| 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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| 11/13/2008 | CA2685514A1 Method of starting turbine engine from low engine speed |
| 11/13/2008 | CA2682306A1 Method for producing an acoustically resistive structure, resulting acoustically resistive structure and skin using one such structure |
| 11/12/2008 | EP1990521A1 Pressure dynamics reduction within a gas turbine engine |
| 11/12/2008 | EP1990519A2 Method of operating a gas turine engine |
| 11/12/2008 | EP1990518A2 Power generation system for an aircraft |
| 11/12/2008 | EP1990517A2 Power generation system for an aircraft |
| 11/12/2008 | EP1990507A1 Impingement cooling structure |
| 11/12/2008 | CN201148909Y Fire coal turbine power device |
| 11/12/2008 | CN100433433C Fuel cell/constant pressure turbine/hybrid system |
| 11/12/2008 | CN100432459C Bearing device for turbocharger |
| 11/11/2008 | US7449251 Heat resistant article having thermal barrier coating |
| 11/11/2008 | US7448845 Gas turbine engine |
| 11/11/2008 | US7448808 Arrangement of bearing supports for the rotating shaft of an aircraft engine and an aircraft engine fitted with such an arrangement |
| 11/11/2008 | US7448220 Torque control for starting system |
| 11/11/2008 | US7448219 Hingeless flapper valve for flow control |
| 11/11/2008 | US7448217 Power plant |
| 11/11/2008 | US7448216 Methods and apparatus for operating gas turbine engine combustors |
| 11/11/2008 | US7448215 Combustion chamber for a gas turbine engine |
| 11/06/2008 | WO2008132410A2 Double seal with pressurised lip |
| 11/06/2008 | WO2008132400A2 System for cooling and adjusting the temperature of apparatuses in the propulsion assembly of an aircraft |
| 11/06/2008 | WO2008132376A1 Device for de-icing the air intake of a gas turbine |
| 11/06/2008 | WO2008132321A1 Lockable guiding system for a mobile part of a nacelle |
| 11/06/2008 | WO2008104716A3 Method for making an acoustic treatment coating and coating thus obtained |
| 11/06/2008 | US20080273963 Impingement skin core cooling for gas turbine engine blade |
| 11/06/2008 | US20080271787 Isentropic compression inlet for supersonic aircraft |
| 11/06/2008 | US20080271461 Method of starting turbine engine from low engine speed |
| 11/06/2008 | CA2681220A1 Device for de-icing the air intake of a gas turbine |
| 11/06/2008 | CA2678657A1 System for cooling and adjusting the temperature of apparatuses in the propulsion assembly of an aircraft |
| 11/06/2008 | CA2677567A1 Lockable guiding system for a mobile part of a nacelle |
| 11/05/2008 | EP1988268A2 Method of starting turbine engine from low engine speed |
| 11/05/2008 | EP1988267A2 Fuel supply system |
| 11/05/2008 | EP1988266A2 Nacelle assembly having inlet airfoil for a gas turbine engine |
| 11/05/2008 | EP1988261A1 Casing gasket |
| 11/05/2008 | EP1988260A2 Method and system for regulating a cooling fluid within a turbomachine in real time |
| 11/05/2008 | EP1988259A2 Turbine nozzle with de-icing device |
| 11/05/2008 | EP1888880B1 Gas turbine with a gap blocking device |
| 11/05/2008 | EP1685310B1 Sealing arrangement in a compressor |
| 11/05/2008 | CN101300406A 涡轮的清洁 Clean turbine |
| 11/05/2008 | CN101298978A Shaft-misalignment-measuring device and shaft-misalignment-measuring method |
| 11/05/2008 | CN100430584C Fixed geometrical supersonic-speed and high supersonic-speed adjusting air inlet |
| 11/05/2008 | CN100430574C Spring mass damper system for turbine shrouds |
| 11/04/2008 | US7445434 Coating material for thermal barrier coating having excellent corrosion resistance and heat resistance and method of producing the same |
| 11/04/2008 | US7444820 Method and system for rich-lean catalytic combustion |
| 11/04/2008 | US7444819 Gas turbine installation including a compressed air humidifier and method |
| 11/04/2008 | US7444802 Gas turbine engine including stator vanes having variable camber and stagger configurations at different circumferential positions |
| 11/03/2008 | CA2630249A1 Low profile bleed air cooler |
| 10/30/2008 | WO2008131432A1 Multi-point injection mixer |
| 10/30/2008 | WO2008130890A2 Generating energy from fluid expansion |
| 10/30/2008 | WO2008130739A1 Articles made from composite materials having toughened and untoughened regions |
| 10/30/2008 | WO2008129652A1 Gas turbine power generating apparatus and method of starting the same |
| 10/30/2008 | WO2008128326A1 Surge detection in a gas turbine engine |
| 10/30/2008 | WO2008128325A1 Improved start flow measurement |
| 10/30/2008 | WO2008128322A2 Diffuser with improved erosion resistance |
| 10/30/2008 | US20080267766 Rotor supports and systems |
| 10/30/2008 | US20080264067 Controlling operation of a compressor to avoid surge |
