| 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) |
|---|
| 04/25/2012 | EP2192289B1 Intake silencer for gas turbine |
| 04/25/2012 | EP1634634B1 Suction filter, turbo compressor, and method of packaging the compressor |
| 04/25/2012 | CN202202991U Closed engine liquefying carbon dioxide through nitrogen |
| 04/25/2012 | CN202202947U High-efficiency gas cooler |
| 04/25/2012 | CN102428332A Method and apparatus for cooling a gaseous hydrocarbon stream |
| 04/25/2012 | CN102428258A Method for producing impeller applied to supercharger |
| 04/25/2012 | CN102425497A 燃气涡轮发动机进气锥固定结构 The gas turbine engine inlet cone fixed structure |
| 04/25/2012 | CN102425486A Highly-efficient gas cooler |
| 04/25/2012 | CN102425460A 用于燃气涡轮机级的喷嘴的简化的支撑装置 For a simplified gas turbine stage nozzle support means |
| 04/25/2012 | CN102425459A 一种重型燃机高温涡轮双工质冷却叶片 A heavy duty gas turbine high temperature turbine blade cooling duplex quality |
| 04/25/2012 | CN101910730B 燃气轮机的燃烧器 A gas turbine combustor |
| 04/24/2012 | US8161725 Compact cyclone combustion torch igniter |
| 04/24/2012 | CA2673001C Jet flow discharge nozzle and jet engine |
| 04/24/2012 | CA2466759C Fuel nozzle sheath retention ring |
| 04/24/2012 | CA2456589C Ventilation device for a high pressure turbine rotor of a turbomachine |
| 04/24/2012 | CA2444984C Reading device for identification connectors |
| 04/19/2012 | WO2012051315A2 Generating power using an ion transport membrane |
| 04/19/2012 | WO2012049500A1 A material, devices and structures including a material, and a method of forming a material |
| 04/19/2012 | WO2012049422A2 Connecting module between a drive shaft of an engine fan and a rolling element bearing |
| 04/19/2012 | WO2012025690A3 Method for mounting shielding on a turbine casing, and mounting assembly for implementing same |
| 04/19/2012 | WO2012025687A3 Method for optimizing the overall energy efficiency of an aircraft, and main power package for implementing same |
| 04/19/2012 | US20120090695 Aircraft nacelle including at least one radial partition between two conducts |
| 04/19/2012 | US20120090331 Systems and methods for supplying fuel to a gas turbine |
| 04/19/2012 | US20120090327 Power plant and method for its operation |
| 04/19/2012 | US20120090291 Internal combustion engine |
| 04/19/2012 | DE102011115364A1 Kraftwerk Power station |
| 04/19/2012 | DE102011054586A1 Dichtungsanordnung für eine Turbomaschine A seal assembly for a turbomachine |
| 04/19/2012 | DE102011054548A1 Systeme und Verfahren zur Zuführung von Brennstoff zu einer Gasturbine Systems and methods for supplying fuel to a gas turbine |
| 04/19/2012 | DE102010048926A1 Antriebswelle, insbesondere Radialwelle für ein Gasturbinentriebwerk Drive shaft, in particular radial shaft for a gas turbine engine |
| 04/19/2012 | DE102010048434A1 Turbinenradanordnung für eine Gas- oder Dampfturbine Turbine wheel for a gas or steam turbine |
| 04/19/2012 | CA2813957A1 Generating power using an ion transport membrane |
| 04/19/2012 | CA2813569A1 Connecting module between a drive shaft of an engine fan and a rolling element bearing |
| 04/18/2012 | EP2441940A2 Method of controlling the operation of a fuel metering unit and such a unit |
| 04/18/2012 | EP2441937A1 Apparatus and method for purging a liquid fuel injection system in a gas turbine |
| 04/18/2012 | EP2441166A1 Method and assembly for the turning gear operation of a turbo set |
| 04/18/2012 | EP2440747A1 Turbomachine |
| 04/18/2012 | CN202194728U 附件箱传动装置及具有其的航空发动机 Accessory gear box and has its aero-engine |
| 04/18/2012 | CN202194727U 改进的燃汽轮机旁路阀门位置反馈装置 Improved combustion turbine bypass valve position feedback device |
| 04/18/2012 | CN102418604A 压力促动的栓 Pressure-actuated bolt |
| 04/18/2012 | CN102418603A 叶片防冰装置及具有该叶片防冰装置的叶片防冰系统 Blade anti-icing device and the blade anti-icing device having a blade anti-ice system |
| 04/18/2012 | CN102418602A Turbomachine including a ceramic matrix composite (cmc) bridge |
| 04/17/2012 | US8157506 Device for supplying ventilation air to the low pressure blades of a gas turbine engine |
| 04/17/2012 | US8156742 Fuel-injection device in a turbomachine |
| 04/17/2012 | US8156726 Semiclosed Brayton cycle power system with direct combustion heat transfer |
| 04/17/2012 | US8156725 CO2 capture during compressed air energy storage |
| 04/17/2012 | US8156724 Combustion chamber |
| 04/17/2012 | CA2714525C Swirl generator |
| 04/12/2012 | WO2012021285A3 Adiabatic compressed air energy storage process |
| 04/12/2012 | WO2012009575A3 Generating power using an ion transport membrane |
| 04/12/2012 | WO2011073664A3 A gas turbine generator |
| 04/12/2012 | US20120085104 Turbine engine including an improved means for adjusting the flow rate of a cooling air flow sampled at the output of a high-pressure compressor |
| 04/12/2012 | US20120085103 Shim for sealing transition pieces |
| 04/12/2012 | US20120085102 Method for purifying flue gases of a gas engine |
