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) |
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05/27/2010 | US20100126136 Electric power generating turbine engine fuel supply system |
05/27/2010 | DE102008058618A1 Baukastensystem für Abgasturbolader Modular system for turbocharger |
05/27/2010 | DE102008058614A1 Producing a ceramic heat insulation layer on a high-temperature loaded or hot gas-loaded component of a gas turbine or aircraft engine, comprises applying a slicker on an area of a component surface having metallic adhesive mediator layer |
05/27/2010 | DE102008057729A1 Exhaust gas turbo-charger for internal combustion engine in motor vehicle, has rotor supported in stator via pneumatic radial bearing and axial bearing, where radial bearing is pneumatically loaded by rotor, during operation of charger |
05/27/2010 | DE102008057207A1 Welleneinrichtung mit einer Dichtungsvorrichtung Shaft means with a sealing device |
05/26/2010 | EP2189637A2 A method of controlling an air preheating system of a gas turbine |
05/26/2010 | EP2188509A1 Wavy cmc wall hybrid ceramic apparatus |
05/26/2010 | EP1928744B1 Engine assembly for an aircraft comprising an engine as well as an engine mounting structure for such an engine |
05/26/2010 | CN201486660U Start device for turbojet engine adopting light diesel oil as fuel |
05/26/2010 | CN1836109B Control device for compressor |
05/26/2010 | CN1707080B Methods and apparatus for low emission gas turbine energy generation |
05/26/2010 | CN1705524B Method and apparatus for cleaning a turbofan gas turbine engine |
05/26/2010 | CN1704574B Fuel nozzle and method for cooling fuel nozzle |
05/26/2010 | CN1693691B Nozzle with build-in rib part and assemble of cooling insertion part |
05/26/2010 | CN1653262B Methods for starting a combustion turbine and combustion turbine generator configured to implement same methods |
05/26/2010 | CN1621671B Method and device for monitoring gas turbine combustion dynamics |
05/26/2010 | CN101713549A System and method for air-fuel mixing in gas turbines |
05/26/2010 | CN101713484A Inhibition to oxidation coking of aviation kerosene by acid cleaning and passivation |
05/26/2010 | CN101713363A Starter drive assembly and method of starting an engine |
05/26/2010 | CN101713339A Apparatus for steam attemperation using fuel gas heater water discharge to reduce feedwater pump size |
05/26/2010 | CN101713338A Method and system for providing cooling and power |
05/26/2010 | CN101713337A Method and apparatus for gas turbine engine temperature management |
05/26/2010 | CN101713336A Turbine nozzle for a gas turbine engine |
05/26/2010 | CN101713335A Sound attenuation system and method |
05/26/2010 | CN101024145B Method of processing volatile organic compound by using gas turbine and processing system thereof |
05/25/2010 | US7722729 Method for repairing high temperature articles |
05/25/2010 | US7721553 Method and apparatus for detecting a flashback condition in a gas turbine |
05/25/2010 | US7721552 Method for operation of a gas turbine group |
05/25/2010 | US7721523 Ground based pulse detonation combustor for power generation |
05/25/2010 | US7721522 Torque load transfer attachment hardware |
05/20/2010 | WO2010056376A1 Hybrid turbo transmission |
05/20/2010 | WO2010055723A1 Compressor drive device and operation method |
05/20/2010 | US20100124495 Turbine Engine Rotor Hub |
05/20/2010 | US20100124483 Apparatus and method for cooling a turbine airfoil arrangement in a gas turbine engine |
05/20/2010 | US20100122538 Methods, apparatus and systems concerning the circumferential clocking of turbine airfoils in relation to combustor cans and the flow of cooling air through the turbine hot gas flowpath |
05/20/2010 | US20100122537 Combustors with inserts between dual wall liners |
05/20/2010 | US20100122536 Plasma flow controlled diffuser system |
05/20/2010 | US20100122518 Oil system heating for aircraft gas turbines |
05/20/2010 | DE102009044513A1 Integrierte Brennkammeranordnung und Erststufen-Leitdüse für eine Gasturbine und Verfahren Integrated combustor assembly and first-stage guide nozzle for a gas turbine and procedures |
05/20/2010 | DE102008057878A1 Supercharger device, particularly exhaust gas turbocharger for combustion engine of motor vehicle, has turbine wheel and compressor carrying shaft, where turbine wheel is partially surrounded by turbine housing |
05/20/2010 | DE102008057532A1 Charging device, particularly exhaust gas turbo charger, has rotor which is supported by combined axial or radial bearing unit in bearing housing |
05/20/2010 | DE102008057504A1 Charging device i.e. exhaust gas turbocharger, has tensioning clamps provided for fastening housing sections and including spring arms for clamping flanges of housing sections against each other |
05/20/2010 | DE102008057428A1 Schutzstruktur und deren Verwendung Protective structure and the use thereof |