| 10/30/2008 | US20080264064 Floatwall dilution hole cooling |
| 10/30/2008 | DE112006003270T5 Verzögerungs- und Filterreinigungsverfahren und -system Delay and filter cleaning method and system |
| 10/30/2008 | DE102007020025A1 Form eines Gaskanals in einer Axialströmungs-Gasturbinenmaschine Form a gas channel in an axial flow gas turbine engine |
| 10/30/2008 | DE102007019762A1 Schallschutzvorrichtung für ein Strahltriebwerk oder eine Turbine Acoustic shielding device for a jet engine or a turbine |
| 10/30/2008 | DE10155508C5 Verfahren und Vorrichtung zur Erzeugung von elektrischer Energie Method and apparatus for production of electric energy |
| 10/30/2008 | CA2684510A1 Diffuser with improved erosion resistance |
| 10/30/2008 | CA2683945A1 Surge detection in a gas turbine engine |
| 10/30/2008 | CA2683942A1 Improved start flow measurement |
| 10/30/2008 | CA2683851A1 Articles made from composite materials having toughened and untoughened regions |
| 10/29/2008 | EP1985863A2 Surge detection in a gas turbine engine |
| 10/29/2008 | EP1985862A1 Controlling operation of a compressor to avoid compressor instability |
| 10/29/2008 | EP1985823A1 Device for producing electric energy in a twin-shaft gas turbine engine |
| 10/29/2008 | EP1985822A2 Start fuel flow measurement |
| 10/29/2008 | EP1985804A1 Cooling structure |
| 10/29/2008 | EP1984602A2 Organic rankine cycle (orc) turbogenerator |
| 10/29/2008 | EP1913242B1 Sound absorber for gas turbine installations |
| 10/29/2008 | CN100429387C Heat and electric power supply system and operation method thereof |
| 10/29/2008 | CN100429384C Flexibly jointed double casing type bearing seat |
| 10/29/2008 | CN100429382C Turbine blade and method for producing turbine blade |
| 10/29/2008 | CN100429381C Mounting method and device for gas turbine jet nozzle |
| 10/28/2008 | US7441585 Apparatus and method for reducing operating stress in a turbine blade and the like |
| 10/28/2008 | US7441399 Gas turbine, combined cycle plant and compressor |
| 10/27/2008 | CA2629798A1 Check valve for a cooling system in a turbine engine |
| 10/27/2008 | CA2629795A1 Device for generating electrical energy in a two-stage gas turbine engine |
| 10/23/2008 | WO2008127467A2 Ceramic-encased hot surface igniter system for jet engines |
| 10/23/2008 | WO2008126242A1 Gum-like substance monitoring apparatus and detecting method and gas turbine equipment |
| 10/23/2008 | WO2008125907A2 Method and apparatus for isolating inactive fuel passages |
| 10/23/2008 | WO2008125507A1 Assembly device for assembling and disassembling a rotor of a turbomachine consisting of rotor disks |
| 10/23/2008 | WO2008125506A1 Securing device for securing a rotor of a turbomachine counter to tilting, said rotor being arranged perpendicular to a horizontal plane and method for the alignment thereof |
| 10/23/2008 | WO2008065517A3 Combined-cycle plant for generation of electrical energy |
| 10/23/2008 | US20080257146 Method of suppressing coke in endothermic fuel processing |
| 10/23/2008 | DE112006003297T5 Befestigung von Gasturbinentriebwerks-Zusatzkomponenten Assembly of gas turbine engine auxiliary components |
| 10/23/2008 | DE112006002967T5 Restdampf-Abführmechanismus und Restdampf-Abführverfahren für eine Dampfkühlleitung einer Gasturbine Residual steam feed-out and final vapor Abführverfahren for a steam cooling line of a gas turbine |
| 10/23/2008 | DE10217225B4 Aufgeladene mehrzylindrige Brennkraftmaschine Charged multi-cylinder internal combustion engine |
| 10/23/2008 | DE102007017823A1 Turbolader mit einer Einrichtung zum Feststellen einer Fehlfunktion des Turboladers und ein Verfahren zum Feststellen einer solchen Fehlfunktion Turbocharger with a device for detecting a malfunction of the turbocharger and a method of detecting such a malfunction |
| 10/22/2008 | EP1983174A2 Apparatus and method of operating a gas turbine engine at start-up |
| 10/22/2008 | EP1983161A1 Safety device for protection of a rotor of a fluid flow engine installed at right angles to the horizontal plane against overturning and mounting device |
| 10/22/2008 | EP1983160A2 Gas turbine engine vane |
| 10/22/2008 | EP1982791A2 Manufacturing method for a hollow fan blade |
| 10/22/2008 | CN101289963A Compressed-air energy-storage system |
| 10/22/2008 | CN100427738C Gas turbine controller |
| 10/22/2008 | CN100427737C Gas turbine controller |
| 10/22/2008 | CN100427736C Provision of sealing for the cabin-air bleed cavity of a jet engine using strip-type seals acting in two directions |
| 10/21/2008 | US7438523 Blade for a turbine engine and method for production of said blade |
| 10/21/2008 | US7438492 Link between two mechanical members |