| 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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| 08/01/2013 | US20130192238 Buffer system that communicates buffer supply air to one or more portions of a gas turbine engine |
| 08/01/2013 | US20130192237 Fuel injector system with fluidic oscillator |
| 08/01/2013 | US20130192235 Internal manifold for turning mid-turbine frame flow distribution |
| 08/01/2013 | US20130192199 Gas turbine engine shaft bearing configuration |
| 08/01/2013 | US20130192197 Anti-icing core inlet stator assembly for a gas turbine engine |
| 08/01/2013 | DE112011103621T5 Gasturbinenbrenner mit Befestigung für Helmholtz-Resonatoren Gas turbine burner mounting for Helmholtz resonators |
| 08/01/2013 | DE102012001603A1 Supercharger for internal combustion engine of motor vehicle, has guide device whose guide vanes are supported at lid- and carrier elements, where carrier element is held at turbine housing and sealed by seal element against turbine housing |
| 08/01/2013 | DE102012001571A1 Triebwerksgehäuse einer Fluggasturbine mit Schalldämpfungselementen im Fan-Einströmbereich Engine casing of an aircraft gas turbine with sound damping elements in the fan inflow |
| 08/01/2013 | DE102010025286B4 Leichtmetallgussteil für einen Verbrennungsmotor Alloy casting for an internal combustion engine |
| 08/01/2013 | CA2803306A1 Hybrid apu start fuel system |
| 07/31/2013 | EP2620628A2 Gas turbine engine nacelle with sound damping means in the fan intake area |
| 07/31/2013 | EP2620622A2 Bevel gear arrangement for axial accessory gearbox |
| 07/31/2013 | EP2620621A2 Gas turbine engine system and method for controlling a temperature of a conduit in a gas turbine engine system |
| 07/31/2013 | EP2620620A2 Fluid flow control device and method |
| 07/31/2013 | EP2620619A2 Method of using external fluid for cooling high temperature components of a gas turbine for a process power plant |
| 07/31/2013 | EP2620618A2 Gas turbine engine in-board cooled cooling air system |
| 07/31/2013 | EP2620617A2 Combustion turbine inlet anti-icing resistive heating system |
| 07/31/2013 | EP2620616A2 Bleed air systems for use with aircrafts and related methods |
| 07/31/2013 | EP2620598A2 Sealing arrangement, method and fluid flow engine |
| 07/31/2013 | EP2619428A2 System and method for high efficiency power generation using a nitrogen gas working fluid |
| 07/31/2013 | EP2619419A1 System for pressurising the bearing chambers of turbine engines machines using air taken from the intake duct |
| 07/31/2013 | EP2619417A1 Sealing device having a sleeve for the passage of a connecting rod of a system for controlling the orientation of the blower blades of a turboprop engine through a partition |
| 07/31/2013 | CN203098055U Heat-insulating cover |
| 07/31/2013 | CN203098054U Thermal-insulating board structure |
| 07/31/2013 | CN103228993A Gas turbine assembly and method therefor |
| 07/31/2013 | CN103228872A Method for controlling the generation of electricity applied to an aircraft gas turbine, and device implementing such a method |
| 07/31/2013 | CN103225548A Bevel gear arrangement for axial accessory gearbox |
| 07/31/2013 | CN103225547A Method For Transferring Fuel |
| 07/31/2013 | CN103225546A Gas turbine engine system and method for controlling a temperature of a conduit in a gas turbine engine system |
| 07/31/2013 | CN103225545A Fuel delivery system for gas turbine and related methods |
| 07/31/2013 | CN103225544A Turbomachine passage cleaning system |
| 07/31/2013 | CN103225543A Combustion turbine inlet anti-icing resistive heating system |
| 07/31/2013 | CN103225542A Deformable bulging gas inlet channel bulging molded surface deformation achievement method |
| 07/31/2013 | CN102278207B Solution dehumidification based inlet gas cooling method for gas turbine |
| 07/31/2013 | CN101793196B System and method for automatic fuel bending and control for combustion gas turbine |
| 07/31/2013 | CN101410300B Air inlet shroud structure |
| 07/30/2013 | US8495880 Thermal management using topological isomerization of fuel |
| 07/30/2013 | US8495857 Gas turbine engine thermal management system |
| 07/30/2013 | DE202013006386U1 Abgasturbolader Exhaust gas turbocharger |
| 07/30/2013 | CA2570243C System for washing an aero gas turbine engine |
| 07/25/2013 | WO2013108328A1 Repair method and repair structure for honeycomb sandwich structural body |
| 07/25/2013 | US20130189085 Turbomachine seal arrangement |
| 07/25/2013 | US20130189081 Filter assembly including pleat tip shapes |
| 07/25/2013 | US20130189071 Oil purge system for a mid turbine frame |
| 07/25/2013 | US20130186707 Unknown |
| 07/25/2013 | US20130186105 Anisotropic vibration isolation mounting assembly |
| 07/25/2013 | US20130186104 Arrangement of components of a wind power plant |
