| 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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| 01/18/2012 | EP1454045B1 Method and apparatus for achieving power augmentation in gas turbines using wet compression |
| 01/18/2012 | CN102325996A Device for restricting throughflow quantity at pump, and pump arrangement having device of this type |
| 01/18/2012 | CN102325981A System for supporting and servicing a gas turbine engine |
| 01/18/2012 | CN102325980A Gas turbine engine and system for servicing a gas turbine engine |
| 01/18/2012 | CN102322354A System and method for pre-heating fuel in a power plant |
| 01/18/2012 | CN102322353A Method for increasing thermal efficiency of cycle of combustion turbine |
| 01/18/2012 | CN102322304A Turbo machine |
| 01/17/2012 | US8096135 Pure air blast fuel injector |
| 01/17/2012 | CA2459498C A method of making a multi-perforated part out of ceramic matrix composite material |
| 01/17/2012 | CA2441058C Sound attenuating aircraft reactor nacelle |
| 01/12/2012 | WO2012005324A1 Turbine blade and engine component |
| 01/12/2012 | WO2012004946A1 Fuel nozzle purge method, fuel nozzle purge device, and heat engine |
| 01/12/2012 | WO2012004515A2 Heat-exchange architecture built into the exhaust of a turbine engine |
| 01/12/2012 | WO2012004496A2 Ignition procedure for a turbine engine combustion chamber |
| 01/12/2012 | WO2012004254A1 Device for removing gas leaks in a device for supplying a gas turbine with gaseous fuel, and associated method |
| 01/12/2012 | WO2011121355A3 Gas turbines |
| 01/12/2012 | WO2011107733A3 Seamless acoustic liner |
| 01/12/2012 | US20120006037 Clamping assembly |
| 01/12/2012 | US20120006035 Turbine rim cutter for air turbine starter |
| 01/12/2012 | US20120006033 Combustor and Combustor Screech Mitigation Methods |
| 01/12/2012 | US20120006032 Systems, methods, and apparatus for confirming ignition in a gas turbine |
| 01/12/2012 | US20120006030 Injection nozzle for a turbomachine |
| 01/12/2012 | US20120006029 Air biasing system in a gas turbine combustor |
| 01/12/2012 | US20120006028 Damping resonator with impingement cooling |
| 01/12/2012 | DE102011051573A1 Kompressible Halterungen für Gasturbinen Compressible holders for gas turbines |
| 01/12/2012 | DE102011051572A1 Systeme, Verfahren und Vorrichtungen zur Bestätigung einer Zündung in einer Gasturbine Systems, methods and apparatus for confirmation of an ignition in a gas turbine |
| 01/12/2012 | DE102010031124A1 Strömungsmaschine Flow machine |
| 01/12/2012 | DE102010026834A1 Gasturbinenabgaskonus Gas turbine exhaust cone |
| 01/12/2012 | CA2804632A1 Turbine blade and engine component |
| 01/12/2012 | CA2802401A1 Heat-exchange architecture built into the exhaust of a turbine engine |
| 01/12/2012 | CA2802399A1 Ignition procedure for a turbine engine combustion chamber |
| 01/11/2012 | EP2405117A1 Approach to extending life of gas turbine engines |
| 01/11/2012 | EP2405116A2 Accessory Gearbox Assembly |
| 01/11/2012 | EP2405115A2 Split flow valve arrangement |
| 01/11/2012 | EP2405103A1 Split ring cooling structure and gas turbine |
| 01/11/2012 | EP2405102A1 Gas turbine with bellows seal |
| 01/11/2012 | EP2134604B1 Device for de-icing the air intake of a gas turbine |
| 01/11/2012 | EP1400300B1 Layered heat-resistant alloy plate and method of producing the same |
| 01/11/2012 | CN102317608A Air vehicle propulsion system with counter rotating fan design and method for noise reduction |
| 01/11/2012 | CN102317599A Aircraft engine with cooling for an electric starting device |
| 01/11/2012 | CN102317598A System of compact contra-rotating propellers |
| 01/11/2012 | CN102312727A Additive injection system for use with a turbine engine and methods of assembling same |
| 01/11/2012 | CN102312725A Critical low-entropy mixed-combustion cyclic thermomotive system |
| 01/11/2012 | CN102312683A Air film hole based on secondary flows of bent passage |
| 01/11/2012 | CN102310942A Non-rotating universal joint for a helicopter drive unit |
| 01/11/2012 | CN101360900B Fuel ratio control in a combustion apparatus with multiple fuel supply lines |
| 01/11/2012 | CN101205968B Gear with built-in overtorque protection |
| 01/11/2012 | CN101063422B Methods and system for reducing pressure losses in gas turbine engines |
| 01/10/2012 | US8091370 Combustor liner cap assembly |
| 01/10/2012 | US8091336 Method to initiate multiple chamber detonation wave combustors |
| 01/10/2012 | CA2500493C Turbine engine high-pressure turbine stator and assembly process |
