| 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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| 04/05/2012 | DE102011053761A1 Vorrichtung und Verfahren zur Kühlung von Plattformbereichen von Turbinenlaufschaufeln Apparatus and method for cooling of platform areas of turbine blades |
| 04/05/2012 | DE102010060944B3 Wärmedämmende Auskleidung für eine Fluggasturbine Heat-insulating lining for an aircraft gas turbine |
| 04/05/2012 | DE102010037969A1 Internal combustion engine for vehicle, has oil circuit which is coupled to coolant jacket of turbine |
| 04/05/2012 | CA2813263A1 Aircraft engine systems and methods for operating same |
| 04/05/2012 | CA2812256A1 Dual fuel aircraft engine control system and method for operating same |
| 04/05/2012 | CA2812250A1 Dual fuel aircraft system and method for operating same |
| 04/05/2012 | CA2812233A1 Fuel storage system |
| 04/04/2012 | EP2436982A1 An igniter |
| 04/04/2012 | EP2435681A1 Stabilizing a gas turbine engine via incremental tuning |
| 04/04/2012 | EP2435680A2 Fluid-cooling device for a turbine engine propulsive unit |
| 04/04/2012 | EP2435679A2 Adsorption-enhanced compressed air energy storage |
| 04/04/2012 | EP2435678A1 Intake air temperature control device and a method for operating an intake air temperature control device |
| 04/04/2012 | EP1846641B1 Method for activating a pressure storage system, and a pressure storage system |
| 04/04/2012 | CN102401398A Fuel injection assembly for use in turbine engines and method of assembling same |
| 04/04/2012 | CN102401377A Apparatus and method for cooling combustor cap |
| 04/04/2012 | CN102400789A 一种可稳定火焰的点火器壳体 One kind of stable flame igniter housing |
| 04/04/2012 | CN102400788A Systems and methods for controlling the startup of a gas turbine |
| 04/04/2012 | CN102400787A 用于生产富氢燃料的系统和方法 System and method for producing a hydrogen-rich fuel |
| 04/04/2012 | CN102400786A Oil varnish mitigation systems |
| 04/04/2012 | CN101014760B Compressed-air generating system |
| 04/03/2012 | US8147188 Air cooled bucket for a turbine |
| 04/03/2012 | US8146369 Integrated direct drive starter/generator for turbines |
| 04/03/2012 | US8146367 Production of synthesis gas using catalyst-coated turbine blades |
| 04/03/2012 | US8146364 Non-rectangular resonator devices providing enhanced liner cooling for combustion chamber |
| 04/03/2012 | US8146342 Exhaust eductor system with a recirculation baffle |
| 04/03/2012 | CA2580594C Fuel manifold with reduced losses |
| 04/03/2012 | CA2520464C Turbojet with a one-piece servicing connector arm and one-piece servicing connector arm |
| 04/03/2012 | CA2495169C Side-fed shielded internal fuel manifold inlet tube |
| 03/29/2012 | WO2012040440A2 CdZnO OR SnZnO BUFFER LAYER FOR SOLAR CELL |
| 03/29/2012 | WO2012039386A1 Self-adjusting seal for turbo rotary machine |
| 03/29/2012 | WO2012038667A1 System for pressurising the bearing chambers of turbine engines machines using air taken from the intake duct |
| 03/29/2012 | WO2012038638A1 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 |
| 03/29/2012 | WO2012038402A2 Oil supply system for a stationary turbomachine |
| 03/29/2012 | WO2012038178A1 Quick-start device for a turbine, and method for operating a quick-start device |
| 03/29/2012 | US20120073306 Gas turbine combustion chamber made of cmc material and subdivided into sectors |
| 03/29/2012 | US20120073305 Combustion chamber and method for operating a combustion chamber |
| 03/29/2012 | US20120073302 Fuel nozzle assembly for gas turbine system |
| 03/29/2012 | US20120073301 Critical flow nozzle for controlling fuel distribution and burner stability |
| 03/29/2012 | US20120073300 Apparatus and method for a combustor |
| 03/29/2012 | US20120073299 High temperature manifolds for gas turbine engines |
| 03/29/2012 | DE102011053432A1 Brennstoffdüsenanordnung für Gasturbinensysteme Fuel nozzle assembly for gas turbine systems |
| 03/29/2012 | DE102011052675A1 Komponenten mit konform gekrümmten Filmlöchern und Verfahren für deren Herstellung Components compliant with curved film holes and methods for their preparation |
| 03/29/2012 | DE102011052672A1 Spitzenströmungspfadprofil Peak flow path profile |
| 03/29/2012 | DE102011051477A1 Verfahren und Vorrichtung zum Zusammenbau von Rotationsmaschinen Method and apparatus for the assembly of rotating machinery |
| 03/29/2012 | DE102010046598A1 Exhaust gas turbocharger has housing provided with air guiding section, exhaust gas guiding section and bearing section, where friction condition is adjusted in bearing |
| 03/29/2012 | DE102010046594A1 Bearing device for shaft of running things of exhaust gas turbocharger, has bearing that is provided with bearing sleeve, where bearing sleeve is configured in shaft |
| 03/29/2012 | DE102010028975A1 Verdichtergehäusezusatz Additional compressor housing |
