| 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) |
|---|
| 02/26/2008 | US7334407 Method of suppressing coke in endothermic fuel processing |
| 02/26/2008 | US7334391 Electric power supply equipment |
| 02/26/2008 | US7334389 Afterburner igniter |
| 02/26/2008 | US7334333 Method for making a hollow fan blade with machined internal cavities |
| 02/26/2008 | US7334332 Method of manufacturing a hollow blade for a turbine engine |
| 02/26/2008 | US7334331 Methods and apparatus for machining components |
| 02/26/2008 | US7334328 Method of manufacturing axis seals having reduced gas leakage properties and a rotary machine using axis seals |
| 02/26/2008 | US7334306 Methods and apparatus for fabricating a turbine nozzle assembly |
| 02/25/2008 | CA2598435A1 Interturbine duct with integrated baffle and seal |
| 02/25/2008 | CA2598379A1 Oil bearing and tube assembly concept |
| 02/23/2008 | CA2596484A1 Strainer for a gas turbine engine |
| 02/22/2008 | CA2597272A1 Optimized internal manifold heat shield attachment |
| 02/22/2008 | CA2594062A1 Oil strainer for a gas turbine engine |
| 02/21/2008 | WO2008020483A1 Bearing device for gas turbine power generation facility and gas turbine power generation facility |
| 02/21/2008 | WO2008019493A1 Gas turbine engine exhaust duct ventilation |
| 02/21/2008 | US20080042857 Fire Warning System |
| 02/21/2008 | US20080041058 Resonator device at junction of combustor and combustion chamber |
| 02/21/2008 | US20080040872 System for Washing an Aero Gas Turbine Engine |
| 02/21/2008 | DE102006037571A1 Aircraft gas turbine, has connecting area thermally isolated and radially shielded by ring unit against outlet area of compressor plate in flow direction, and impeller and turbine connected with each other using shaft |
| 02/21/2008 | DE102006032429A1 Kraftstoffeinspritzvorrichtung für eine Fluggasturbine Fuel injection device for an aircraft gas turbine |
| 02/20/2008 | EP1888894A1 System for deicing the leading edge of a nose inlet cowl for a turbine engine |
| 02/20/2008 | EP1888880A1 Gas turbine with a gap blocking device |
| 02/20/2008 | EP1360439B1 A method and a device for supplying fuel to a combustion chamber |
| 02/20/2008 | CN201025157Y Micro turbine jet engine |
| 02/20/2008 | CN201025131Y Frequency conversion startup device of steamship engine |
| 02/20/2008 | CN201025130Y Culvert straight axis gas engine |
| 02/20/2008 | CN201025129Y A supporting base for steamship machine |
| 02/20/2008 | CN101128662A Aircraft engine fuel supply |
| 02/20/2008 | CN101126353A 燃气轮机系统和燃气轮机控制方法 Gas turbine and gas turbine system control method |
| 02/20/2008 | CN101126351A Low flow resistance veneer structure |
| 02/20/2008 | CN101126350A Square shape auxiliary flow-disturbing column veneer structure |
| 02/20/2008 | CN101126349A Ancient coin type flow-disturbing column veneer structure |
| 02/20/2008 | CN100370177C Combustion chamber for firing one kind of combustable liquid mixed fuel |
| 02/19/2008 | US7331755 Method for coating gas turbine engine components |
| 02/19/2008 | US7331219 Method for determining fluctuating fuel properties during the operation of a power plant |
| 02/19/2008 | US7331182 Combustion chamber for a gas turbine |
| 02/19/2008 | US7331169 Control logic for fuel controls on APUs |
| 02/19/2008 | CA2361962C Gas turbine combustor with cooling water injection |
| 02/14/2008 | WO2008017567A1 Air inlet for a jet engine |
| 02/14/2008 | US20080034759 Methods and apparatus for radially compliant component mounting |
| 02/14/2008 | US20080034756 Air Compression Heat Accumulating Power Plant With An Underground Heat Accumulator Formed In The Aquifer (Gaes) |
| 02/14/2008 | US20080034727 Triple Cycle Power Plant |
| 02/13/2008 | EP1887199A2 Gas turbine engine assembly |
| 02/13/2008 | EP1887198A1 Gasification hybrid power generation equipment and method for controlling the same |
| 02/13/2008 | EP1885999A1 An air intake for a turbocharger for an internal combustion engine |
| 02/13/2008 | EP1629184B1 A method for operation of a gas turbine group |
| 02/13/2008 | EP1546522B1 Internally mounted radial flow intercooler for a combustion air charger |
| 02/13/2008 | EP1504177B1 Variable, exhaust-gas turbocharger with an auxiliary drive for an internal combustion engine |
| 02/13/2008 | EP1441874A4 Method for removing coating material from a cooling hole of a gas turbine engine component |
| 02/13/2008 | CN101122260A Heat transfer system and method for turbine engine using heat pipes |
| 02/13/2008 | CN100368712C Sealer |
| 02/13/2008 | CN100368667C Attenuated and diffused combustion nozzle of combustion turbine |
| 02/13/2008 | CN100368666C Humidification method of eddy flow spray and humidification tower |