| 01/10/2012 | CA2495594C Turbofan architecture having two front fans |
| 01/08/2012 | CA2745120A1 Flow machine |
| 01/07/2012 | CA2745014A1 Gear driven accessory for gearbox |
| 01/05/2012 | WO2012003080A1 Low emission power generation systems and methods |
| 01/05/2012 | WO2012003077A1 Low emission triple-cycle power generation systems and methods |
| 01/05/2012 | WO2012003076A1 Low emission triple-cycle power generation systems and methods |
| 01/05/2012 | WO2012002528A1 Shroud segment producing method and shroud segment |
| 01/05/2012 | WO2012001852A1 Gas turbine gap assessment device and gas turbine system |
| 01/05/2012 | WO2012001684A2 An apparatus, a container and methods thereof for heating foodstuff |
| 01/05/2012 | WO2012000980A1 Screwable bearing housing cover for a supercharging device |
| 01/05/2012 | US20120000205 Adaptive power and thermal management system |
| 01/05/2012 | US20120000204 Multi-spool intercooled recuperated gas turbine |
| 01/05/2012 | US20120000178 Systems involving fiber optic igniters |
| 01/05/2012 | DE102011105041A1 Schmiervorrichtung für einen Turbolader eines Motors für ein Fahrzeug A lubricating device for a turbocharger of an engine for a vehicle |
| 01/05/2012 | DE102011050967A1 Verfahren und Vorrichtung für Labyrinthdichtungspackungsringe Method and apparatus for labyrinth packing rings |
| 01/05/2012 | DE102011050962A1 Gas turbine engine system for turbine deceleration during shutdown procedure, has starting system in communication with rotor, and reversing operation of electrical generator to apply torque to rotor during shutdown procedures |
| 01/05/2012 | DE102010025614A1 Abgasturbolader Exhaust gas turbocharger |
| 01/05/2012 | CA2801499A1 Low emission power generation systems and methods |
| 01/05/2012 | CA2801488A1 Low emission triple-cycle power generation systems and methods |
| 01/05/2012 | CA2801476A1 Low emission triple-cycle power generation systems and methods |
| 01/04/2012 | EP2402642A1 Compensator for connecting tubes for waste gas containing dust |
| 01/04/2012 | EP2402622A1 Thrust bearing lubrication nozzle |
| 01/04/2012 | EP2402566A2 Liner aft end support mechanisms and spring loaded liner stop mechanisms |
| 01/04/2012 | EP2402560A1 Gear arrangement |
| 01/04/2012 | EP2401491A2 Improved air riding seal |
| 01/04/2012 | EP2102062B1 Aircraft leading edge |
| 01/04/2012 | EP1815149B1 Device for the withdrawal and recycling of cooling flows |
| 01/04/2012 | CN1525048B Gas turbine engine turbine nozzle bifurcated impingement baffle |
| 01/04/2012 | CN102308066A Method for flushing a section of a fuel system of a gas turbine |
| 01/04/2012 | CN102307784A Turbojet engine nacelle |
| 01/04/2012 | CN102307783A Acoustic processing panel, more particularly adapted for an air intake in an aircraft nacelle |
| 01/04/2012 | CN102305133A Particle separator and gas turbine |
| 01/03/2012 | US8087253 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 |
| 01/03/2012 | US8087252 Turbomachine combustion chamber |
| 01/03/2012 | US8087251 Gas turbine, method of controlling air supply and computer program product for controlling air supply |
| 01/03/2012 | CA2611732C Automated detection and control system and method for high pressure water wash application and collection applied to aero compressor washing |
| 01/03/2012 | CA2600080C Surface treatment method and repair method |
| 01/03/2012 | CA2531428C Electrical power generation system and method |
| 01/03/2012 | CA2487219C A method of inhibiting deposit formation in a jet fuel at high temperatures |
| 01/03/2012 | CA2472876C Turbojet nacelle hood locking mechanism |
| 01/03/2012 | CA2469943C Aircraft engine rear hanging device |
| 01/03/2012 | CA2461519C Lighter turbomachine blade and process for manufacturing the same |
| 01/03/2012 | CA2400149C A heat exchanger for cooling and for a pre-cooler for turbine intake air conditioning |
| 12/29/2011 | WO2011162330A1 Axial seal structure and rotation mechanism provided with same |
| 12/29/2011 | WO2011160440A1 Power fluid gas working medium compression system |
| 12/29/2011 | US20110318162 Gas turbine engine rotor tip clearance and shaft dynamics system and method |
| 12/29/2011 | US20110314831 Secondary water injection for diffusion combustion systems |
| 12/29/2011 | US20110314830 Oil supply system with main pump deaeration |
| 12/29/2011 | US20110314828 bleeding of air via the diffuser of a centrifugal compressor of a turbine engine |