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)
07/2013
07/18/2013US20130180250 Fuel supply apparatus, fuel-flow-rate-control apparatus, and gas-turbine power plant
07/18/2013US20130180249 System for injecting a fluid, compressor and turbomachine
07/18/2013US20130180227 Fastening element and de-icing device of an aircraft gas-turbine engine
07/18/2013DE102012200539A1 Shielding device for turbine housing of thermal gas turbine, has restriction element for limiting flow channel in sections between high pressure side and low pressure side of turbine housing, where bar is arranged in flow channel
07/18/2013DE102012000890A1 Befestigungselement und Enteisungsvorrichtung eines Fluggasturbinentriebwerks Fastener and de-icer an aircraft gas turbine engine
07/18/2013DE102009059330B4 Verfahren und Vorrichtung zur Kühlung eines Übergangsstücks Method and apparatus for cooling a transition piece
07/17/2013EP2615277A2 Turbomachine drive arrangement
07/17/2013EP2615276A2 Air recovery system for precooler heat-exchanger
07/17/2013EP2615275A1 Coolant Supply System
07/17/2013EP2615260A2 Gas turbine engine bearing chamber seals
07/17/2013EP2615259A2 Gas turbine engine bearing chamber seals
07/17/2013EP2615258A2 Startup method for large steam turbines
07/17/2013EP2614242A1 Propulsion system for a flying machine, particularly for a missile
07/17/2013EP2614241A1 Liquid fuel assist ignition system of a gas turbine and method to provide a fuel/air mixture to a gas turbine
07/17/2013EP2614239A1 Screw shaft turbine compressor and system
07/17/2013CN203067096U Multi-disk solar indirect-cooling back-heating re-heating type air turbine thermal power generation device
07/17/2013CN103210257A Nozzle, gas turbine combustor and gas turbine
07/17/2013CN103206726A Turbine Fuel Nozzle Assembly And Method For Operating A Turbine
07/17/2013CN102080600B System and method for generating power by applying chemical purge gas
07/17/2013CN101959758B Aircraft engine assembly comprising an annular force-transfer structure surrounding the central casing of a turbojet engine
07/17/2013CN101952573B Air intake structure for an aircraft nacelle
07/17/2013CN101675228B Gas turbine combustor
07/17/2013CA2802060A1 Gas turbine engine with pylon mounted accessory drive
07/16/2013US8484981 Integrated fuel gas characterization system
07/16/2013US8484976 System, method and apparatus for fluidic effectors for enhanced fluid flow mixing
07/16/2013US8484975 Apparatus and method for start-up of a power plant
07/16/2013US8484942 Planetary gear system arrangement with auxiliary oil system
07/11/2013WO2013103572A1 Waterproof and salt repellant media and filter
07/11/2013WO2013103469A2 Process of producing ceramic matrix composites and ceramic matrix composites formed thereby
07/11/2013WO2012080798A3 Forced flow steam generator having wall heating surface and method for its operation
07/11/2013US20130177406 Gas turbine engine bearing chamber seals
07/11/2013US20130174576 Turbomachine component alignment
07/11/2013US20130174575 Gas turbine engine starter-generator with integrated lube oil scavenge functionality
07/11/2013US20130174574 Gas turbine engine bearing chamber seals
07/11/2013US20130174570 Engine systems with enhanced start control schedules
07/11/2013US20130174569 System and method for supplying a working fluid to a combustor
07/11/2013US20130174568 Combustor and method for distributing fuel in the combustor
07/11/2013US20130174564 System and method for operating a gas turbine
07/11/2013US20130174563 Combustor fuel nozzle and method for supplying fuel to a combustor
07/11/2013US20130174562 Gas turbine engine, combustor and dome panel
07/11/2013US20130174558 System for injecting fuel in a gas turbine engine
07/11/2013US20130174557 Combustor for a gas turbine engine
07/11/2013US20130174553 Diffuser having fluidic actuation
07/11/2013DE102005003853B4 Verfahren zum Betreiben eines Flugtriebwerks A method of operating an aircraft engine
07/10/2013EP2613041A2 Turbine to operate at part-load
07/10/2013EP2613040A2 Engine systems with enhanced start control schedules
07/10/2013EP2613039A2 Fuel distribution manifold
