTORING EXHAUST NOZZLE THERMAL SHIELD
Assignee
Filed
Jun 7, 1993
Granted
Jan 23, 1996
Location
WEST CHESTER OH US
Abstract
A thrust vectoring axisymmetric vectoring exhaust nozzle having universally pivoting divergent flaps is provided with a surrounding thermal shield of overlapping outer flaps and seals generally disposed in an aftwards converging conical arrangement and having a means for changing its shape from axisymmetrical to asymmetrical. Additional thermal and cooling protection is provided by a series of ejector slots located on the divergent universally pivotal flaps and adjacent interflap seals of the nozzle to both cool and thermally shield the flaps and seals.
Source: Google Patents
35 USC §181 Secrecy Order
Imposed
Oct 20, 1993
Rescinded
Jan 13, 1994
Duration
2 months
Inventor
- 1JONATHAN M. WOOD
Record Details
- Patent number
- US 5485959
- Application
- 08072678
- Aerospace match
- Yes
- Dataset source
- 35 USC §181 SO records
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