Patents
Sitemap › F02 - Combustion engines; Hot-gas or combustion-product engine plants › F02C - Gas-turbine plants; Air intakes for jet-propulsion plants; Controlling fuel supply in air-breathing jet-propulsion plants › F02C 7 - Features, component parts, details or accessories, not provided for in, or of interest apart from, groups; Air intakes for jet-propulsion plants
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)
10/2010
10/20/2010CN101868602A Damping device and gas turbine combustor
10/20/2010CN101865793A Air filtration sampling point adaptor
10/20/2010CN101865037A Alignment device for gas turbine casing
10/20/2010CN101865036A System and method for augmenting power output of turbine during transient event
10/20/2010CN101865035A Filter washing system for gas turbine engines
10/20/2010CN101865034A Air inlet bending head reinforced shock absorption structure of internal combustion turbine
10/20/2010CN101865033A Method for expanding compressor discharge bleed air
10/19/2010US7815743 Method and apparatus for cleaning a turbofan gas turbine engine
10/19/2010US7815415 Mounting structure for air separator, and gas turbine
10/19/2010US7814753 Low profile attachment hanger system for a cooling liner within a gas turbine engine swivel exhaust duct
10/19/2010CA2476747C Methods and apparatus for cooling turbine engine combustor exit temperatures
10/19/2010CA2472605C Turbofan variable fan nozzle
10/19/2010CA2418879C Methods and apparatus for varying gas turbine engine inlet air flow
10/19/2010CA2389525C Variable cycle propulsion device employing exhaust bypass for supersonic aircraft, and operating process
10/17/2010CA2699124A1 Hp turbine vane airfoil profile
10/16/2010CA2698865A1 Dual orifice pilot fuel injector
10/14/2010WO2010116071A1 Air bleed having an inertial filter in the tandem rotor of a compressor
10/14/2010WO2010075393A3 Gas turbine engine and system for servicing a gas turbine engine
10/14/2010US20100260598 Thermal control system for turbines
10/14/2010US20100258260 Producing metallic articles by reduction of nonmetallic precursor compounds and melting
10/14/2010US20100257869 Diffuser arranged between the compressor and the combustion chamber of a gas turbine
10/14/2010US20100257867 Monitoring of a high-pressure pump in a turbine engine fuel supply circuit
10/14/2010US20100257838 Model based health monitoring of aeroderivatives, robust to sensor failure and profiling
10/14/2010US20100257837 Systems involving hybrid power plants
10/14/2010DE202010010427U1 Vorrichtung zur Verringerung von Schäden durch Vogelschlag an Triebwerken Apparatus for reducing damage caused by bird strikes on engines
10/14/2010DE102009016802A1 Einlaufkonus aus Faserverbundmaterial für ein Gasturbinentriebwerk Inlet cone made of fiber composite material for a gas turbine engine
10/14/2010DE102009016688A1 Hülsenelement zur axialen Festlegung sowie Abgasturbolader Sleeve member for axial retention and exhaust gas turbocharger
10/14/2010DE102009015863A1 Gas sealing device for turbo machine shaft, has floating ring seal for sealing turbo machine shaft against turbo machine housing, where ring seal is lubricated and blocked with operating gas
10/14/2010CA2758078A1 Air bleed having an inertial filter in the tandem rotor of a compressor
10/13/2010EP2239440A1 Gas turbine engine with stacked accessory components
10/13/2010EP2239439A2 Method and system for adjusting the position of a turbomachine valve
10/13/2010EP2239438A2 Systems and Methods for Controlling Compressor Extraction Cooling
10/13/2010EP2239437A2 Systems and methods for providing compressor extraction cooling
10/13/2010EP2238325A2 Gas turbine systems and methods employing a vaporizable liquid delivery device
10/13/2010EP2238315A1 Sealing segment and sealing-segment arrangement
10/13/2010CN1952369B Gas turbine engine assembly and methods of assembling same
10/13/2010CN1550714B Differential pressure induced purging fuel injector with asymmetric cyclone
10/13/2010CN101861451A Monitoring of a high-pressure pump in a turbomachine fuel supply circuit
10/13/2010CN101858257A Gas turbine inner flowpath coverpiece
10/13/2010CN101858256A Combined convection/effusion cooled one-piece can combustor
10/13/2010CN101858255A Systems and methods for providing compressor extraction cooling
10/13/2010CN101858254A Filter retention systems and devices
10/12/2010US7810337 Method to re-engage start of dynamoelectric machine
