| Patent No. | Patent Title: |
| 7762080 | Fuel metering pump calibration method |
| 7726115 | Axial flow positive displacement worm compressor |
| 7721545 | Device for injecting a mixture of air and fuel, combustion chambe... |
| 7721522 | Torque load transfer attachment hardware |
| 7716933 | Multi-channel fuel manifold |
| 7712300 | Water treatment and pressurization system for the adiabatic cooli... |
| 7707814 | Fuel-flow-rate control device for power generation system |
| RE41229 | Methods and apparatus for regulating gas turbine engine fluid flo... |
| 7698897 | Engine control |
| 7690185 | System for driving accessory machines of a double-bodied turbine ... |
| 7685807 | Three component injector for kerosene-oxygen rocket engine |
| 7685822 | Rotary cup fuel injector |
| 7685805 | Turbofan gas turbine engine and nacelle arrangement |
| 7677046 | Method for starting a pressure storage plant |
| 7673442 | Turbofan engine cowl assembly |
| 7673460 | System of attaching an injection system to a turbojet combustion ... |
| 7673459 | System and method for providing air to a compressor of an aircraf... |
| 7669423 | Operating method for CAES plant using humidified air in a bottomi... |
| 7669424 | Combustor assembly |
| 7669422 | Combustor liner and method of fabricating same |
| 7665294 | Exhaust nozzle assembly |
| 7665293 | Low speed rotor shaft for a small twin spool gas turbine engine |
| 7665308 | Methods and apparatus for injecting fluids into a turbine engine |
| 7658060 | Lubricant cooling exchanger dual intake duct |
| 7658061 | Gas turbine engine provided with a foreign matter removal passage |
| 7654075 | Fan static structure |
| 7647778 | Engine arrangements and control |
| 7644575 | Morphing structure |
| 7640726 | Injector assembly having multiple manifolds for propellant delive... |
| 7640643 | Conversion of combined cycle power plant to compressed air energy... |
| 7640752 | Device for guiding an element in an orifice in a wall of a turbom... |
| 7634916 | Stiffener for low pressure compressor for an aircraft engine |
| 7631486 | Thrust orienting nozzle |
| 7628006 | Thrust termination device for solid rocket motor |
| 7624579 | Convergent divergent nozzle with supported divergent seals |
| 7621133 | Methods and apparatus for starting up combined cycle power system... |
| 7621132 | Pilot combustor for stabilizing combustion in gas turbine engines |
| 7617688 | Combustion chamber of a gas turbine engine with an upstream fairi... |
| 7614238 | Method for lean blowout protection in turbine engines |
| 7614237 | CAES system with synchronous reserve power requirements |
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