| 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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| 05/30/2012 | CN202250403U Sealed mounting structure |
| 05/30/2012 | CN202250402U Nitrogen replacing and blowing system of combustion gas turbine |
| 05/30/2012 | CN202250401U Combined circular main engine oil system |
| 05/30/2012 | CN202250400U Gas turbine lubricant system |
| 05/30/2012 | CN202250399U Particle separation device and combustion gas turbine |
| 05/30/2012 | CN202250398U 集油箱 Collection tank |
| 05/30/2012 | CN102482997A 用于从液体燃料到气体燃料和相反过程的转换燃气轮机燃烧器操作的方法 The method of gas fuel from the liquid fuel to the gas turbine combustor and converting the reverse process for the operation |
| 05/30/2012 | CN102477904A Combustion dynamics monitoring ignition system for a gas turbine |
| 05/30/2012 | CN101657566B Discharge surface treatment method and repairing method |
| 05/30/2012 | CN101473107B Platform cooling structure of gas turbine rotor blade |
| 05/30/2012 | CA2759719A1 Engine case with wash system |
| 05/30/2012 | CA2758670A1 Inlet particle separator system |
| 05/29/2012 | US8186938 Turbine apparatus |
| 05/29/2012 | US8186169 Nitrogen cooled gas turbine with combustor nitrogen injection and partial nitrogen recycling |
| 05/29/2012 | US8186167 Combustor transition piece aft end cooling and related method |
| 05/29/2012 | US8186164 Turbine engine fuel injector |
| 05/29/2012 | US8186162 Acoustically tuned combustion for a gas turbine engine |
| 05/29/2012 | US8186144 Component ventilation and pressurization in a turbomachine |
| 05/29/2012 | US8186142 Systems and method for controlling stack temperature |
| 05/29/2012 | CA2759191A1 Combination low spool generator and ram air turbine generator |
| 05/29/2012 | CA2681866C Coating material and method of manufacturing same, coating method, and moving blade with shroud |
| 05/24/2012 | WO2012067540A1 Gas-turbine electric power station |
| 05/24/2012 | WO2012038402A3 Oil supply system for a stationary turbomachine |
| 05/24/2012 | WO2012027154A3 Integral plus proportional dual pump switching system |
| 05/24/2012 | US20120125011 Method for use with annular gas turbine engine component |
| 05/24/2012 | US20120125009 Aircraft safety device systems |
| 05/24/2012 | US20120125008 Low calorific value fuel combustion systems for gas turbine engines |
| 05/24/2012 | US20120125007 Method and system for engine ignition and monitoring |
| 05/24/2012 | US20120124961 Filter Cartridge Assembly For Use With Turbine Engine Systems |
| 05/24/2012 | DE202012004682U1 Abgasturbolader Exhaust gas turbocharger |
| 05/24/2012 | DE10322703B4 Gasturbinenregelungssystem Gas turbine control system |
| 05/24/2012 | DE102011118158A1 Gasturbinenmotor und Schaufel für einen Gasturbinenmotor Gas turbine engine and blade for a gas turbine engine |
| 05/24/2012 | DE102011080995A1 Turbine mit variabler Geometrie und deren Montage A variable geometry turbine and their assembly |
| 05/24/2012 | DE102010052150A1 Rotationsenergiebereitsstellungsvorrichtung, Notstromaggregat und Luftfahrzeug Already rotational energy delivery device, Generator and aircraft |
| 05/24/2012 | DE102010044098A1 Turbocharger i.e. exhaust gas turbocharger, for internal combustion engine of motor car, has bearing disk made of steel and comprising lubricant channel leading toward contact socket that is made of copper alloy |
| 05/24/2012 | CA2759320A1 Remote shaft driven open rotor propulsion system with electrical power generation |
| 05/24/2012 | CA2758435A1 Method for monitoring the oil system of a turbomachine |
| 05/24/2012 | CA2758123A1 Dc motor assembly with soft starting capability |
| 05/24/2012 | CA2757683A1 Advanced air and oil circuit architecture for turbomachine |
| 05/23/2012 | EP2455597A2 Axial accessory gearbox |
| 05/23/2012 | EP2455596A2 Safety instrumented system (SIS) for a turbine system |
| 05/23/2012 | EP2454461A2 Gas turbine exhaust gas cooling system |
| 05/23/2012 | EP2454460A2 Method for removal of entrained gas in a combined cycle power generation system |
| 05/23/2012 | EP2454452A1 Spiral wound brush seal |
| 05/23/2012 | CN202228189U Generating set cooling device of gas turbine |
| 05/23/2012 | CN202228188U Gas turbine engine lubricant system |
| 05/23/2012 | CN202223998U Gas filter device |
| 05/23/2012 | CN102472493A 燃气轮机燃烧器及燃气轮机 A gas turbine combustor and a gas turbine |
