Patent Assignment
Reel/Frame 024140/0503
Change of Name
Recorded: 2010-03-26
Pages: 6
Assignor
SNECMA MOTEURS
Executed: 2005-06-27
Assignee
SNECMA
2 BD DU GENERAL MARTIAL VALIN, PARIS, 75015, FRANCE
Covered Properties
(78)
Thrust Vectoring Nozzle Assembly
Patent:
4,993,638 →
Application:
07/486,851 →
Seal for a Rotating Shaft
Patent:
5,039,115 →
Application:
07/490,306 →
Variable Stator Vane with Separate Guide Disk
Patent:
5,039,277 →
Application:
07/513,862 →
Compressor Casing for a Gas Turbine Engine
Patent:
5,154,578 →
Application:
07/597,024 →
System for Deforming a Turbine Stator Housing
Patent:
5,123,241 →
Application:
07/597,353 →
Cooling System for a Gas Turbine
Patent:
5,163,285 →
Application:
07/634,520 →
Jig Assembly for a Tool Support
Patent:
5,121,580 →
Application:
07/652,627 →
Friction Welding Method with Induction Heat Treating
Patent:
5,240,167 →
Application:
07/663,022 →
Turnbine Vane with Internal Cooling Circuit
Patent:
5,073,083 →
Application:
07/665,244 →
Control System for Oxidizer Intake Diaphragms
Patent:
5,159,807 →
Application:
07/694,256 →
Specular System for Recovering Laser Beam Energy
Patent:
5,173,583 →
Application:
07/706,308 →
Apparatus for Attaching a Pre-Atomization Bowl to a Gas Turbine Engine Combustion Chamber
Patent:
5,172,545 →
Application:
07/710,112 →
Casting Mold for Single Crystal Solidification Casting
Patent:
5,269,365 →
Application:
07/724,789 →
Apparatus for Detecting Impurities in a Fluid Circuit Using Optical Fibers and a Magnet
Patent:
5,173,600 →
Application:
07/765,931 →
Thrust Reverser for a High-Bypass Ratio Turbofan Engine
Patent:
5,255,510 →
Application:
07/885,611 →
System for Removably Mounting a Pre-Vaporizing Bowl to a Combustion Chamber
Patent:
5,222,358 →
Application:
07/909,691 →
Gas Turbine Engine Impeller Having an Annular Collar Platform
Patent:
5,263,823 →
Application:
07/917,181 →
Mounting System for a Stator Vane
Patent:
5,217,347 →
Application:
07/940,360 →
Anti-Flameout Safety System for a Gas Turbine Engine
Patent:
5,265,414 →
Application:
07/943,693 →
Turbojet-Ramjet Hypersonic Aircraft Engine
Patent:
5,284,014 →
Application:
07/961,319 →
System for Reducing Nitrogen-Oxide Emissions from a Gas Turbine Engine
Patent:
5,285,630 →
Application:
07/978,819 →
Fuel Injector for a Gas Turbine Engine
Patent:
5,242,117 →
Application:
07/996,129 →
Gas-Turbine Engine with Detachable Combustion Chamber
Patent:
5,524,430 →
Application:
08/004,606 →
Fuel Injector for a Turbojet Engine Afterburner
Patent:
5,297,391 →
Application:
08/032,484 →
Apparatus for Sumultaneously Molding Portions of Separable Article
Patent:
5,304,057 →
Application:
08/070,672 →
Cooling System for a Gas Turbine Engine Compressor
Patent:
5,297,386 →
Application:
08/098,864 →
Gas Turbine Engine with Improved Water Ingestion Prevention
Patent:
5,339,622 →
Application:
08/107,175 →
Combustion Chamber with Axially Displaced Fuel Injectors
Patent:
5,335,491 →
Application:
08/118,249 →
Afterburner for a Turbofan Engine
Patent:
5,400,589 →
Application:
08/132,245 →
Aerodynamic Fuel Injection System for a Gas Turbine Combustion Chamber
Patent:
5,351,475 →
Application:
08/136,263 →
Method and Apparatus for Detecting Internal Defects
Patent:
5,513,532 →
Application:
08/153,190 →
Variable Geometry Exhaust Nozzle for a Turbojet Engine
Patent:
5,359,851 →
Application:
08/155,217 →
Afterburner Assembly for a Gas Turbine Engine
Patent:
5,359,849 →
Application:
08/162,883 →
Safety Sealing Conduit Connector
Patent:
5,340,163 →
Application:
08/171,706 →
Method for Simultaneously Molding Portions of Separable Article
Patent:
5,443,784 →
Application:
08/188,730 →
Separator for an Annular Gas Turbine Combustion Chamber
Patent:
5,417,069 →
Application:
08/253,912 →
Removable Inspection Hole Plug
Patent:
5,431,534 →
Application:
08/276,885 →