| 07/25/2013 | US20130186103 Near flow path seal for a turbomachine |
| 07/25/2013 | US20130186101 Method of using external fluid for cooling high temperature components of gas turbine for a process power plant |
| 07/25/2013 | US20130186098 Fluid flow control device and method |
| 07/25/2013 | US20130186096 Method for monitoring a fuel circuit shut-off valve |
| 07/25/2013 | US20130186095 Gas turbine with motive fluid driven jet-compressor |
| 07/25/2013 | US20130186093 Process of fabricating a fuel nozzle assembly, process of fabricating a fuel nozzle ring, and a fuel nozzle ring |
| 07/25/2013 | US20130186057 Naphtha and process gas/syngas mixture firing method for gas turbine engines |
| 07/25/2013 | US20130186056 Gas turbine engine comprising means for axially retaining a fan of the engine |
| 07/25/2013 | DE102012200768A1 Method for manufacturing closure element to close inspection aperture of gas turbine, involves producing inner body and/or bearing shell in layers by generative process, and producing layer of inner body together with layer of bearing shell |
| 07/25/2013 | DE102012002154B3 Device for protecting aircraft engine against bird strike, consists of lattice bars, which are so tightly arranged that invasion of birds in aircraft engine is barred, where lattice bars are permeable to air through material recesses |
| 07/24/2013 | EP2617979A2 Fastening element and de-icing device of a aviation gas turbine engine |
| 07/24/2013 | EP2617966A2 Gas turbine engine accessory gearbox |
| 07/24/2013 | EP2617965A2 Gas turbine engine with pylon mounted accessory drive |
| 07/24/2013 | EP2617964A2 Combustor blowout recovery method and system |
| 07/24/2013 | EP2617963A2 Liquid fuel heating system |
| 07/24/2013 | EP2617962A2 Filter assembly including pleat tip shapes |
| 07/24/2013 | CN203081582U Starting control system of engine |
| 07/24/2013 | CN203081581U Internal combustion wave rotor with pressurization function based on nonsteady combustion |
| 07/24/2013 | CN103221660A System and method for high efficiency power generation using a nitrogen gas working fluid |
| 07/24/2013 | CN103221644A Power plant line having a variable-peed pump |
| 07/24/2013 | CN103217028A Fan-shaped radiator |
| 07/24/2013 | CN103216337A 液体燃料加热系统 Liquid fuel heating system |
| 07/24/2013 | CN103216336A Chemical heat regenerator |
| 07/24/2013 | CN103216335A Process of fabricating a fuel nozzel assembly, process of fabricating a fuel nozzle ring, and a fuel nozzle ring |
| 07/24/2013 | CN103216333A Countercurrent tangential type micro turbojet engine |
| 07/24/2013 | CN103216275A Near flow path seal for a turbomachine |
| 07/24/2013 | CN102425497B Gas intake cone fixation structure of gas turbine engine |
| 07/24/2013 | CN101802367B Intake silencer for gas turbine |
| 07/24/2013 | CN101761394B Negative overload resistant double-chamber oil supply device and method thereof |
| 07/24/2013 | CN101082307B Device for optimizing cooling in gas turbines |
| 07/24/2013 | CA2802542A1 Oil purge system for a mid turbine frame |
| 07/23/2013 | US8490916 Suspension system for aircraft auxiliary power unit with elastomeric member |
| 07/23/2013 | US8490411 Axial accessory gearbox |
| 07/23/2013 | US8490410 Axial accessory gearbox |
| 07/23/2013 | US8490409 Bleed air transfer tube |
| 07/23/2013 | US8490406 Method and apparatus for controlling a heating value of a low energy fuel |
| 07/23/2013 | US8490405 Gas turbine engine mixing duct and method to start the engine |
| 07/23/2013 | US8490398 Premixed burner for a gas turbine combustor |
| 07/23/2013 | US8490381 Systems involving fiber optic igniters transmitting fuel and laser light |
| 07/23/2013 | CA2802246A1 Filter assembly including pleat tip shapes |
| 07/23/2013 | CA2683942C Improved start flow measurement |
| 07/23/2013 | CA2538223C Multi-spool turbogenerator system and control method |
| 07/23/2013 | CA2498459C Gas turbine inlet flow straightener |
| 07/18/2013 | WO2013105606A1 Shaft seal device and rotary machine with same |
| 07/18/2013 | WO2013105299A1 Seal structure for rotary machine, and gas turbine with same |
| 07/18/2013 | WO2013077924A3 Gas turbine engine system and supersonic exhaust nozzle |
| 07/18/2013 | US20130183143 Sealing device having a sleeve for the passage of a connecting rod of a system for controlling the orientation of the blower blades of a turboprop engine through a partition |
| 07/18/2013 | US20130181413 Spring loaded seal assembly for turbines |
| 07/18/2013 | US20130180262 Gas turbine engine accessory gearbox |
| 07/18/2013 | US20130180261 Combustor and method for reducing thermal stresses in a combustor |
| 07/18/2013 | US20130180260 Combustor recovery method and system |
| 07/18/2013 | US20130180256 Turbine fuel nozzle assembly and method for operating a turbine |
| 07/18/2013 | US20130180255 Rational late lean injection |