| 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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| 07/26/2012 | DE102011003001A1 Turbinengehäuse Turbine housing |
| 07/26/2012 | CA2824369A1 Nacelle for an aircraft bypass turbojet engine |
| 07/26/2012 | CA2824367A1 Nacelle for an aircraft bypass turbojet engine |
| 07/25/2012 | EP2479408A2 Aircraft engine fuel system |
| 07/25/2012 | EP2479407A1 Mounting/dismounting jig for combustor tail pipe and tail pipe installation method |
| 07/25/2012 | EP2479406A2 Bearing System for Gas Turbine Engine |
| 07/25/2012 | EP2479405A2 Gas turbine equipment utilizing high humidity |
| 07/25/2012 | EP2478202A1 A noise attenuation panel and a gas turbine component comprising a noise attenuation panel |
| 07/25/2012 | EP2260184B1 Centrifugal oil separator having variable channel section |
| 07/25/2012 | CN202348445U Starting device for starting plurality of gas turbines |
| 07/25/2012 | CN202348444U Adjustable guide vane system for power turbine of gas turbine |
| 07/25/2012 | CN202348443U Adjustable protective cover at air inlet of jet engine |
| 07/25/2012 | CN102612592A Reinforced thermal energy storage pressure vessel for an adiabatic compressed air energy storage system |
| 07/25/2012 | CN102606623A Lube spacer bearing with pressure loading channel |
| 07/25/2012 | CN102606342A Metal/water/air reaction feedback type engine and high-speed sea flitting aircraft with diving function |
| 07/25/2012 | CN102606313A 冷却装置 Cooling device |
| 07/25/2012 | CN102606312A Cooling method used for segmented geometric adjustment of guide vanes of gas turbine |
| 07/25/2012 | CN102606311A Pneumatic jet engine |
| 07/25/2012 | CN102606310A CO2 near zero emission medium-low temperature solar heat energy and fossil energy complementary system and flow |
| 07/24/2012 | US8226356 Air intake for a turbocharger for an internal combustion engine |
| 07/24/2012 | US8226028 Device for mounting an aircraft turboprop engine comprising hydraulic attachments |
| 07/24/2012 | US8225615 Gas turbine engine with heat insulation device |
| 07/24/2012 | US8225614 Shim for sealing transition pieces |
| 07/24/2012 | US8225613 High altitude combustion system |
| 07/24/2012 | US8225593 Twin fan turbomachine |
| 07/24/2012 | CA2550890C Gas turbine engine with a single oil cavity |
| 07/24/2012 | CA2480584C Turbine engine with two sections connected by a joint |
| 07/19/2012 | WO2012096024A1 Fuel nozzle, gas turbine combustor equipped with same, and gas turbine equipped with this gas turbine combustor |
| 07/19/2012 | WO2012095592A1 Turbofan engine |
| 07/19/2012 | WO2012095590A1 Method for starting a turbomachine |
| 07/19/2012 | WO2012055784A3 Disc damper for charge air lines of an internal combustion engine having a turbocharger |
| 07/19/2012 | WO2012054310A3 System and method for liquid air production, power storage and power release |
| 07/19/2012 | US20120185144 Stoichiometric exhaust gas recirculation and related combustion control |
| 07/19/2012 | US20120180501 Bleed valve module |
| 07/19/2012 | US20120180499 Power generation system |
| 07/19/2012 | US20120180498 Anti-windmilling starter generator |
| 07/19/2012 | US20120180497 Fuel reformer system for a turbomachine system |
| 07/19/2012 | US20120180496 Gas turbine engine |
| 07/19/2012 | US20120180495 System and method for injecting fuel |
| 07/19/2012 | US20120180494 Turbine fuel nozzle assembly |
| 07/19/2012 | US20120180493 Apparatus and method for controlling oxygen emissions from a gas turbine |
| 07/19/2012 | US20120180491 Fuel injector |
| 07/19/2012 | US20120180489 Fuel injector |
| 07/19/2012 | US20120180488 Gas turbine combustor endcover assembly with integrated flow restrictor and manifold seal |
| 07/19/2012 | US20120180487 System for flow control in multi-tube fuel nozzle |
| 07/19/2012 | US20120180486 Gas turbine fuel system for low dynamics |
| 07/19/2012 | DE102012100371A1 Endabdeckungsanordnung einer Gasturbinenbrennkammer mit integrierter Durchflussbegrenzung und Verteilerabdichtung End cover assembly of a gas turbine combustion chamber with an integrated flow limitation and distributor seal |
| 07/19/2012 | DE102012100266A1 Gekrümmte Kühlkanäle für eine Turbinenkomponente Curved cooling channels for a turbine component |
| 07/19/2012 | DE102012100263A1 Brennstoffinjektor Fuel injector |
| 07/19/2012 | DE102012100262A1 Brennstoffdüsenanordnung für eine Turbine Fuel nozzle assembly for a turbine |
| 07/19/2012 | DE102011055152A1 Anordnung und Verfahren zur Verhinderung eines Fluidflusses Apparatus and method for preventing fluid flow |
| 07/19/2012 | DE102011008922A1 Verfahren zur Herstellung eines Schallabsorbers, insbesondere für einen Gasturbinenabgaskonus A process for producing a sound absorber, especially for a gas turbine exhaust cone |