05/20/2010 | DE102008057162A1 Verfahren zur Reparatur des Bauteils einer Gasturbine Method to repair the component of a gas turbine |
05/20/2010 | DE102008057159A1 Gas turbine useful in aircraft engine, comprises two rotor discs, which are braced to each other and which directly adjoin to each other in a contact area, where one of the rotor discs is equipped in the contact area |
05/20/2010 | DE102008056851A1 Rotor einer Turbomaschine Rotor of a turbomachine |
05/19/2010 | EP2187129A1 Gas turbine |
05/19/2010 | EP2187128A1 Combustor |
05/19/2010 | EP2187023A1 Fuel control system for gas turbine and feed forward control method |
05/19/2010 | EP2187022A1 Cooling structure for gas-turbine combustor |
05/19/2010 | EP2187021A1 Gas turbine combustor |
05/19/2010 | EP2187020A1 Method for repairing turbine rotor blade |
05/19/2010 | EP2187019A1 Exhaust section structure of gas turbine and gas turbine |
05/19/2010 | EP2187003A2 Oil heating system for aircraft gas turbine engines |
05/19/2010 | EP2187001A1 Blade structure for turbine |
05/19/2010 | EP2186999A1 Gas turbine blade and gas turbine equipped with the same |
05/19/2010 | EP2186996A2 Rotor for a turbomachine |
05/19/2010 | EP2186729A1 Acoustic barrel for aircraft engine nacelle including crack and delamination stoppers |
05/19/2010 | EP2186592A1 Method of repair |
05/19/2010 | CN201474779U Residual oil recovery unit of jet nozzle of gas turbine |
05/19/2010 | CN1987067B Heat-electricity-cold combined supply system of melting carbonate fuel battery gas turbine bottom layer circulation |
05/19/2010 | CN101709673A Device and method used for cooling gas turbine |
05/19/2010 | CN101709672A High-efficiency high-temperature internal and external mixed gas turbine |
05/18/2010 | US7716933 Multi-channel fuel manifold |
05/18/2010 | US7716913 Engine |
05/18/2010 | CA2485179C Split flow turbine nozzle |
05/18/2010 | CA2462318C Method of applying environmental and bond coatings to turbine flowpath parts |
05/18/2010 | CA2454922C Process of removing a ceramic coating deposit in a surface hole of a component |
05/18/2010 | CA2451303C Methods for replacing combustor liners |
05/14/2010 | WO2010052434A2 System and method for washing and purging the liquid fuel system of a turbine with water |
05/13/2010 | US20100119718 Dense protective coatings, methods for their preparation and coated articles |
05/13/2010 | US20100119368 Double seal with pressurised lip |
05/13/2010 | US20100119357 Gas Turbine |
05/13/2010 | US20100115966 Gas turbine combustor |
05/13/2010 | US20100115960 Gas Turbine Installation with Flue Gas Recirculation |
05/13/2010 | US20100115959 Fuel metering pump calibration method |
05/13/2010 | US20100115957 Combustion Chamber for A Compact Lightweight Turbine |
05/13/2010 | US20100115956 Fuel injector |
05/13/2010 | US20100115954 Gas turbine fuel injector with a rich catalyst |
05/13/2010 | US20100115953 Integrated Combustor and Stage 1 Nozzle in a Gas Turbine and Method |
05/13/2010 | US20100115952 Gum substance monitoring apparatus, gum substance detecting method, and gas turbine system |
05/12/2010 | EP2184466A2 Aircraft engine relight method |
05/12/2010 | EP2184465A1 Intake air heating control device for gas turbine |
05/12/2010 | EP2184464A2 An inlet system for a gas turbine with EGR system |
05/12/2010 | EP2184448A2 An air bleeding assembly |
05/12/2010 | EP2184447A2 A noise reduction device |
05/12/2010 | DE4422701B4 Gasturbogruppe mit sequentieller Verbrennung Gas turbine group with sequential combustion |
05/12/2010 | DE202005021819U1 System zum Waschen eines Luftgasturbinentriebwerks System for washing a gas turbine engine air |
05/12/2010 | DE102009044407A1 Von Außen verstellbare Befestigung eines Aufprallkühlverteilers und Thermoelement-Gehäuse External adjustable attachment of a impingement cooling manifold and thermocouple housing |
05/12/2010 | DE102009044027A1 System und Verfahren zur Kühlung unter Verwendung eines Systemauslasses System and method for cooling using a Systemauslasses |
05/12/2010 | DE102008056741A1 Verschleissschutzschicht für Tial Wear protection for Tial |
05/12/2010 | DE102008056358A1 Twinscroll-Abgasturbolader Twin Scroll turbocharger |
05/12/2010 | CN201461095U Fuel switch valve in fuel pump governor control system |
05/12/2010 | CN1975131B 燃气轮机 Gas turbine |
05/12/2010 | CN1755080B Nose cone for a turbomachine |
05/12/2010 | CN1740538B Regulator feeding control with two flow rate laws |
05/12/2010 | CN101705871A Gas fuel regulating valve of combustion gas turbine |
05/12/2010 | CN101705870A Air-oil heat exchanger suitable for gas turbine engine |
05/12/2010 | CN101705844A Power generating system of coal-gas turbine without carbon emission and method thereof |
05/12/2010 | CN101184912B 燃气涡轮发动机冷却系统和方法 A gas turbine engine cooling systems and methods |