| 05/23/2012 | CN102472169A Split ring cooling structure and gas turbine |
| 05/23/2012 | CN102472168A 燃气轮机外壳结构 Turbine housing structure |
| 05/23/2012 | CN102472114A Multi-stage radial turbine |
| 05/23/2012 | CN102472110A Turbo engine having steam tapping |
| 05/23/2012 | CN102471833A Ni-based monocrystalline superalloy and turbine blade |
| 05/23/2012 | CN102465764A System and method for combustion dynamics control |
| 05/23/2012 | CN102465763A Integrated turbomachine oxygen plant |
| 05/23/2012 | CN102465762A 等离子处理式过滤器 The plasma processing filter |
| 05/23/2012 | CN102465761A 旁通涡轮机进气口 Turbine bypass air inlet |
| 05/23/2012 | CN101417592B Improvement for rotorcraft equipped with turboshaft engines |
| 05/23/2012 | CN101415607B Air inlet lip for a pod with electric defrosting |
| 05/22/2012 | US8181965 Replaceable brush seal elements |
| 05/22/2012 | US8181624 Open-cycle internal combustion engine |
| 05/22/2012 | US8181467 Mid-turbine frame torque box having a concave surface |
| 05/22/2012 | US8181466 Mid-turbine frame |
| 05/22/2012 | US8181465 Positioning arrangement for components of a pressure vessel and method |
| 05/22/2012 | US8181441 Controlled fan stream flow bypass |
| 05/22/2012 | US8181440 Arrangement of a semiconductor-type igniter plug in a gas turbine engine combustion chamber |
| 05/22/2012 | CA2757712A1 Method and system for engine ignition and monitoring |
| 05/22/2012 | CA2638186C Scalloped flexure ring |
| 05/22/2012 | CA2505618C Device for lubricating a component in an assembly of parts |
| 05/22/2012 | CA2500483C Device for axial support of spacer area for panel of a high-pressure turbine of a gas turbine engine |
| 05/18/2012 | WO2012065155A1 Blade off protection systems and methods |
| 05/18/2012 | WO2012064452A1 End-fed liquid fuel gallery for a gas turbine fuel injector |
| 05/17/2012 | US20120119020 Aircraft, propulsion system, and system for taxiing an aircraft |
| 05/17/2012 | US20120117976 Apparatus and method for igniting a combustor |
| 05/16/2012 | EP2453144A1 Bearing device, bearing unit, and rotary machine |
| 05/16/2012 | EP2452876A2 Aircraft propulsion system and system for taxiing an aircraft |
| 05/16/2012 | EP2451556A1 A gas filtering device and a method of manufaturing a gas filtering device |
| 05/16/2012 | DE102011055381A1 Plasmabehandeltes Filter Plasma-treated filter |
| 05/16/2012 | DE102011055241A1 Einrichtung und Verfahren zum Zünden einer Brennkammeranordnung Apparatus and method for igniting a combustion chamber arrangement |
| 05/16/2012 | DE102011055150A1 Turbinenschaufelanordnung Turbine blade assembly |
| 05/16/2012 | CN102459849A Stabilizing a gas turbine engine via incremental tuning |
| 05/16/2012 | CN102459848A 吸附增强压缩空气蓄能 Enhanced adsorption compressed air energy storage |
| 05/16/2012 | CN102459821A Device and method for detecting a fault in a low-pressure fuel pump of a turbojet and turbojet including one such device |
| 05/16/2012 | CN102459820A Turbomachine |
| 05/16/2012 | CN102454485A Systems and methods for supplying fuel to a gas turbine |
| 05/16/2012 | CN102454482A Integrated gasification combined cycle system with a nitrogen cooled gas turbine |
| 05/16/2012 | CN102454480A Axial compressor and associated operating method |
| 05/16/2012 | CN102454437A Communication system for turbine engine |
| 05/16/2012 | CN102454431A Variable turbine nozzle system |
| 05/16/2012 | CA2758549A1 Aircraft, propulsion system, and system for taxiing an aircraft |
| 05/16/2012 | CA2758545A1 Aircraft and propulsion system |
| 05/16/2012 | CA2758466A1 Aircraft, propulsion system, and system for taxiing an aircraft |
| 05/15/2012 | US8176724 Hybrid Brayton cycle with solid fuel firing |
| 05/15/2012 | CA2485435C Device for assembly of a shroud placed between an aircraft engine air intake and a pylon |
| 05/15/2012 | CA2456705C Annular platform for distributor of low-pressure turbine of jet engine |
| 05/10/2012 | WO2012060378A1 Ammonia injection device |
| 05/10/2012 | WO2012045029A8 Dual fuel aircraft engine control system and method for operating same |
| 05/10/2012 | WO2012030934A3 Electrical arrangement of hybrid ignition device |
| 05/10/2012 | US20120111026 Castable high temperature aluminum alloy |
| 05/10/2012 | US20120111024 Gas turbine engine and high speed rolling element bearing |