| 02/13/2008 | CN100368665C Combined cycle method and installation of combustion turbine of burning blast furnace gas |
| 02/12/2008 | US7328771 Zero acoustic splice fan case liner |
| 02/12/2008 | US7328581 Low emission thermal plant |
| 02/12/2008 | CA2373192C Device for controlling air flow in a turbine blade |
| 02/07/2008 | WO2008015777A1 Air cycle refrigerating machine turbine unit |
| 02/07/2008 | WO2008015145A1 Method of analysis of secondary-air circuits in gas-turbine plants |
| 02/07/2008 | US20080028766 Highly Efficient Heat Cycle Device |
| 02/07/2008 | DE202004021368U1 System und Vorrichtungen zum Behandeln von Abwässern von einer Triebwerksreinigung System and apparatus for treating wastewater of an engine cleaning |
| 02/07/2008 | DE102006036648A1 Eisschlagschutzring für das Fangehäuse einer Fluggasturbine Eisschlagschutzring for the fan casing of an aircraft gas turbine |
| 02/07/2008 | DE102006036520A1 Gasturbinenbauteil mit einer Wärmedämmschicht, Wärmedämmschicht für ein Gasturbinenbauteil sowie Verfahren zur Herstellung einer Wärmedämmschicht auf einem Gasturbinenbauteil A gas turbine component having a thermal barrier coating, the thermal barrier coating on a gas turbine component and method for preparing a thermal barrier coating on a gas turbine component |
| 02/07/2008 | DE102006028059A1 Working fluid heating method for e.g. operating steam engine, involves absorbing primary energy from primary heating fluid based on its flow at closed loop in heater to continuously deliver energy to working fluid for heating working fluid |
| 02/06/2008 | EP1884879A1 Method of analysis of secondary air circuits in gas turbine plants |
| 02/06/2008 | EP1884640A1 Method of operation of a gas turbine plant, control device and a gas and steam turbine plant |
| 02/06/2008 | EP1884639A2 Ice strike sheathing ring for the fan casing of an aircraft engine |
| 02/06/2008 | CN201016307Y Combustion engine set lubricating oil and jacking oil supplying system |
| 02/06/2008 | CN201016306Y Dust combustion engine |
| 02/06/2008 | CN101117919A Cooling of a shroud hanger assembly of a gas turbine engine |
| 02/06/2008 | CN100366866C Turbine bucket damper pin |
| 02/06/2008 | CN100366379C Surface processing method for matchable, conforming to fluid tech. |
| 02/05/2008 | US7326873 Apparatus and methods for repairing tenons on turbine buckets |
| 02/05/2008 | US7325402 Pilot nozzle heat shield having connected tangs |
| 02/05/2008 | CA2488316C Thermal management system for an aircraft |
| 02/05/2008 | CA2291606C Dual-contact brush seal |
| 01/31/2008 | WO2008012117A1 Method for operating a power station with integrated coal gasification and power station |
| 01/31/2008 | US20080027639 Method of anticipating a vehicle destination |
| 01/31/2008 | US20080022692 Embedded mount for mid-turbine frame |
| 01/31/2008 | US20080022687 Method for starting a pressure storage plant and pressure storage plant |
| 01/31/2008 | US20080022683 Storing Thermal Energy and Generating Electricity |
| 01/31/2008 | DE202004021367U1 Apparat zur Reinigung eines Turbofan-Gasturbinentriebwerks An apparatus for cleaning a turbofan gas turbine engine |
| 01/30/2008 | EP1882824A2 Lubricant cooling exchanger dual intake duct |
| 01/30/2008 | CN101115954A Method for controlling calorific value of gas and apparatus for controlling calorific value of gas |
| 01/30/2008 | CN101113689A Heat transfer system and method for turbine engine using heat pipes |
| 01/30/2008 | CN100365257C Methods and apparatus for cooling gas turbine engine rotor assemblies |
| 01/30/2008 | CN100365249C Gas turbine group |
| 01/30/2008 | CN100365248C Running controlling apparatus and running controlling method for single-shaft combine equipment with clutch |
| 01/30/2008 | CN100365247C Combined circulation generator and steam supply method for cooling |
| 01/29/2008 | US7322373 High accuracy low leakage valve for high pressure applications |
| 01/29/2008 | US7322198 System for vaporization of liquid fuels for combustion and method of use |
| 01/29/2008 | US7322197 Variable rate ignition |
| 01/29/2008 | US7322196 Combustion chamber for combusting a combustible fluid mixture |
| 01/29/2008 | US7322195 Acoustic dampers |
| 01/29/2008 | US7322181 Turbofan engine with the fan fixed to a drive shaft supported by a first and a second bearing |
| 01/29/2008 | US7322180 Turbo-jet engine with fan integral with a drive shaft supported by first and second bearings |
| 01/29/2008 | US7322179 Air intake and method for breathing air using an air intake |
| 01/29/2008 | US7322178 Device for indicating a residual power margin of aircraft turbine engines |
| 01/28/2008 | CA2594049A1 Heat transfer system and method for turbine engine using heat pipes |
| 01/28/2008 | CA2594048A1 Heat transfer system and method for turbine engine using heat pipes |