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Louis J. Casaregola

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Edits on 28 Nov, 2022
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edited on 28 Nov, 2022
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The Deer Hunter
The Deer Hunter
Edits on 14 Dec, 2021
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edited on 14 Dec, 2021
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Patent primary examiner of
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US Patent 7089744 Onboard supplemental power system at varying high altitudes
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US Patent 7093420 Flow divider and ecology valve
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US Patent 7093423 Methods and apparatus for operating gas turbine engines
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US Patent 7093437 Extended operability aircraft fuel delivery system
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US Patent 7093443 Gas turbine apparatus
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US Patent 7094033 Methods and apparatus for assembling gas turbine engines
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US Patent 7096657 Gas turbine engine electromechanical variable inlet guide vane actuation system
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US Patent 7096658 Centrifugal pump fuel system and method for gas turbine engine
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US Patent 7096659 Gas turbine electric power generation equipment and air humidifier
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US Patent 7096660 Plasma impulse device
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US Patent 7096667 Control of gas turbine for catalyst activation
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US Patent 7096669 Method and apparatus for the prevention of critical process variable excursions in one or more turbomachines
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US Patent 7096672 Fluid heating and gas turbine integration method
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US Patent 7096673 Blade tip clearance control
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US Patent 7100355 Battle override valve
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US Patent 7100357 System for controlling gas turbine by adjusting a target exhaust temperature
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US Patent 7100359 Gas turbine installation
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US Patent 7100377 Methods for operating gas turbine engines
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US Patent 7100378 Method and apparatus for controlling fuel flow to an engine
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US Patent 7104070 Liquid fuel nozzle apparatus with passive water injection purge
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US Patent 7104071 Method for operating a gas turbine group
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US Patent 7107773 Turbine engine sequenced combustion
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US Patent 7111462 Onboard supplemental power system at varying high altitudes
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US Patent 7111464 Acceleration control in multi spool gas turbine engine
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US Patent 7114336 Flow pulsing valve and fuel supply system for a turbine engine incorporating same
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US Patent 7117662 Gas turbine control system
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US Patent 7117663 Air breathing, hydrogen fueled jet engine for high speed aircraft
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US Patent 7124573 Rotary pulse detonation system with aerodynamic detonation passages for use in a gas turbine engine
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US Patent 7124590 Ejector for cooling air supply pressure optimization
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US Patent 7127897 Combustion chamber
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US Patent 7131259 High density combined cycle power plant process
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US Patent 7134269 Gas turbine engine
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US Patent 7134284 Modular fuel conditioning system
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US Patent 7137242 Fuel system
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US Patent 7146794 Gas turbine installation
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US Patent 7165405 Fully premixed secondary fuel nozzle with dual fuel capability
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US Patent 7188475 Starting and controlling speed of a two spool gas turbine engine
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US Patent RE39796 Method of eliminating mach waves from supersonic jets
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US Patent 7406828 Power augmentation of combustion turbines with compressed air energy storage and additional expander with airflow extraction and injection thereof upstream of combustors
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US Patent 7418814 Dual expander cycle rocket engine with an intermediate, closed-cycle heat exchanger
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US Patent 7421835 Air-staged reheat power generation system
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US Patent 7428817 Premix burner with a swirl generator delimiting a conical swirl space and having sensor monitoring
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US Patent 7428818 System and method for augmenting power output from a gas turbine engine
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US Patent 7430850 Bifurcated oil scavenging bearing compartment within a gas turbine engine
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US Patent 7434406 Drive for using a direct driven generator to start a counter-rotating multi-spool gas turbine engine
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US Patent 7437871 Automatic engine protection system for use when electronic parts of a control system are exposed to overtemperature conditions
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US Patent 7441398 NOx adjustment system for gas turbine combustors
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US Patent 7448215 Combustion chamber for a gas turbine engine
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US Patent 7448217 Power plant
