Patents
Patents for F02C 7 - Features, component parts, details or accessories, not provided for in, or of interest apart from, groups; Air intakes for jet-propulsion plants (30,889)
06/2010
06/29/2010CA2429938C A turbine arrangement and a method of operating a turbine arrangement
06/29/2010CA2407480C Gas turbine power generation facility
06/24/2010WO2010070066A1 System including counter-rotating propellers driven by an epicyclic train ensuring a balanced couple distribution between the two propellers
06/24/2010WO2010046704A3 Method and system for altering engine air intake geometry
06/24/2010US20100158699 Rotor mounting system for gas turbine engine
06/24/2010US20100158669 Microcircuits for small engines
06/24/2010US20100156104 Thermal Reduction Gasification Process for Generating Hydrogen and Electricity
06/24/2010US20100155224 Multi-Component Deposition
06/24/2010US20100154436 Forward sleeve retainer plate and method
06/24/2010US20100154434 Gas Turbine
06/24/2010US20100154433 Turbine cooling air from a centrifugal compressor
06/24/2010US20100154427 Flow restrictor for lubrication line
06/24/2010US20100154426 Combustor liner with reverse flow for gas turbine engine
06/24/2010US20100154425 Strain tolerant thermal barrier coating system
06/24/2010US20100154424 Low cross-talk gas turbine fuel injector
06/24/2010US20100154423 system for mixing gas flows in a gas turbine engine, gas turbine engine and an aircraft engine
06/24/2010US20100154382 Method and systems for adaptive ignition energy
06/24/2010DE102008062363A1 Fangehäuse für ein Strahltriebwerk Fan casing for a jet engine
06/24/2010DE102008062088A1 Vorrichtung und Verfahren zur Energie-Rückgewinnung in Flugzeugtriebwerken beim Landeanflug. Apparatus and method for energy recovery in aircraft engines during the landing approach.
06/24/2010CA2746569A1 System including counter-rotating propellers driven by an epicyclic train ensuring a balanced couple distribution between the two propellers
06/24/2010CA2688607A1 Blade retention at a compressor rectifier stage for impact resistance
06/23/2010EP2199573A1 Generator coupling for use with gas turbine engine
06/23/2010EP2199572A2 Fuel system
06/23/2010EP2199571A2 System and method for removing a foreign object from an airstream entering a turbomachine
06/23/2010EP2199567A2 A system and method for heating a fuel using a solar heating system
06/23/2010EP2197743A2 Air intake structure to be mounted upstream of a nacelle middle structure for aircraft engine, and nacelle equipped with such air intake structure
06/23/2010CN101749286A Deep chilled air washer
06/23/2010CN101749120A Cooling system for a turbomachine
06/23/2010CN101749119A Turbine inlet air heat pump-type system
06/23/2010CN101749118A Static oil-gas separator
06/23/2010CN101749117A Base load control of gas turbine realized by chilling modulation
06/23/2010CN101749116A Low-grade heat recovery system for air inlet of turbine
06/23/2010CN101746938A Residential community excrement and kitchen waste collection and treatment and combined cold heat and power supply method
06/23/2010CA2688878A1 Automatic shut-off valve for the oil circuit in an airplane engine
06/23/2010CA2688201A1 Combined surface cooler and acoustic absorber for turbomachines
06/23/2010CA2688099A1 Centrifugal compressor forward thrust and turbine cooling apparatus
06/23/2010CA2687800A1 Turbine cooling air from a centrifugal compressor
06/22/2010US7739866 Turbofan case and method of making
06/22/2010US7739865 Gas turbine engine inlet with noise reduction features
06/22/2010US7739864 Systems and methods for power generation with carbon dioxide isolation
06/22/2010CA2688790A1 Combined pumping and separating machine for the oil circuit of a turbojet
06/22/2010CA2688674A1 Flow restrictor for lubrication line
06/22/2010CA2688374A1 Rotor mounting system for gas turbine engine
06/19/2010CA2687932A1 Multipoint probe assembly and method
06/17/2010WO2010067836A1 Hydrogen production system and power generation system
06/17/2010WO2010066791A1 Fan for a turbine engine including a balancing system with blind holes for housing bodies, and related turbine engine
06/17/2010US20100150735 Multi-Peripheral Serpentine Microcircuits For High Aspect Ratio Blades
