THRUST NOZZLE FOR A GAS TURBINE ENGINE
Assignee
Filed
Jan 11, 1980
Granted
Jun 28, 2011
Location
ALLESTREE GB
35 USC §181 Secrecy Order
Imposed
Apr 1, 1982
Rescinded
Nov 23, 2010
Duration
28 years, 8 months
Inventor
- 1MAURICE TAYLOR
Record Details
- Patent number
- US 7967219
- Application
- 06116026
- Aerospace match
- Yes
- Dataset source
- 35 USC §181 SO records
More from this assignee
IMPROVED CATALITIC SYNTHESIS OF CAGED POLYNITRAMINE COMPOUNDS
SOLID ROCKET PROPELLANT
DUAL INFRARED BAND OBJECTIVE LENS
BANDGAP RADIATION DETECTOR
METHOD OF FORMING TEXTURED HIGH-TEMPERATURE SUPERCONDUCTORS
APPARATUS FOR CONTROLLING THE POSITION AND DIRECTION OF A LASER BEAM
Related by domain
GAS TURBINE ENGINE COMBUSTOR HAVING TRAPPED DUAL VORTEX CAVITY
General Electric
GAS TURBINE ENGINE FAN (U)
General Electric
TURNING VANE ARRANGEMENT FOR IR SUPPRESSORS
SIKORSKY AIRCRAFT CORPORATION
MODULAR ROCKET BOOSTED PENETRATING WARHEAD
LOCKHEED MARTIN CORP.
INTEGRAL SOLID BOOSTER AND HYBRID THRUST SUSTAINING SYSTEM AND PROJECTILE INCORPORATING THE SAME
ENVIRONMENTAL AEROSCIENCE CORPORATION
ROCKET MOTOR CASE USING PLANK SECTIONS AND METHODS OF MANUFACTURING
AEROJET-GENERAL CORPORATION