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US Patent 7448220 Torque control for starting system
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US Patent 7451599 Fuel manifold inlet tube
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US Patent 7451601 Method of tuning individual combustion chambers in a turbine based on a combustion chamber stratification index
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US Patent 7451602 Methods and apparatus for injecting fluids into turbine engines
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US Patent 7464533 Apparatus for operating gas turbine engines
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US Patent 7464536 Methods and apparatus for assembling gas turbine engines
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US Patent 7469543 Rich catalytic injection
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US Patent 7469545 Auxiliary power unit inlet door position control system and method
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US Patent 7472541 Compressor control unit and gas turbine power plant including this unit
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US Patent 7475532 Valve assembly for a gas turbine engine
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US Patent 7475549 Thermal management system for a gas turbine engine
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US Patent 7478524 Coal fired power generation plant
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US Patent 7481061 Fuel control for starting a gas turbine engine
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US Patent 7484352 Combustor for a gas turbine
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US Patent 7484369 Apparatus for observing combustion conditions in a gas turbine engine
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US Patent 7487642 Methods and apparatus for operating gas turbine engines
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US Patent 7493752 Control system for aircraft engine
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US Patent 7497083 Fuel supply system
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US Patent 7500353 Eductor swirl buster
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US Patent 7500364 System for coupling flow from a centrifugal compressor to an axial combustor for gas turbines
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US Patent 7503178 Thermal power plant with sequential combustion and reduced-CO
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US Patent 7506496 Effervescent aerodynamic system for injecting an air/fuel mixture into a turbomachine combustion chamber
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US Patent 7506501 Compact mixer with trimmable open centerbody
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US Patent 7506512 Advanced effusion cooling schemes for combustor domes
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US Patent 7506514 Augmentor fuel conduit bushing
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US Patent 7506515 Method for regulating fuel flow into a turbine
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US Patent 7509793 Fluid system
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US Patent 7509796 Pintle-controlled propulsion system with external dynamic seal
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US Patent 7509810 Inter-turbine temperature display compensation method
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US Patent 7509813 Combustor heat shield
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US Patent 7513099 Temperature measuring device and regulation of the temperature of hot gas of a gas turbine
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US Patent 7513100 Systems for low emission gas turbine energy generation
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US Patent 7516607 Method and apparatus for mixing substances
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US Patent 7516609 Carbon dioxide recirculation
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US Patent 7516621 Modular LRU accessory mounting substrate for auxiliary power unit
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US Patent 7520135 Variable-section turbomachine nozzle
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US Patent 7523604 Thrust reverser mounting structure
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US Patent 7526912 Pulse detonation engines and components thereof
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US Patent 7530216 Control system for a gas turbine engine
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US Patent 7530218 Pulsed plasma thruster using vapor
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US Patent 7530232 Method for regulating the flow rate of fuel to a turboshaft engine in acceleration or in deceleration
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US Patent 7533517 Exhaust nozzle for an engine of a flying craft
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US Patent 7536850 Emergency fuel shutoff system
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US Patent 7540144 Bleed valve for a gas turbine engine
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US Patent 7540156 Combustion liner for gas turbine formed of cast nickel-based superalloy
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US Patent 7543439 Generator assembly
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US Patent 7543441 Hall-effect plasma thruster
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US Patent 7546738 Turbine engine nozzle
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US Patent 7546741 Ignition detecting system and method for gas turbine
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US Patent 7546743 Bolting configuration for joining ceramic combustor liner to metal mounting attachments
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US Patent 7549282 Multi-slot inter-turbine duct assembly for use in a turbine engine
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US Patent 7549291 Methods and apparatus for operating gas turbine engines
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US Patent 7549292 Method of controlling bypass air split to gas turbine combustor
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US Patent 7549293 Pressure control method to reduce gas turbine fuel supply pressure requirements
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US Patent 7552591 Twin spool turbine engine with power take-off means on the low-pressure and high-pressure rotors, and power take-off module for the turbine engine