| 07/19/2012 | DE102011008921A1 Gasturbinenabgaskonus Gas turbine exhaust cone |
| 07/19/2012 | DE102011008920A1 Schallabsorber, insbesondere für einen Gasturbinenabgaskonus und Verfahren zu dessen Herstellung A sound absorber, in particular for a gas turbine exhaust cone and process for its preparation |
| 07/19/2012 | DE102011008905A1 Bearing unit for shaft for turbo supercharger, comprises outer ring, inner ring and two bearing rows that are arranged between outer ring and inner ring which is radially fixed on shaft |
| 07/19/2012 | DE102011008812A1 Zwischengehäuse Intermediate housing |
| 07/19/2012 | DE102011008773A1 Wärmetauscher und Strahltriebwerk mit solchem Heat exchangers and jet engine with such |
| 07/19/2012 | DE102011008649A1 Turbinenreinigung Turbine cleaning |
| 07/19/2012 | DE102011002869A1 Reflektionsschalldämpfer Reflection silencer |
| 07/19/2012 | CA2823517A1 Method for starting a turbomachine |
| 07/19/2012 | CA2819384A1 Turbofan engine |
| 07/18/2012 | EP2476884A2 Water recovery system for a cooling tower |
| 07/18/2012 | EP2476880A1 Gas turbine engine and corresponding operating method |
| 07/18/2012 | EP2476866A1 Anti-windmilling starter generator |
| 07/18/2012 | EP2475861A2 Method for the operation of a micro gas turbine arrangement, and micro gas turbine arrangement for converting biomass into energy |
| 07/18/2012 | EP2475860A2 Heat shield for fuel feed conduits of a gas turbine engine |
| 07/18/2012 | EP2475858A1 Method for switching over a gas turbine burner operation from liquid to gas fuel and vice-versa |
| 07/18/2012 | CN102597583A Hydrodynamic circumferential seal system for large translations |
| 07/18/2012 | CN102597489A Turbine engine starter/generator, and method for the control thereof |
| 07/18/2012 | CN102597477A A noise attenuation panel and a gas turbine component comprising a noise attenuation panel |
| 07/18/2012 | CN102597462A Gas turbine |
| 07/18/2012 | CN102597459A 燃气轮机系统 Gas Turbine System |
| 07/18/2012 | CN102597429A Metal annular connecting structure for an aircraft turbine engine |
| 07/18/2012 | CN102594018A Anti-windmilling starter generator |
| 07/18/2012 | CN102589006A Combustor assemblies for use in turbine engines and methods of assembling same |
| 07/18/2012 | CN102588118A 燃气轮机系统和工艺 Gas Turbine Systems and processes |
| 07/18/2012 | CN102588117A Apparatus and method for controlling oxygen emissions from a gas turbine |
| 07/18/2012 | CN102588116A System for providing cooling and purging air flow to a rotary machine online monitoring system |
| 07/18/2012 | CN102588112A Jet-flow efficient thermal power system |
| 07/18/2012 | CN102588111A Backflow compression system for air compression |
| 07/18/2012 | CN102588080A Dynamic fluid gas working medium compression system |
| 07/18/2012 | CN102588015A Internal combustion engine with cylinder head and turbine |
| 07/18/2012 | CN101122260B Heat transfer system and method for turbine engine using heat pipes |
| 07/17/2012 | US8220275 Inlet bleed heat system thermal lag mitigation using compressor interstage bleeds |
| 07/17/2012 | US8220268 Turbine engine having fuel-cooled air intercooling |
| 07/17/2012 | US8220267 Process to detect two-phase flow in a conduit |
| 07/17/2012 | CA2713627C Composite casing for rotating blades |
| 07/12/2012 | WO2012094362A2 APPLYING OZONE NOx CONTROL TO AN HRSG FOR A FOSSIL FUEL TURBINE APPLICATION |
| 07/12/2012 | WO2012093299A1 Expansion turbine |
| 07/12/2012 | WO2012093235A1 Fuel circuit of an aeronautical turbine engine having a fuel pressure regulating valve |
| 07/12/2012 | US20120177490 Attachment of threaded holes to composite fan case |
| 07/12/2012 | US20120174595 Arrangement for maintaining flow to an air inlet of an auxiliary power unit assembly |
| 07/12/2012 | US20120174594 Turbomachine fuel delivery method and assembly |
| 07/12/2012 | US20120174591 Fuel Line System, Method for Operating of a Gas Turbine, and a Method for Purging the Fuel Line System of a Gas Turbine |
| 07/12/2012 | US20120174590 System and method for controlling combustor operating conditions based on flame detection |
| 07/12/2012 | US20120174589 Combustion Chamber End Cover Without Welding or Brazing |
| 07/12/2012 | US20120174587 fuel flowmeter having an improved regulator device |
| 07/12/2012 | DE102012100170A1 Verfahren, Systeme und Vorrichtungen zum Erkennen von Materialdefekten in Brennkammern von Verbrennungskraft-Turbinenmaschinen Methods, systems and devices for detecting material defects in combustion chambers of internal combustion-turbine engines |
| 07/12/2012 | DE102012100012A1 Prallplatte für Turbomaschinenkomponenten und mit dieser ausgestattete Komponenten Flapper turbomachinery components and equipped with these components |
| 07/12/2012 | DE102011122406A1 Verfahren zum Betrieb einer Gasturbine A method of operating a gas turbine |