| 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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| 12/14/2011 | CN102278147A 用于涡轮的弹性加载密封组件 Resilient seal assembly for a turbine load |
| 12/13/2011 | US8074452 Nested channel ducts for nozzle construction and the like |
| 12/13/2011 | CA2507168C Engine nacelle for a supersonic aircraft |
| 12/13/2011 | CA2454262C Gas turbine |
| 12/08/2011 | WO2011152944A2 Self-regulating fuel staging port for turbine combustor |
| 12/08/2011 | WO2011152906A2 Optical monitoring system for a turbine engine |
| 12/08/2011 | WO2011152049A1 Gas turbine system |
| 12/08/2011 | WO2011151567A1 Spark plug preheat |
| 12/08/2011 | US20110299984 Improved Air Riding Seal |
| 12/08/2011 | US20110299974 Lubricating and cooling epicyclic stepdown gearing |
| 12/08/2011 | US20110296848 Fluid transfer arrangement |
| 12/08/2011 | US20110296847 Mounting assembly |
| 12/08/2011 | US20110296846 Aeronautical engine with cooling of an electric starting device |
| 12/08/2011 | US20110296845 Combined heat and power with a peak temperature heat load |
| 12/08/2011 | US20110296844 Gas turbine combustion system with rich premixed fuel reforming and methods of use thereof |
| 12/08/2011 | US20110296843 Positive displacement power extraction compensation device |
| 12/08/2011 | US20110296840 Gas turbine combustor injection assembly, and combustor fuel mixture feed method |
| 12/08/2011 | US20110296839 Self-Regulating Fuel Staging Port for Turbine Combustor |
| 12/08/2011 | US20110296811 Heat transfer arrangement for fluid-washed surfaces |
| 12/08/2011 | US20110296810 Life management system and method for gas turbine thermal barrier coatings |
| 12/08/2011 | CA2801051A1 Spark plug preheat |
| 12/07/2011 | EP2392798A1 Aircraft with a preheating device for a fluid/fluid heat exchanger thereof |
| 12/07/2011 | EP2392797A2 Gas turbine combustion system with rich premixed fuel reforming and methods of use thereof |
| 12/07/2011 | EP2392796A1 Device for the emission reduction of a turboshaft engine and corresponding method |
| 12/07/2011 | EP2392055A1 Ignition laser |
| 12/07/2011 | EP2391803A1 Assembly including an agb and an oil tank |
| 12/07/2011 | EP1645659B1 Method for repairing machine part, method for forming restored machine part, method for manufacturing machine part, gas turbine engine, electric discharge machine, method for repairing turbine component, and method for forming restored turbine component |
| 12/07/2011 | CN102272428A 发动机 Engine |
| 12/07/2011 | CN102272427A 发动机 Engine |
| 12/07/2011 | CN102269059A 附件箱传动装置及具有其的航空发动机 Accessory gear box and has its aircraft engine |
| 12/06/2011 | US8070432 Static gas turbine component and method for repairing such a component |
| 12/06/2011 | US8069673 Seal structure for gas turbine combustor |
| 12/06/2011 | US8069671 Burner fuel lance configuration and method of use |
| 12/06/2011 | CA2467810C Method of manufacturing a hollow blade for a turbine engine |
| 12/01/2011 | WO2011148935A1 Vibration damping blade for fluid |
| 12/01/2011 | WO2011148899A1 Seal structure, turbine machine equipped with same, and power plant equipped with said turbine machine |
| 12/01/2011 | WO2011148078A2 Gearbox in a turbomachine |
| 12/01/2011 | WO2011082939A3 Turbo compressor and compressor system comprising said turbo compressor |
| 12/01/2011 | US20110293414 Locking device designed to be arranged in a junction region of a nacelle |
| 12/01/2011 | US20110293403 Blade monitoring system |
| 12/01/2011 | US20110290163 Hybrid oxy-fuel boiler system |
| 12/01/2011 | US20110289934 Gas Turbine Startup Control |
| 12/01/2011 | US20110289933 Hybrid Prefilming Airblast, Prevaporizing, Lean-Premixing Dual-Fuel Nozzle for a Gas Turbine Combustor |
| 12/01/2011 | US20110289932 System for fuel and diluent control |
| 12/01/2011 | US20110289930 System and Method for Exhaust Gas Use in Gas Turbine Engines |
| 12/01/2011 | US20110289929 Turbomachine fuel nozzle |
| 12/01/2011 | US20110289928 Air/fuel supply system for use in a gas turbine engine |
| 12/01/2011 | US20110289927 Method for Flushing a Section of a Fuel System of a Gas Turbine |
| 12/01/2011 | US20110289926 Extruded fluid manifold for gas turbomachine combustor casing |
| 12/01/2011 | US20110289925 Fuel pumping system for a gas turbine engine |
| 12/01/2011 | DE102010048305A1 Turbocharger for commercial vehicle, has shaft connecting turbine wheel and compressor wheel of rotor, and bearings arranged at axial ends of rotor, where bearings are formed as toe bearings |