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US Patent 7555892 Cooling system for a gas turbine
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US Patent 7559191 Ducted spinner for engine cooling
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US Patent 7559202 Reduced thermal stress fuel nozzle assembly
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US Patent 7565793 Gas turbine engine fuel control system having start / back up check valve (SBUC) providing a main fuel check valve function
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US Patent 7565794 Premix burner for a gas turbine combustion chamber
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US Patent 7565805 Method for operating gas turbine engine systems
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US Patent 7568347 Method for designing flowfield molded hypersonic inlet for integrated turbojet and ram-scramjet applications
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US Patent 7568349 Method for controlling combustion device dynamics
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US Patent 7574864 Diffuser for a gas turbine, and gas turbine for power generation
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US Patent 7578121 Thrust termination device for solid rocket motor
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US Patent 7581379 Gas turbine power generating machine
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US Patent 7581385 Metering sheet and iso-grid arrangement for a non axi-symmetric shaped cooling liner within a gas turbine engine exhaust duct
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US Patent 7581399 Damped coil pin for attachment hanger hinge
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US Patent 7581401 Methods and apparatus for cooling gas turbine engine components
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US Patent 7584602 Augmentor flow control with thermal recirculation function using augmentor valves
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US Patent 7584616 Method for the operation of a gas turbo group
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US Patent 7587900 Gas turbine engine fuel control system having a transfer valve and a shutoff valve and a common controller therefor
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US Patent 7594386 Apparatus for the prevention of critical process variable excursions in one or more turbomachines
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US Patent 7594387 Modified fuel burning gas turbine
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US Patent 7596953 Method for detecting compressor stall precursors
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US Patent 7600369 Gas turbine load control device
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US Patent 7603840 LNG power plant
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US Patent 7603842 Method for reducing the nonsteady side loads acting on a nozzle of a rocket engine
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US Patent 7603860 High efficiency flexfuel internal combustion engine
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US Patent 7610745 Combustion control device for gas turbine
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US Patent 7610746 Combustion control device for gas turbine
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US Patent 7610760 Two-displacement setting variable displacement pump used as engine over-thrust protection with fuel system thermal benefit
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US Patent 7610762 High efficiency thermal engine
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US Patent 7614237 CAES system with synchronous reserve power requirements
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US Patent 7614238 Method for lean blowout protection in turbine engines
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US Patent 7617688 Combustion chamber of a gas turbine engine with an upstream fairing for separating the gas stream, annular wall forming a cap of the upstream fairing of the chamber, and gas turbine engine with the chamber
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US Patent 7621132 Pilot combustor for stabilizing combustion in gas turbine engines
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US Patent 7621133 Methods and apparatus for starting up combined cycle power systems
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US Patent 7624579 Convergent divergent nozzle with supported divergent seals
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US Patent 7628006 Thrust termination device for solid rocket motor
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US Patent 7631486 Thrust orienting nozzle
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US Patent 7634916 Stiffener for low pressure compressor for an aircraft engine
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US Patent 7640643 Conversion of combined cycle power plant to compressed air energy storage power plant
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US Patent 7640726 Injector assembly having multiple manifolds for propellant delivery
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US Patent 7640752 Device for guiding an element in an orifice in a wall of a turbomachine combustion chamber
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US Patent 7644575 Morphing structure
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US Patent 7647778 Engine arrangements and control
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US Patent 7654075 Fan static structure
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US Patent 7658060 Lubricant cooling exchanger dual intake duct
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US Patent 7658061 Gas turbine engine provided with a foreign matter removal passage
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US Patent 7665293 Low speed rotor shaft for a small twin spool gas turbine engine
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US Patent 7665294 Exhaust nozzle assembly
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US Patent 7665308 Methods and apparatus for injecting fluids into a turbine engine
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US Patent 7669422 Combustor liner and method of fabricating same
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US Patent 7669423 Operating method for CAES plant using humidified air in a bottoming cycle expander
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US Patent 7669424 Combustor assembly
