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Power Plants > Combustion Products Used As Motive Fluid > Combined With Regulation Of Power Output Feature Combined With Regulation Of Power Output FeatureCombined With Regulation Of Power Output Feature patent applications listed are from June 2005 to current and include Date, Patent Application Number, Patent Title, Patent Abstract summary and are linked to the corresponding patent application page.10/18/07 - 20070240426 - Mehtod and controller for operating a gas turbine engine A controller for operating a gas turbine engine, wherein the gas turbine engine is installable in an installation platform, wherein the gas turbine engine includes a compressor, a turbine, and a shaft connecting the turbine to the compressor. The controller includes a program which instructs the controller to run a ... 06/21/07 - 20070137217 - Engine with fuel/lubricant supply system for bearing lubrication A fuel lubrication additive injection system for fuel-lubricated gas turbine engines utilises high-pressure air developed by the engine to transfer stored fuel lubricant additive into the engine fuel stream that lubricates engine bearings. ... 12/14/06 - 20060277920 - Twin spool turbine engine with power take-off means on the low-pressure and high-pressure rotors, power take-off module for the turbine engine and method of assembling the turbine engine The invention relates to a twin spool turbine engine comprising a high-pressure rotor and a low-pressure rotor, at least one accessory gearbox, a drive means, driving coaxial transmission shafts that transmit movement to the accessory gearbox, characterized in that the drive means comprises a high-pressure drive pinion secured to the ... 11/23/06 - 20060260323 - Aircraft with disengageable engine and auxiliary power unit components Several improvements to an aircraft turbine engine and Auxiliary Power Unit (APU) are disclosed, as well as methods of using these improvements in routine and emergency aircraft operations. The improvements comprise the addition of cockpit-controllable clutches that can be used to independently disconnect the engine's integrated drive generator (IDG), engine ... 10/20/05 - 20050229605 - Hybrid inlet A turboprop powerplant with at least a compressor having a forward compressor inlet and a shaft extending axially through the compressor and having a shaft axis, an inlet duct encircling the shaft passing therethrough, the inlet duct having an aft end in gas communication with the compressor inlet and a ... ### FreshPatents.com Support |