| 03/29/2012 | DE102010025998A1 Profile heat exchanger, particularly for gas turbine, has a supply passage, discharge passage and multiple hollow sections, particularly elongated, oval or elliptical shaped cross sections |
| 03/29/2012 | CA2811940A1 System and method for high efficiency power generation using a nitrogen gas working fluid |
| 03/29/2012 | CA2811409A1 System for pressurising the bearing chambers of turbine engines machines using air taken from the intake duct |
| 03/29/2012 | CA2811269A1 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 |
| 03/28/2012 | EP2434132A2 Critical flow nozzle for controlling fuel distribution and burner stability |
| 03/28/2012 | EP2434130A2 Turbine starter valve |
| 03/28/2012 | EP2434129A2 Fuel manifolds for high temperature operation in gas turbine engines |
| 03/28/2012 | EP2434128A1 Oil supply system for a stationary turbo engine |
| 03/28/2012 | EP2434127A2 Methods and systems for modeling turbine operation |
| 03/28/2012 | EP2434125A1 Method for producing impeller applied to supercharger |
| 03/28/2012 | EP2434103A1 High speed turbine arrangement |
| 03/28/2012 | EP2432978A2 Aircraft engine starting/generating system and method of control |
| 03/28/2012 | EP2136050B1 Gas turbine plant |
| 03/28/2012 | CN102395773A Method for detecting an icing condition of or the need for servicing a fuel circuit of a turbine engine |
| 03/28/2012 | CN102395772A Double-body gas turbine engine provided with an inter-shaft bearing |
| 03/28/2012 | CN102392740A Oil feeding device and oil feeding method |
| 03/28/2012 | CN101680306B Blade structure for turbine |
| 03/28/2012 | CN101270768B Actuator position controller with a fail freeze servo-valve |
| 03/27/2012 | US8141370 Methods and apparatus for radially compliant component mounting |
| 03/27/2012 | US8141369 Method of regulation of the temperature of hot gas of a gas turbine |
| 03/27/2012 | US8141335 Intake air heating control device for gas turbine |
| 03/27/2012 | CA2472939C Device to passively control thermal expansion of the extension casing of a turbojet |
| 03/27/2012 | CA2399552C Iron base high temperature alloy |
| 03/22/2012 | WO2012004515A3 Heat-exchange architecture built into the exhaust of a turbine engine |
| 03/22/2012 | US20120067062 Turbine starter valve |
| 03/22/2012 | US20120067061 Bleed valve |
| 03/22/2012 | US20120067055 System and method for managing thermal issues in gas turbine engines |
| 03/22/2012 | US20120067051 Gas turbine engine and combustor |
| 03/22/2012 | DE102010045851A1 Turbo-machine e.g. turbine stage of gas turbine of aircraft engine, has housing control unit for displacement of housing portions against each other and/or bearing control unit for displacement of housing and rotor shaft against each other |
| 03/22/2012 | DE102010045712A1 Turbomaschinengehäuse Turbo machine housing |
| 03/22/2012 | DE102010041144A1 Schnellstartvorrichtung für eine Turbine, sowie Verfahren zum Betreiben einer Schnellstartvorrichtung Quick start-up device for a turbine and method for operating a quick start device |
| 03/22/2012 | DE102010041066A1 Trägergehäuse und Brennkraftmaschine Support housing and internal combustion engine |
| 03/21/2012 | CN102388224A Air bleed having an inertial filter in the tandem rotor of a compressor |
| 03/21/2012 | CN102383970A Turbofan engine |
| 03/21/2012 | CN102383943A Auxiliary hydraulic power generation system |
| 03/21/2012 | CN102383942A System and method for fast turbine deceleration |
| 03/21/2012 | CN102383941A Systems, methods, and apparatus for confirming ignition in a gas turbine |
| 03/21/2012 | CN102383940A Oil seal vehicle with out-of-operation starter for aircraft engine |
| 03/21/2012 | CN102383939A Multi-working-medium turbine engine |
| 03/21/2012 | CN102383938A Liner aft end support mechanisms and spring loaded liner stop mechanisms |
| 03/21/2012 | CN102383937A Turbojet engine |
| 03/21/2012 | CN101542092B Intake air heating control apparatus for gas turbine |
| 03/21/2012 | CN101449039B Gas turbine engine starting method and control device |
| 03/21/2012 | CN101178028B Compound tubine cooled engine |
| 03/20/2012 | US8136362 Turbomachine fan duct |
| 03/20/2012 | CA2750585C Caes plant using humidified air in the bottoming cycle expander |
| 03/20/2012 | CA2638961C Generator for gas turbine engine having main dc bus accessory ac bus |
| 03/20/2012 | CA2551539C Gas turbine engine combustor with improved cooling |
| 03/20/2012 | CA2514435C Flow control in accordance with two separate regulating laws for emergency regulator |
| 03/20/2012 | CA2506174C System and devices for collecting and treating waste water from engine washing |
| 03/20/2012 | CA2470069C Ignition plug waterproofing device, not soldered to the chamber wall |
| 03/15/2012 | WO2012033564A1 Screw shaft turbine compressor and system |
| 03/15/2012 | WO2012032557A1 Gas turbine power generation system |