| 04/12/2012 | US20120085100 Combustor with a Lean Pre-Nozzle Fuel Injection System |
| 04/12/2012 | US20120085099 Tunable seal in a gas turbine engine |
| 04/12/2012 | DE102011054387A1 System und Verfahren zur Turbinenraumbelüftung SYSTEM AND METHOD FOR turbine ventilation |
| 04/12/2012 | DE102011054308A1 Brennkammer mit einem Magerbetrieb-Vordüsen-Brennstoffeinspritzsystem Combustion chamber with a lean operation fuel injection system pre-orifices |
| 04/12/2012 | DE102011052420A1 Beilage zur Abdichtung von Übergangsstücken Supplement for sealing transition pieces |
| 04/12/2012 | DE102010048147A1 Schichtsystem zur Rotor-/Statordichtung einer Strömungsmaschine und Verfahren zum Herstellen eines derartigen Schichtsystems Layer system for the rotor / stator seal of a turbo machine and method for producing such a layer system |
| 04/12/2012 | DE102010047971A1 Haupttriebwerksstart mit Hilfe einer flugzeugseitigen Klimaanlage Main engine start using a plane-side air conditioning |
| 04/12/2012 | DE102010047612A1 Impeller used as e.g. compressor wheel of e.g. supercharger, has blades that include partial sections comprising sub-elements which are provided in axial direction and arranged with respect to rotational axis |
| 04/11/2012 | EP2439448A1 Method and device for detecting liquid fuel leakage in a gas turbine system combustion assembly |
| 04/11/2012 | EP2439390A1 Control method for cooling a turbine stage in a gas turbine |
| 04/11/2012 | EP2439389A1 Method for manufacturing combustor constituent member, combustor constituent member, gas turbine combustor, and gas turbine |
| 04/11/2012 | EP2439388A1 Solar gas turbine and solar gas turbine power generating device |
| 04/11/2012 | EP2438278A2 Internal combustion engine |
| 04/11/2012 | EP2438274A1 Device and method for detecting a fault in a low-pressure fuel pump of a turbojet and turbojet including one such device |
| 04/11/2012 | EP1582289B1 Apparatus and method for repairing tenons on turbine buckets |
| 04/11/2012 | CN102414522A 跨临界热激活的冷却、加热和制冷系统 Transcritical thermally activated cooling, heating and cooling systems |
| 04/11/2012 | CN102414422A 用于航空设备的单件托架 One-piece bracket for aviation equipment |
| 04/11/2012 | CN102414398A Split ring cooling structure and gas turbine |
| 04/11/2012 | CN102410088A Adjustable guide vane system of gas turbine power turbine |
| 04/11/2012 | CN101307442B Method for making high-temperature articles |
| 04/10/2012 | US8152471 Apparatus and method for retaining bladed rotor disks of a jet engine |
| 04/10/2012 | US8151574 Gas turbine integrated with fuel catalytic partial oxidation |
| 04/10/2012 | US8151573 Turbomachine flameout confirmation |
| 04/10/2012 | US8151572 Method of starting and stopping gas turbine and start-and-stop control device |
| 04/10/2012 | US8151549 High humidity gas turbine equipment |
| 04/10/2012 | CA2703115C Passive cooling system for auxiliary power unit installation |
| 04/10/2012 | CA2557440C Dual conduit fuel manifold for gas turbine engine |
| 04/05/2012 | WO2012045035A2 Fuel storage system |
| 04/05/2012 | WO2012045034A2 Aircraft engine systems and methods for operating same |
| 04/05/2012 | WO2012045029A1 Dual fuel aircraft engine control system and method for operating same |
| 04/05/2012 | WO2012045028A1 Dual fuel aircraft system and method for operating same |
| 04/05/2012 | WO2012043073A1 Air recovery-type cooling structure for air-cooled gas turbine combustor |
| 04/05/2012 | WO2012042655A1 Gas turbine system, control device for gas turbine system, and control method for gas turbine system |
| 04/05/2012 | WO2012042652A1 Gas turbine system and method of controlling same |
| 04/05/2012 | WO2012042641A1 Combined cycle plant utilizing solar heat |
| 04/05/2012 | WO2012042639A1 Combined cycle power generation plant utilzing solar heat |
| 04/05/2012 | WO2012042638A1 Solar heat utilization gas turbine plant |
| 04/05/2012 | WO2012042628A1 Gas turbine power generation device, gas turbine power generation system, and method of controlling the system |
| 04/05/2012 | WO2012022869A3 Acoustic panel for a turbojet engine nacelle, with in-built fasteners |
| 04/05/2012 | WO2011139741A3 Brush ring seal |
| 04/05/2012 | WO2006120168A8 Fuel supply for a gas turbine, comprising a deviation zone |
| 04/05/2012 | US20120079832 Device and method for detecting a fault in a low-pressure fuel pump of a turbojet and turbojet including one such device |
| 04/05/2012 | US20120079831 Method, apparatus and system for igniting wide range of turbine fuels |
| 04/05/2012 | US20120079829 Turbomachine including a mixing tube element having a vortex generator |
| 04/05/2012 | US20120079828 Gas Turbine Combustor |
| 04/05/2012 | US20120079827 Air-cooled swirlerhead |
| 04/05/2012 | DE102011054175A1 Verfahren, Vorrichtung und System zur Zündung eines breiten Spektrums an Turbinenbrennstoffen A method, apparatus and system for igniting a wide range of turbine fuels |