| 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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| 08/07/2001 | US6270037 Rapid response attitude control logic for shaft-driven lift fan STOVL engine |
| 08/07/2001 | US6269628 Apparatus for reducing combustor exit duct cooling |
| 08/07/2001 | US6269626 Regenerative fuel heating system |
| 08/07/2001 | US6269625 Methods and apparatus for igniting a catalytic converter in a gas turbine system |
| 08/07/2001 | CA2255883C Combustor tail tube cooling structure |
| 08/07/2001 | CA2229880C Gas turbine seal apparatus |
| 08/02/2001 | WO2001055625A1 Self-centering brush seal |
| 08/02/2001 | WO2001055273A2 Thermal shield for a component carrying hot gases, especially for structural components of gas turbines |
| 08/02/2001 | WO2001054981A2 Propulsion module |
| 08/02/2001 | WO2000071781A3 Bond coats for turbine components and method of applying the same |
| 08/02/2001 | WO2000038985A9 Low drag ducted ram air turbine generator and cooling system |
| 08/02/2001 | US20010010797 Connector tube for a turbine rotor cooling circuit |
| 08/02/2001 | DE10002581A1 Turbocharger for gas fuelled engines has gas passage openings in air induction pipe of compressor for feed of gas and located in region of smallest diameter |
| 08/02/2001 | DE10002084A1 Gas- und Dampfturbinenanlage Gas and steam turbine plant |
| 08/01/2001 | EP1120559A2 System and method for pressure modulation of turbine sidewall cavities |
| 08/01/2001 | EP1120544A1 Turbo machine with a device for supplying a pressurized gas |
| 08/01/2001 | EP1120480A2 Enhanced coating system for turbine airfoil applications |
| 08/01/2001 | EP1119693A1 Exciter controlled by full authority digital electronic control (fadec) system |
| 07/31/2001 | US6268913 Method and combustor apparatus for sensing the level of a contaminant within a combustion flame |
| 07/31/2001 | US6266961 Film cooled combustor liner and method of making the same |
| 07/31/2001 | US6266954 Double wall bearing cone |
| 07/31/2001 | CA2070435C Vane line with axially positioned heat shields |
| 07/26/2001 | WO2001053729A1 Thermally stressable wall and method for sealing a gap in a thermally stressed wall |
| 07/26/2001 | WO2001053660A1 Gas and steam turbine installation |
| 07/26/2001 | US20010009247 Method of removing a thermal barrier coating |
| 07/26/2001 | US20010009246 Method of removing ceramic coatings |
| 07/25/2001 | EP1118920A1 Machine protection system for rotating equipment and method |
| 07/25/2001 | EP1118806A1 Thermally charged wall structure and method to seal gaps in such a structure |
| 07/25/2001 | EP1118695A2 Method of removing a thermal barrier coating |
| 07/25/2001 | EP1118419A2 Method of forming cooling holes |
| 07/25/2001 | EP1117913A1 Fuel preheating in a gas turbine |
| 07/25/2001 | EP1117912A1 Gas turbine engine |
| 07/25/2001 | EP1117588A1 Aircraft engine air intake system |
| 07/24/2001 | US6265080 Pest resistant molybdenum disilicide type materials |
| 07/24/2001 | US6264426 Gas turbine stationary blade |
| 07/24/2001 | US6263678 Method of evaporating a low temperature liquid medium |
| 07/24/2001 | US6263664 Combined steam and gas turbine engine with magnetic transmission |
| 07/24/2001 | US6263662 Combined cycle power generation plant and cooling steam supply method thereof |
| 07/24/2001 | US6263661 System for power generation |
| 07/24/2001 | CA2234922C Cooled shroud of gas turbine stationary blade |
| 07/24/2001 | CA2229322C Cooling medium path in gas turbine moving blade |
| 07/19/2001 | WO2001051787A1 Piloted airblast lean direct fuel injector |
| 07/19/2001 | WO2001051772A1 Turbine blade and method of repair |
| 07/19/2001 | US20010008708 Ceramic heat barrier coating having low thermal conductivity, and process for the deposition of said coating |
| 07/19/2001 | US20010008323 Method and fixture for disposing filler material in an article |
| 07/19/2001 | US20010008069 Method for supplying lift and hydraulic fluid for a gas turbine |
| 07/19/2001 | DE10001112A1 Cooling air cooler for gas turbine unit, with water separator on cooling air side behind jet device in flow direction |
| 07/18/2001 | EP1116861A2 A cooling circuit for and method of cooling a gas turbine bucket |
| 07/18/2001 | EP1116523A2 Masking fixture and method |
| 07/18/2001 | EP1115967A2 Fan noise reduction from turbofan engines using adaptive herschel-quincke tubes |
