| 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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| 05/08/2013 | EP2588732A1 Low emission triple-cycle power generation systems and methods |
| 05/08/2013 | EP2588731A1 Screwable bearing housing cover for a supercharging device |
| 05/08/2013 | EP2588730A1 Low emission power generation systems and methods |
| 05/08/2013 | EP2588729A1 Low emission triple-cycle power generation systems and methods |
| 05/08/2013 | DE102011117865A1 Sealing arrangement for exhaust gas turbine, has housing and shaft that are disassembled by moving housing and shaft in direction of the axis of rotation |
| 05/08/2013 | DE102011117862A1 Sealing arrangement, particularly for exhaust gas turbine, has shaft and housing which encloses shaft, where shaft is rotated over rotational axis relative to housing, and housing and shaft are limited together with sealing gap |
| 05/08/2013 | DE102011085801A1 Bauelement und Turbomaschine mit einem Bauelement Component and turbo engine with a component |
| 05/08/2013 | DE102010001414B4 Verfahren zur Reparatur von Labyrinth-Dichtungsstegen A method for repairing the labyrinth seal ridges |
| 05/08/2013 | CN202926472U Turbine machine shaft inner pipe balancing and centering device |
| 05/08/2013 | CN103097780A Shaft seal mechanism and rotary machine provided with same |
| 05/08/2013 | CN103097696A Method for optimizing the control of a free turbine power package for an aircraft, and control for implementing same |
| 05/08/2013 | CN103097694A Generating power using an ion transport membrane |
| 05/08/2013 | CN103091367A System for detecting contaminants in an intake flow of a compressor |
| 05/08/2013 | CN103089453A Apparatus for head end direct air injection with enhanced mixing capabilities |
| 05/08/2013 | CN103089451A Thermal-protection cover |
| 05/08/2013 | CN103089450A Gas turbine engine front center body architecture |
| 05/08/2013 | CN103089449A Gas turbine engine front center body architecture |
| 05/08/2013 | CN103089448A Inlet bleed heat system |
| 05/08/2013 | CN103089447A Bleed system for heating the compressor inlet air |
| 05/08/2013 | CN103089446A Gas turbine engine thermal management system |
| 05/08/2013 | CN103089445A Counter pressure preventing structure of air inlet channel of inspiration type impulse knocking engine |
| 05/08/2013 | CN103089444A Structure for reducing back pressure of air inlet channel of inspiration type impulse knocking engine |
| 05/08/2013 | CN103089443A Systems And Methods For Use In Monitoring Operation Of A Rotating Component |
| 05/08/2013 | CN103089437A Fuel gas turbine |
| 05/08/2013 | CN103089436A System for operating a power plant |
| 05/08/2013 | CN103089434A Combustible gas engine |
| 05/08/2013 | CN103089433A Stable-combustion water-cooled turbine engine |
| 05/08/2013 | CN103089345A Accommodating device used for rotary component |
| 05/08/2013 | CN101865034B Air inlet bending head reinforced shock absorption structure of internal combustion turbine |
| 05/08/2013 | CN101749120B Cooling system for a turbomachine |
| 05/07/2013 | US8434312 Gas turbine with improved part load emissions behavior |
| 05/07/2013 | US8434292 Ceramic-encased hot surface igniter system for jet engines |
| 05/07/2013 | CA2502796C High efficiency rotor for the first phase of a gas turbine |
| 05/04/2013 | CA2793505A1 Electrical harness |
| 05/04/2013 | CA2793501A1 Electrical harness connector |
| 05/04/2013 | CA2793497A1 Electrical harness |
| 05/04/2013 | CA2756914A1 Turbofan mounting arrangement |
| 05/02/2013 | WO2013062048A1 Member-assembling device for rotary machine |
| 05/02/2013 | WO2013062040A1 Shaft sealing device and rotating machine comprising same |
| 05/02/2013 | WO2013061945A1 Heat-resistant alloy member and method for producing same |
| 05/02/2013 | WO2013061928A1 Liquefied gas treatment system, control method therefor, liquefied gas carrier provided therewith, and liquefied gas storage facility provided therewith |
| 05/02/2013 | WO2013061662A1 Rotary internal combustion engine |
| 05/02/2013 | WO2013061303A1 Method for modifying a gas turbine burner assembly |
| 05/02/2013 | WO2013060987A2 Annular wall of a combustion chamber with improved cooling at the primary and/or dilution holes |
| 05/02/2013 | WO2013060966A1 Impregnation mandrel comprising a vacuum bag for the production of a gas turbine casing from composite material |
| 05/02/2013 | WO2013060523A1 Gas turbine engine support strut assembly |
| 05/02/2013 | WO2013060516A1 Gas turbine and method for guiding compressed fluid in a gas turbine |
| 05/02/2013 | US20130108420 Layered spline seal assembly for gas turbines |