10/12/2010US7810336 System for introducing fuel to a fluid flow upstream of a combustion area
10/12/2010US7810309 Fuel system utilizing dual mixing pump
10/12/2010CA2510218C Hingeless flapper valve for flow control
10/12/2010CA2389780C Emergency device for restarting a turbojet in autorotation
10/12/2010CA2371335C Procedure for de-icing a jet engine air inlet cowl and device for applying the said procedure
10/12/2010CA2359266C Gas injector system and its fabrication
10/12/2010CA2303316C Nozzles for water injection in a turbine engine
10/09/2010CA2695048A1 Sensor head for a dry powder agent
10/07/2010WO2010112542A1 Filter cassette, filter arrangement, and gas turbine with such filter cassette
10/07/2010WO2010112453A1 Rotating inlet cowl for a turbine engine, including an eccentric front end
10/07/2010WO2010111909A1 Turboshaft engine
10/07/2010US20100254801 Cooled aerofoil for a gas turbine engine
10/07/2010US20100251725 Combustor and Method for Modifying the Same
10/07/2010US20100251723 Thimble, sleeve, and method for cooling a combustor assembly
10/07/2010US20100251722 Wall elements for gas turbine engine combustors
10/07/2010US20100251720 Fuel injector nozzles for gas turbine engines
10/07/2010US20100251719 Centerbody for mixer assembly of a gas turbine engine combustor
10/07/2010US20100251718 Damping device and gas turbine combustor
10/07/2010US20100251687 Gas turbine: seal between adjacent can annular combustors
10/07/2010CA2756845A1 Rotating inlet cowl for a turbine engine, including an eccentric front end
10/07/2010CA2756512A1 Filter cassette, filter arrangement, and gas turbine with such filter cassette
10/06/2010EP2236924A2 Staging valve arrangement and valve for use therein
10/06/2010EP2236923A1 Dissolved gas removal system
10/06/2010EP2236793A1 Burner assembly
10/06/2010EP2236775A2 Turbomachine inlet heating system
10/06/2010EP2236766A2 Reducing inter-seal gap in gas turbine
10/06/2010EP2236747A2 Systems, methods, and apparatus for passive purge flow control in a turbine
10/06/2010EP2236640A2 Multi-component coating deposition
10/06/2010EP2236585A1 Method of operating a thermal device and use of such a method to inhibit vanadium corrosion
10/06/2010EP2234886A1 Nacelle for turbojet engine
10/06/2010CN201599097U 发动机增压器垫片 Engine turbocharger gaskets
10/06/2010CN201599096U 高效高温型内外混燃气轮机 Efficient mix of high-temperature gas turbine inside and outside
10/06/2010CN1891999B System for fixing an injection system to the dome of turbine combustion chamber and method of fixation
10/06/2010CN101855135A Air intake structure to be mounted upstream of a nacelle middle structure for aircraft engine, and nacelle equipped with such air intake structure
10/06/2010CN101852136A Device for reducing inter-seal gap in gas turbine
10/06/2010CN101852135A Systems and methods for controlling compressor extraction cooling
10/06/2010CN101852132A Thermally decoupled can-annular transition piece
10/06/2010CN101852104A Exhaust plenum for a turbine engine
10/05/2010US7805949 Device for supporting and housing auxiliaries in a bypass turbojet
10/05/2010US7805948 Internally mounted device for a pressure vessel
10/05/2010US7805947 Aircraft with disengageable engine and auxiliary power unit components
10/05/2010US7805943 Shroud for a turbomachine combustion chamber
10/05/2010CA2486024C Method and apparatus for arresting a crack within a body
10/05/2010CA2430143C Cooling of upstream flange of high pressure turbine by chamber end twin injectors
10/02/2010CA2697741A1 Combined acoustic absorber and heat exchanging outlet guide vanes
09/2010
09/30/2010WO2010111357A2 High-flow-capacity centrifugal hydrogen gas compression systems, methods and components therefor
09/30/2010WO2010110936A2 Variable actuation pressure system for independent pressure control
09/30/2010WO2010110833A2 Recuperator for gas turbine engines
09/30/2010WO2010110327A1 Cmc turbine stator vane
09/30/2010WO2010110325A1 Cmc turbine stator vane
09/30/2010WO2010109954A1 Turbine blade and gas turbine
09/30/2010WO2010109152A2 Aircraft nacelle comprising a reinforced outer wall
09/30/2010US20100247300 Reducing inter-seal gap in gas turbine
09/30/2010US20100247290 Turbine blade and gas turbine
09/30/2010US20100247285 Systems and Methods for Providing Compressor Extraction Cooling
09/30/2010US20100247005 Sealing Segment and Sealing-Segment Arrangement
09/30/2010US20100242496 Gas turbine engine with stacked accessory components
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