| 07/18/2001 | EP1115963A2 Gas turbine engine |
| 07/18/2001 | EP1115906A1 Method for processing the interior of a hollow part |
| 07/18/2001 | EP0839285B1 Compressor stall and surge control using airflow asymmetry measruement |
| 07/18/2001 | EP0797729B1 Recuperative steam cooled gas turbine |
| 07/17/2001 | US6260658 Silencer for a gas turbine |
| 07/17/2001 | US6260567 Mission adaptive inlet |
| 07/17/2001 | US6260351 Controlled spring rate gearbox mount |
| 07/17/2001 | US6260350 Gas turbine |
| 07/17/2001 | US6260349 Multi-stage turbo-machines with specific blade dimension ratios |
| 07/17/2001 | US6260347 Method of and apparatus for generating power |
| 07/12/2001 | WO2001050000A1 Silencer for the compressor of an exhaust gas turbocharger |
| 07/12/2001 | DE19960278A1 Maschinensatz Machine set |
| 07/12/2001 | DE10053432A1 Selbstbindende MCrAlY-Pulver Self-binding MCrAlY powder |
| 07/11/2001 | EP1114991A2 Methods and systems for estimating engine faults |
| 07/11/2001 | EP1114878A1 Alloy of molybdenum disilicide containing rhenium which is pest resistant |
| 07/11/2001 | EP1114279A1 Dynamic control system and method for catalytic combustion process and gas turbine engine utilizing same |
| 07/11/2001 | EP1114241A1 Sealing ring for non-hermetic fluid seals |
| 07/11/2001 | EP1113959A1 Multi-linkage suspension system including outboard isolators |
| 07/11/2001 | CN1068409C Cooling system for gas turbine |
| 07/11/2001 | CN1068408C Power apparatus |
| 07/10/2001 | US6257834 Method and arrangement for the indirect cooling of the flow in radial gaps formed between rotors and stators of turbomachines |
| 07/10/2001 | US6257828 Turbine blade and method of producing a turbine blade |
| 07/10/2001 | US6256995 Simple low cost fuel nozzle support |
| 07/10/2001 | US6256978 Power generation in a combination power plant with a gas turbine and a steam turbine |
| 07/10/2001 | US6256976 Exhaust gas recirculation type combined plant |
| 07/10/2001 | US6256975 Method for reliably removing liquid fuel from the fuel system of a gas turbine, and a device for carrying out the method |
| 07/10/2001 | CA2229218C Gas-turbine engine |
| 07/05/2001 | WO2001048887A2 Brush seal |
| 07/05/2001 | WO2001048404A1 Brush seals |
| 07/05/2001 | WO2000020738A9 Gas turbine engine |
| 07/05/2001 | US20010006707 Method and apparatus for thermal barrier coating and removal |
| 07/05/2001 | US20010006601 Steam cooling system for a gas turbine |
| 07/05/2001 | US20010006278 Sealing configuration, in particular for a rotary machine |
| 07/04/2001 | EP1113162A2 Ducting for duel fan concept |
| 07/04/2001 | EP1113159A2 Method and apparatus for encapsulating gas turbine engine fuel connections |
| 07/04/2001 | EP1113146A2 Rotatory machine having a seal assembly |
| 07/04/2001 | CN1068092C Process for cooling coolant of gas turbine and device for carrying out said process |
| 07/03/2001 | US6254346 Gas turbine cooling moving blade |
| 07/03/2001 | US6253554 Gas turbine plant with fuel heating and turbine cooling features |
| 06/28/2001 | WO2001046944A1 Fan and compressor noise attenuation |
| 06/28/2001 | WO2001046576A1 Method for operating a steam turbine, and a turbine system provided with a steam turbine that functions according to said method |
| 06/28/2001 | WO2001046563A1 Machine set |
| 06/28/2001 | WO2001045877A2 Multi-wall core and process |
| 06/28/2001 | US20010005480 Apparatus and methods for relieving thermally induced stresses in inner and outer bands of thermally cooled turbine nozzle stages |
| 06/28/2001 | US20010004835 Combustion chamber for a gas turbine engine |
| 06/28/2001 | US20010004828 Gas turbine fuel system comprising fuel oil distribution control system, fuel oil purge system, purging air supply system and fuel nozzle wash system |
| 06/28/2001 | US20010004827 Fuel system configuration for staging fuel for gas turbines utilizing both gaseous and liquid fuels |
| 06/28/2001 | DE19962244A1 Kühlluft-Führungssystem im Hochdruck-Turbinenabschnitt eines Gasturbinen Triebwerkes Cooling air guide system in the high pressure turbine section of a gas turbine engine |
| 06/27/2001 | EP1111323A2 Article surface with metal wires and method for making |
| 06/27/2001 | EP1111226A1 Hot air exhaust device for a jet engine air intake fairing with de-icing circuit |