Cladded Combustion Chamber Construction
Patent:
5,499,499 →
Application:
08/316,338 →
Gas-Flow Separator for a Double Dome Gas Turbine Engine Combustion Chamber
Patent:
5,528,896 →
Application:
08/337,537 →
Perforated Wall for a Gas Turbine Engine
Patent:
5,590,531 →
Application:
08/355,474 →
Variable Geometry Turbojet Engine Exhaust Nozzle
Patent:
5,494,221 →
Application:
08/375,477 →
Pre-Mixing Injection System for a Turbojet Engine
Patent:
5,592,819 →
Application:
08/400,574 →
System for Supplying Fuel to and Cooling a Fuel Injector of a Dual Head Combustion Chamber
Patent:
5,568,721 →
Application:
08/492,567 →
Self Regulating Bleed Valve
Patent:
5,531,566 →
Application:
08/518,721 →
Dual Head Combustion Chamber
Patent:
5,642,621 →
Application:
08/561,275 →
Method of Supplying Fuel to a Dual Head Combustion Chamber
Patent:
5,634,328 →
Application:
08/561,335 →
System for Regulating Oil and Fuel Temperatures of a Turbojet Engine
Patent:
5,615,547 →
Application:
08/582,613 →
Annular Combustion Chamber with a Perforated Wall
Patent:
5,713,207 →
Application:
08/660,599 →
Exhaust Nozzle Mixer for a Turbofan Engine
Patent:
5,755,092 →
Application:
08/732,926 →
Gas Turbine Engine Combustion Chamber for Optimizing the Mixture of Burned Gases
Patent:
5,934,067 →
Application:
08/845,133 →
Variable Geometry Turbojet Engine Exhaust Nozzle
Patent:
5,934,564 →
Application:
08/874,507 →
Reduced Pollution Combustion Chamber Having an Annular Fuel Injector
Patent:
5,937,653 →
Application:
08/884,668 →
Fuel Injection System with Improved Air/Fuel Homogenization
Patent:
5,941,075 →
Application:
08/912,815 →
Turbojet Engine Combustion Chamber with Heat Protecting Lining
Patent:
6,029,455 →
Application:
08/919,353 →
Aerodynamic Fuel Injection System for a Gas Turbine Engine
Patent:
6,035,645 →
Application:
08/939,084 →
Oxidizer Control Device for a Gas Turbine Engine
Patent:
5,996,333 →
Application:
08/950,017 →
Cooling System for Turbine Blade Platforms
Patent:
6,017,189 →
Application:
09/013,238 →
Thrust Reverser for a High Bypass Turbofan Engine
Patent:
6,050,522 →
Application:
09/022,277 →
Turbine Vane Cooling System
Patent:
5,993,156 →
Application:
09/104,200 →
Cooled Turbine-Nozzle Vane
Patent:
6,109,867 →
Application:
09/199,777 →
Ultrasonic Testing Method for a Part of Complex Geometry
Patent:
6,202,489 →
Application:
09/302,374 →
Converging Exhaust Nozzle Fitted with Translating Cold Flaps
Patent:
6,164,563 →
Application:
09/356,321 →
Turbo Jet Engine Exhaust Nozzle with Masked Gas Jet
Patent:
6,179,225 →
Application:
09/356,362 →
Turbojet Engine Thrust Reverser and Exhaust Nozzle
Patent:
6,289,670 →
Application:
09/479,077 →
Turbojet engine thrust reverser and exhaust nozzle assembly
Patent:
6,185,926 →
Application:
09/497,178 →
Axisymmetric, directable and adjustable turbojet-engine exhaust nozzle
Patent:
6,276,126 →
Application:
09/523,465 →
Swiveling, Converging-Diverging, Axisymmetric Exhaust Nozzle
Patent:
6,375,095 →
Application:
09/549,539 →
Axisymmetric, converging-diverging exhaust nozzle swiveled by a guided ring
Patent:
6,360,527 →
Application:
09/550,024 →
Universal-joint vectoring system for a turbojet-engine exhaust nozzle
Patent:
6,327,846 →
Application:
09/551,749 →
Axisymmetric, converging-diverging, jet-deflecting turbojet-engine exhaust-nozzle
Patent:
6,349,539 →
Application:
09/613,733 →
Suspension System with Intrinsic Safety Features for Aircraft Powerplants
Patent:
6,474,596 →
Application:
09/678,259 →
Blade Locking Device with Hammer Fastener on a Disk
Rotor Blade Retaining Apparatus
Bleed System Driven in Simplified Manner for a Turbojet or Turboprop Engine
Centripetal Air-Bleed System
Device for Centering a Tube in a Turbine Shaft
Gas Turbine Engine Axial Stator Compressor
Cylindrical Hole and Form Centring and Drilling Device