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US Patent 7673442 Turbofan engine cowl assembly
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US Patent 7673459 System and method for providing air to a compressor of an aircraft auxiliary gas turbine engine
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US Patent 7673460 System of attaching an injection system to a turbojet combustion chamber base
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US Patent 7677046 Method for starting a pressure storage plant
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US Patent 7685805 Turbofan gas turbine engine and nacelle arrangement
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US Patent 7685807 Three component injector for kerosene-oxygen rocket engine
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US Patent 7685822 Rotary cup fuel injector
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US Patent 7690185 System for driving accessory machines of a double-bodied turbine engine
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US Patent RE41229 Methods and apparatus for regulating gas turbine engine fluid flow
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US Patent 7707814 Fuel-flow-rate control device for power generation system
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US Patent 7712300 Water treatment and pressurization system for the adiabatic cooling of comburent air
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US Patent 7716933 Multi-channel fuel manifold
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US Patent 7721522 Torque load transfer attachment hardware
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US Patent 7721545 Device for injecting a mixture of air and fuel, combustion chamber and turbomachine both equipped with such a device
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US Patent 7726115 Axial flow positive displacement worm compressor
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US Patent 7762080 Fuel metering pump calibration method
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US Patent 8001762 Method and device to increase thrust and efficiency of jet engine
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US Patent 8001786 Combustor of a gas turbine engine
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US Patent 8001787 Transition support system for combustion transition ducts for turbine engines
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US Patent 8006479 Thrust reversing variable area nozzle
Edits on 8 Dec, 2021
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Golden AI
edited on 8 Dec, 2021
Edits made to:
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Infobox
Patent primary examiner of
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US Patent 8006479 Thrust reversing variable area nozzle
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Golden AI
edited on 8 Dec, 2021
Edits made to:
Infobox (+1 properties)
Infobox
Patent primary examiner of
‌
US Patent 8001787 Transition support system for combustion transition ducts for turbine engines
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Golden AI
edited on 8 Dec, 2021
Edits made to:
Infobox (+1 properties)
Infobox
Patent primary examiner of
‌
US Patent 8001786 Combustor of a gas turbine engine
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Golden AI
edited on 8 Dec, 2021
Edits made to:
Infobox (+1 properties)
Infobox
Patent primary examiner of
‌
US Patent 8001762 Method and device to increase thrust and efficiency of jet engine
Edits on 5 Dec, 2021
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Golden AI
edited on 5 Dec, 2021
Edits made to:
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Patent primary examiner of
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US Patent 7762080 Fuel metering pump calibration method
Edits on 4 Dec, 2021
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Golden AI
edited on 4 Dec, 2021
Edits made to:
Infobox (+1 properties)
Infobox
Patent primary examiner of
‌
US Patent 7726115 Axial flow positive displacement worm compressor
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Golden AI
edited on 4 Dec, 2021
Golden AI profile picture
Golden AI
edited on 4 Dec, 2021
Edits made to:
Infobox (+1 properties)
Infobox
Patent primary examiner of
‌
US Patent 7721522 Torque load transfer attachment hardware
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Golden AI
edited on 4 Dec, 2021
Edits made to:
Infobox (+1 properties)
Infobox
Patent primary examiner of
‌
US Patent 7716933 Multi-channel fuel manifold
Golden AI profile picture
Golden AI
edited on 4 Dec, 2021
Edits made to:
Infobox (+1 properties)
Infobox
Patent primary examiner of
‌
US Patent 7712300 Water treatment and pressurization system for the adiabatic cooling of comburent air
Golden AI profile picture
Golden AI
edited on 4 Dec, 2021
Edits made to:
Infobox (+1 properties)
Infobox
Patent primary examiner of
‌
US Patent 7707814 Fuel-flow-rate control device for power generation system
Edits on 4 Dec, 2021
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Golden AI
edited on 4 Dec, 2021
Edits made to:
Infobox (+1 properties)
Infobox
Patent primary examiner of
‌
US Patent RE41229 Methods and apparatus for regulating gas turbine engine fluid flow
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Golden AI
edited on 4 Dec, 2021
Edits made to:
Infobox (+1 properties)
Infobox
Patent primary examiner of
‌
US Patent 7690185 System for driving accessory machines of a double-bodied turbine engine
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Golden AI
edited on 4 Dec, 2021
Edits made to:
Infobox (+1 properties)
Infobox
Patent primary examiner of
‌
US Patent 7685822 Rotary cup fuel injector
Golden AI profile picture
Golden AI
edited on 4 Dec, 2021
Edits made to:
Infobox (+1 properties)
Infobox
Patent primary examiner of
‌
US Patent 7685807 Three component injector for kerosene-oxygen rocket engine
Golden AI profile picture
Golden AI
edited on 4 Dec, 2021
Edits made to:
Infobox (+1 properties)
Infobox
Patent primary examiner of
‌
US Patent 7685805 Turbofan gas turbine engine and nacelle arrangement
Golden AI profile picture
Golden AI
edited on 4 Dec, 2021
Edits made to:
Infobox (+1 properties)
Infobox
Patent primary examiner of
‌
US Patent 7677046 Method for starting a pressure storage plant
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Golden AI
edited on 4 Dec, 2021
Edits made to:
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Infobox
Patent primary examiner of
‌
US Patent 7673460 System of attaching an injection system to a turbojet combustion chamber base

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