06/17/2010US20100150700 Bypass air scoop for gas turbine engine
06/17/2010US20100146988 Gas turbine system
06/17/2010US20100146987 Gas turbine engine
06/17/2010US20100146986 Cavity ventilation
06/17/2010US20100146985 High Temperature-Resistant Sealing Assembly, Especially for Gas Turbines
06/17/2010US20100146981 Turbine Inlet Air Heat Pump-Type System
06/17/2010US20100146977 Deep Chilled Air Washer
06/17/2010US20100146976 Inlet Air Heating and Cooling System
06/17/2010US20100146930 Low Grade Heat Recovery System for Turbine Air Inlet
06/17/2010US20100146929 Method for Increasing the Efficiency of a Combined Gas/Steam Power Station With Integrated Gasification Combined Cycle
06/17/2010US20100146928 Fuel manifold for gas turbine engine
06/17/2010US20100146926 System for recovering water from flue gas
06/17/2010DE102009044765A1 Kühlsystem und -verfahren für eine Turbomaschine Cooling system and method for a turbo machine
06/17/2010DE102008062555A1 Loading device i.e. exhaust-gas turbocharger, for use in internal combustion engine of motor vehicle, has heating shield defining adjusting area together with bearing housing, where adjusting area accommodates adjusting ring
06/17/2010CA2746249A1 Fan for a turbine engine including a balancing system with blind holes for housing bodies, and related turbine engine
06/17/2010CA2733575A1 Hydrogen production system and power generation system
06/17/2010CA2687934A1 Fuel manifold for gas turbine engine
06/16/2010EP2196653A2 Deep chilled air washer
06/16/2010EP2196652A2 Gas turbine base load control by chilling modulation
06/16/2010EP2196651A2 Low grade heat recovery system for turbine air inlet
06/16/2010EP2196650A1 Turbine facility and power generating apparatus
06/16/2010EP2196634A2 Cavity ventilation
06/16/2010EP2196633A1 Power plant with a turbine unit and a generator
06/16/2010EP2196623A1 Gas Turbine
06/16/2010EP2196394A2 Method and apparatus for collecting and treating waste water from engine washing
06/16/2010CN1952372B Gas turbine engine assembly and methods of assembling the same
06/16/2010CN1948732B Bolting configuration for joining ceramic combustor liner to metal mouting attachments
06/16/2010CN1924321B Method and system for detecting gas turbine inlet filter rupture
06/16/2010CN1818362B Inboard radial dump venturi for combustion chamber of a gas turbine
06/16/2010CN1769655B Gas turbine power generating plant
06/16/2010CN101743391A Exhaust section structure of gas turbine and gas turbine
06/16/2010CN101737803A Fuel nozzle assembly for use with a gas turbine engine and method of assembling same
06/16/2010CN101737794A Method for controlling and optimizing performance heater
06/16/2010CN101737169A Fuel control system for gas turbine and feed forward control method
06/16/2010CN101737168A System and method for reducing corrosion in a gas turbine system
06/16/2010CN101737167A Methods, apparatus and systems concerning the circumferential clocking of turbine airfoils and the flow of cooling air
06/16/2010CN101737166A Air cooling apparatus for a purge valve
06/16/2010CN101737165A Method of controlling an air preheating system of a gas turbine
06/16/2010CN101737087A Rotor of turbine
06/16/2010CN101287898B Seal structure of gas turbine combustor
06/16/2010CN101194091B System for deicing the leading edge of a nose inlet cowl for a turbine engine
06/16/2010CN101128662B Aircraft engine fuel supply
06/16/2010CN101084366B Ventilating air intake arrangement with mobile closing device
06/16/2010CA2688727A1 Bypass air scoop for gas turbine engine
06/15/2010CA2429461C Bypass duct fan noise reduction assembly
06/12/2010CA2686729A1 Method for moving and aligning heavy device
06/11/2010CA2687015A1 Deep chilled air washer
06/11/2010CA2687003A1 Inlet air heating and cooling system
06/11/2010CA2687002A1 Low grade heat recovery system for turbine air inlet
06/11/2010CA2686728A1 Gas turbine base load control by chilling modulation
06/11/2010CA2686360A1 Turbine inlet air heat pump-type system
06/10/2010WO2010064921A1 Gas turbine with external combustion, applying a rotating regenerating heat exchanger
06/10/2010US20100143149 Turbine with at least one rotor which comprises rotor disks and a tie-bolt