| 12/01/2011 | DE102010021929A1 Ansaugtrakt für eine Verbrennungskraftmaschine Intake system for an internal combustion engine |
| 12/01/2011 | CA2799661A1 Gearbox in a turbomachine |
| 11/30/2011 | EP2390486A2 Accessory gearbox with internal layshaft |
| 11/30/2011 | EP2390485A2 Gas turbine startup control |
| 11/30/2011 | EP2390484A2 Fuel pumping system for a gas turbine engine |
| 11/30/2011 | EP2250357B1 Air intake structure for an aircraft nacelle |
| 11/30/2011 | EP2222560B1 Aircraft nacelle guidance system installation |
| 11/30/2011 | EP1635955B1 Water distribution and vaporization assembly |
| 11/30/2011 | CN202052356U 油气分离装置及具有该油气分离装置的燃气轮机润滑系统 Oil and gas separation equipment and gas turbine lubrication system which has a gas separation unit |
| 11/30/2011 | CN102261281A 包括人字形薄膜冷却孔的物品与相关工艺 Chevron film cooling holes including the items associated with the process |
| 11/30/2011 | CN102258922A 过滤器介质褶皱套件保持 Filter media pleat kit maintain |
| 11/30/2011 | CN101798960B 催化燃烧体系 Catalytic combustion system |
| 11/30/2011 | CN101592071B 用于废气涡轮增压器的轴向轴承密封装置 Axial bearing seals for exhaust turbocharger |
| 11/29/2011 | CA2643489C Gas turbine engine oil system operation |
| 11/29/2011 | CA2586548C Testing rig and method for a fuel nozzle assembly |
| 11/29/2011 | CA2533394C Dual action inlet door and method for use thereof |
| 11/29/2011 | CA2516700C Compact compound engine package |
| 11/25/2011 | CA2736449A1 Fuel pumping system for a gas turbine engine |
| 11/24/2011 | WO2011145326A1 Turbine of gas turbine engine |
| 11/24/2011 | WO2011144842A2 Multi-layer acoustic treatment panel |
| 11/24/2011 | WO2011144567A2 Method and device for supplying cooling air to an engine, in particular an aircraft engine, gas turbine, or the like |
| 11/24/2011 | WO2011123392A3 Unitized engine nacelle structure |
| 11/24/2011 | US20110288731 Systems and methods for controlling an integrated drive train |
| 11/24/2011 | US20110284328 Assembly including an agb and an oil tank |
| 11/24/2011 | US20110284095 Turbojet engine nacelle |
| 11/24/2011 | US20110283713 System For Cooling A Heat Exchanger On Board An Aircraft |
| 11/24/2011 | US20110283711 Gas turbine component and a gas turbine engine comprising the component |
| 11/24/2011 | US20110283710 Synthesis gas-based fuel system including admixture of a second fuel, and method for the operation of a synthesis gas-based fuel system |
| 11/24/2011 | US20110283706 System and methods for pre-heating fuel in a power plant |
| 11/24/2011 | DE102010029048A1 Turbo machine for use in form of turbocharger, has bearing housing, shaft, impeller and sealing, where shaft is rotatably supported in inner chamber of bearing housing |
| 11/24/2011 | DE102010022218A1 Abgasturbolader Exhaust gas turbocharger |
| 11/24/2011 | DE102010020800A1 Verfahren und Vorrichtung zur Kühlluftversorgung für ein Triebwerk, insbesondere Flugtriebwerk, Gasturbine oder dergleichen Method and apparatus for cooling air supply for an engine, in particular aircraft engine, gas turbine or the like |
| 11/24/2011 | DE102004024294B4 Gasturbinenanlage Gas turbine plant |
| 11/24/2011 | CA2799543A1 Multi-layer acoustic treatment panel |
| 11/23/2011 | EP2388456A2 System and method for pre-heating fuel in a power plant |
| 11/23/2011 | EP2388438A1 Turbine element-forming core assembly and method of manufacturing a turbine blade |
| 11/23/2011 | EP2387737A1 Method and measurement device for determining a condition of an electric igniter of a gas turbine burner and an ignition device for a gas turbine burner |
| 11/23/2011 | CN102257260A System including counter-rotating propellers driven by an epicyclic train ensuring a balanced couple distribution between the two propellers |
| 11/23/2011 | CN102251858A Late lean injection injector |
| 11/23/2011 | CN102251857A System for cooling turbine combustor transition piece |
| 11/23/2011 | CN102251818A Gas and steam turbine system |
| 11/23/2011 | CN102251814A Gas turbine engine turbine nozzle bifurcated impingement baffle |
| 11/23/2011 | CN102251246A System for protecting turbine engine surfaces from corrosion |
| 11/23/2011 | CN102247735A Device for gas inlet of filtering gas turbine |
| 11/23/2011 | CN101784841B Gas turbine combustor |
| 11/23/2011 | CN101008351B Method and apparatus for enabling engine turn down |
| 11/22/2011 | US8063501 Gas turbine bleed energy recovery via counter rotating generator |
| 11/22/2011 | US8061146 Heat transfer augmentation in a compact heat exchanger pedestal array |
| 11/22/2011 | US8061141 Combustor assembly including one or more resonator assemblies and process for forming same |