| 05/02/2013 | US20130104567 Method and apparatus for cooling gas turbine rotor blades |
| 05/02/2013 | US20130104564 Active clearance control system and method for gas turbine |
| 05/02/2013 | US20130104560 Gas turbine engine with intercooling turbine section |
| 05/02/2013 | US20130104559 Gas turbine engine thermal management system |
| 05/02/2013 | US20130104555 Turbofan engine mixer assembly |
| 05/02/2013 | US20130104517 Component and method of fabricating the same |
| 05/02/2013 | DE112011101253T5 Turbineneinlassdüsenführungsschaufelbefestigungsstruktur für Gasturbinenradialtriebwerk Turbine inlet nozzle guide vane mounting structure for gas turbine radial engine |
| 05/02/2013 | CA2852393A1 Annular wall of a combustion chamber with improved cooling at the primary and/or dilution holes |
| 05/02/2013 | CA2852379A1 Impregnation mandrel comprising a vacuum bag for the production of a gas turbine casing from composite material |
| 05/01/2013 | EP2587151A2 System for Turbine Combustor Fuel Mixing |
| 05/01/2013 | EP2587102A1 Axial seal structure and rotation mechanism provided with same |
| 05/01/2013 | EP2587028A2 Active clearance control system and method for a gas turbine engine |
| 05/01/2013 | EP2587027A2 Gas turbine engine with intercooling turbine section |
| 05/01/2013 | EP2587026A2 Gas turbine engine with intercooling turbine section and intercooling turbine section bypass |
| 05/01/2013 | EP2587025A2 A system for heating a fuel |
| 05/01/2013 | EP2587024A2 Gas turbine engine thermal management system |
| 05/01/2013 | EP2587021A1 Gas turbine and method for guiding compressed fluid in a gas turbine |
| 05/01/2013 | EP2587020A2 Journal pin for gear system |
| 05/01/2013 | EP2587003A1 Gas turbine engine support strut assembly |
| 05/01/2013 | CN202914145U New shafting of gas-steam combined cycle 'one-on-one' unit |
| 05/01/2013 | CN103080503A Combined cycle power generation plant utilzing solar heat |
| 05/01/2013 | CN103080502A Solar gas turbine system |
| 05/01/2013 | CN103075747A Fuel injection assembly for use in turbine engines and method of assembling same |
| 05/01/2013 | CN103075256A Turbomachine configured to burn ash-bearing fuel oils and method thereof |
| 05/01/2013 | CN103075255A Start control system for aircraft engine |
| 05/01/2013 | CN103075254A System for heating a fuel |
| 05/01/2013 | CN103075253A Gas turbine engine system and method of providing a fuel supplied to combustors |
| 05/01/2013 | CN103075252A Shaft support |
| 05/01/2013 | CN103075203A Layered spline seal assembly for gas turbines |
| 05/01/2013 | CN101235728B Impingement cooled bucket shroud, turbine rotor incorporating the same, and cooling method |
| 05/01/2013 | CN101134508B Fan exhaust nozzle for turbofan engine |
| 04/30/2013 | US8429919 Expansion hula seals |
| 04/30/2013 | US8429917 Fuel control method of a can annular combustor array |
| 04/30/2013 | CA2793232A1 Component and method of fabricating the same |
| 04/30/2013 | CA2699124C Hp turbine vane airfoil profile |
| 04/30/2013 | CA2427384C Ni-base sintered alloy |
| 04/27/2013 | CA2789465A1 Gas turbine engine front center body architecture |
| 04/27/2013 | CA2789325A1 Gas turbine engine front center body architecture |
| 04/25/2013 | WO2013058209A1 Lean fuel intake gas turbine |
| 04/25/2013 | US20130098471 Aircraft nacelle comprising a hot air supply device for a panel combining acoustic and frost treatments |
| 04/25/2013 | US20130098454 Isentropic compression inlet for supersonic aircraft |
| 04/25/2013 | US20130098066 Turbine engine comprising a contrarotating propeller receiver supported by a structural casing attached to the intermediate housing |
| 04/25/2013 | US20130098065 Structural cooling fluid tube for supporting a turbine component and supplying cooling fluid to transition section |
| 04/25/2013 | US20130098064 Structural cooling fluid tube for supporting a turbine component and supplying cooling fluid |
| 04/25/2013 | US20130098063 Coolng structure for recovery-type air-cooled gas turbine combustor |
| 04/25/2013 | US20130098062 Compressor bleed cooling fluid feed system |
| 04/25/2013 | US20130098059 Windmill operation of a gas turbine engine |
| 04/25/2013 | US20130098058 Split accessory drive system |
| 04/25/2013 | US20130098057 Controllable speed windmill operation of a gas turbine engine through low spool power extraction |
| 04/25/2013 | US20130098050 Gas turbine engine with intercooling turbine section |
| 04/25/2013 | US20130098044 Flashback resistant tubes in tube lli design |
| 04/25/2013 | US20130098043 Hydrajetting Nozzle and Method |