07/10/2013EP2613038A2 Systems and methods for monitoring fluid seperation and/or monitoring the health of a valve
07/10/2013EP2613037A2 A method and apparatus for operating a gas turbine engine
07/10/2013EP2613036A2 Gas turbine inlet system
07/10/2013EP2613018A2 Method for meeting a purge flow requirement for a power plant and a power plant having a purge control system
07/10/2013EP2613016A2 System and method for operating a gas turbine
07/10/2013EP2612815A2 Speed card-controlled override fuel pump assist field
07/10/2013EP2612749A1 Method for manufacturing a composite fan inlet housing
07/10/2013EP2612020A2 Electrical arrangement of hybrid ignition device
07/10/2013DE202010018001U1 Leichtmetallgussteil für einen Verbrennungsmotor Alloy casting for an internal combustion engine
07/10/2013CN203050895U Igniter and ignition starting device of turbojet engine
07/10/2013CN203050894U Starting control system of aircraft engine
07/10/2013CN203050893U Diesel oil supply device of aeroengine
07/10/2013CN203050892U Engine radiating shaft tube and turbojet engine
07/10/2013CN103199387A Electrical grounding plane
07/10/2013CN103195612A Multifunctional turbofan jet engine
07/10/2013CN103195586A Systems and methods for monitoring fluid seperation and/or monitoring the health of a valve
07/10/2013CN103195584A Turbine to operate at part-load
07/10/2013CN103195579A Custody transfer system and method for gas fuel
07/10/2013CN103195578A System and method for operating a gas turbine
07/10/2013CN103195577A Air intake temperature regulating system of gas turbine
07/10/2013CN103195576A Infrared inhibiting device for smoke extraction of gas turbines of ships
07/10/2013CN103195575A 燃气涡轮入口系统 Gas turbine inlet systems
07/10/2013CN103195574A Late lean injection system transition piece
07/10/2013CN103195573A Exhaust strut and turbine machinery including same
07/10/2013CN103195572A 涡轮扩散器 Turbine diffuser
07/10/2013CN103195571A Power plant
07/10/2013CN103195570A Method and apparatus for operating a gas turbine engine
07/10/2013CN103195515A System for axial retention of rotating segments of a turbine
07/10/2013CN103195497A Nozzle used for gas turbine and seal carrier
07/10/2013CN102472169B Split ring cooling structure and gas turbine
07/10/2013CN101688477B System for cooling and adjusting the temperature of apparatuses in the propulsion assembly of an aircraft
07/10/2013CA2799107A1 Gas turbine engine bearing chamber seals
07/10/2013CA2798841A1 Gas turbine engine bearing chamber seals
07/09/2013US8479754 System for washing an aero gas turbine engine
07/09/2013US8479524 Combustion chamber arrangement for operating a gas turbine
07/09/2013US8479522 Method of starting a turbomachine by testing operational support systems during the purging process
07/09/2013US8479491 Clamping system and method for thrust reverser attachment
07/09/2013US8479490 Combustors with impingement cooled igniters and igniter tubes for improved cooling of igniters
07/09/2013US8479489 Turbine exhaust recirculation
07/09/2013US8479486 Oil system heating for aircraft gas turbines
07/09/2013CA2513783C Turbo engine inlet bullet fairing
07/09/2013CA2489629C Methods and apparatus for machining components
07/08/2013DE202013001098U1 Staustrahltriebwerk mit veränderbarer Einlaufgeometrie Ramjet engine with variable intake geometry
07/05/2013CA2801083A1 Turbine engine shaft
07/04/2013WO2013102098A1 Vavle for gas turbine engine
07/04/2013WO2013101873A1 Hot gas expander inlet casing assembly and method
07/04/2013WO2013101506A1 Method and apparatus for swaged liquid injector spoke
07/04/2013WO2013101488A1 Gas turbine with coulombic thermal protection
07/04/2013US20130167554 Temperature sensing device and method of assembling the same
07/04/2013US20130167553 Hyperstatic truss comprising connecting rods
07/04/2013US20130167552 Exhaust strut and turbomachine incorprating same
07/04/2013US20130167550 Method for meeting a purge flow requirement for a power plant and a power plant having a purge control system
07/04/2013US20130167548 Method and apparatus for operating a gas turbine engine
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