Patents
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)
10/2006
10/11/2006EP1710418A2 Fuel conveying member with phase change cooling means
10/11/2006EP1488080B1 Refrigeration power plant
10/11/2006EP1386060B1 Turbine or compressor device and method for assembling the device
10/11/2006EP1330593B1 Uninterruptible oil supply system
10/11/2006EP1287234B1 Device for controlling the cooling flows of gas turbines
10/10/2006US7118636 Precipitation-strengthened nickel-iron-chromium alloy
10/10/2006US7118464 Apparatus for smoothing the surface of a gas turbine blade
10/10/2006US7118336 Pressurized oil supply for propeller engine system
10/10/2006US7117983 Support apparatus and method for ceramic matrix composite turbine bucket shroud
10/10/2006US7117683 Main engine electric start system
10/10/2006US7117680 Cooling scheme for scramjet variable geometry hardware
10/10/2006US7117678 Fuel injector head
10/10/2006US7117676 Apparatus for mixing fluids
10/10/2006US7117675 Cooling of liquid fuel components to eliminate coking
10/10/2006US7117674 Catalytic combustor and method for substantially eliminating various emissions
10/10/2006US7117662 Gas turbine control system
10/10/2006CA2344128C Method and apparatus for the cooling of jet-engine turbine casings
10/10/2006CA2326423C Combustor rear facing step hot side contour method and apparatus
10/05/2006WO2006104059A1 COBALT-FREE Ni BASE SUPERALLOY
10/05/2006WO2006102765A1 Internal fuel manifold with airblast nozzles
10/05/2006WO2006102761A1 Fuel conveying member with heat pipe
10/05/2006US20060222919 Fuel cell/constant pressure turbine/hybrid system
10/05/2006US20060218933 Method for producing a model-based control device
10/05/2006US20060218931 Method for injecting a liquid mist into an intake duct
10/05/2006US20060218930 Temperature measuring device and regulation of the temperature of hot gas of a gas turbine
10/05/2006US20060218926 Fuel conveying member with heat pipe
10/05/2006US20060218925 Internal fuel manifold with airblast nozzles
10/05/2006US20060218911 Pressure regulator
10/05/2006CA2604636A1 Internal fuel manifold with airblast nozzles
10/05/2006CA2603410A1 Fuel conveying member with heat pipe
10/04/2006EP1707761A1 Turbogenerator
10/04/2006EP1707752A1 Turbogenerator
10/04/2006EP1706620A1 Gas turbine engine architecture
10/04/2006EP1706316A1 Pressurized oil supply for propeller engine system
10/04/2006EP1631417B1 A turbine blade
10/04/2006CN1840878A Two-spool turbomachine, driving module for the turbomachine and turbomachine assembly method
10/04/2006CN1278063C Shaft sealer and turbine
10/04/2006CN1278062C Thermally stressable wall and method for sealing gap in thermally stressed wall
10/03/2006US7114920 Shroud and vane segments having edge notches
10/03/2006US7114915 Gas turbine and turbine rotor for a gas turbine
10/03/2006US7114914 Device for controlling clearance in a gas turbine
10/03/2006US7114912 Fan blade with embrittled tip
10/03/2006US7114519 Normally open reverse flow flapper valve
10/03/2006US7114339 Cavity on-board injection for leakage flows
10/03/2006US7114336 Flow pulsing valve and fuel supply system for a turbine engine incorporating same
10/03/2006US7114322 Gas-turbine power generating installation and method of operating the same
10/03/2006US7114321 Thermal isolation device for liquid fuel components
09/2006
09/29/2006CA2541127A1 Turbojet rear suspension
09/28/2006WO2006100983A1 Gas turbine combustor and its ignition method
09/28/2006WO2006100342A1 Method of operating a gas engine plant and fuel feeding system of a gas engine
09/28/2006US20060213726 Rotating shaft scavenging scoop
09/28/2006US20060213183 Power plant and operating method
09/28/2006DE102005013421A1 Intake cone for turbofan gas turbine engine, has attachment portion having axial contact surface abutted to one of guard rings as such that diagonal bolt hole can be bored into both guard ring and contact surface
09/27/2006EP1705393A1 Bearing device for turbocharger
09/27/2006EP1705343A2 Low leakage finger seal
09/27/2006EP1704313A1 Method for operating a power plant
09/27/2006EP1704312A1 Method for operating an atomiser in a gas turbine group
09/27/2006EP1040261B1 Nozzles for water injection in a turbine engine
09/27/2006CN1837591A Fuel injector bearing plate assembly and swirler assembly
09/27/2006CN1837590A Link device between an enclosure for passing cooling air and a stator nozzle in a turbomachine
09/27/2006CN1837589A Link device between an enclosure for passing cooling air and a stator nozzle in a turbomachine
09/26/2006US7112040 Method of guiding a blade having a variable pitch angle
09/26/2006US7111463 Combustion wave ignition for combustors
09/26/2006US7111462 Onboard supplemental power system at varying high altitudes
09/26/2006CA2168631C Sealing device between an air inlet and a fan frame of a turbofan engine
09/21/2006WO2006096982A1 Modular fuel nozzle and method of making
09/21/2006WO2006085920A3 Pneumatic valve control using downstream pressure feedback and an air turbine starter incorporating the same
09/21/2006US20060210390 Film cooling for microcircuits
09/21/2006US20060207263 Combustion chamber
09/21/2006US20060207260 Gas-turbine power generating installation and method of operating the same
09/21/2006US20060207259 Acoustic damper
09/21/2006US20060207254 Compact lightweight turbine
09/21/2006CA2533045A1 Fuel injection bearing plate assembly and swirler assembly
09/20/2006EP1703102A2 Liquefied natural gas power plant and operation method thereof
09/20/2006EP1703085A2 A multi-shaft arrangement for a turbine engine
09/20/2006EP1423595A4 Combustion turbine fuel inlet temperature management for maximum power output
09/20/2006CN2818818Y Miniature primary surface heat regenerator of gas turbine
09/20/2006CN1836109A Control device for compressor
09/20/2006CN1836098A Cogeneration system
09/20/2006CN1834431A Method and apparatus for cooling gas turbine fuel nozzles
09/19/2006US7108479 Methods and apparatus for supplying cooling fluid to turbine nozzles
09/19/2006US7108477 Warning before pump limit or in case of blade failure on a turbomachine
09/19/2006US7107774 Method and apparatus for combined cycle power plant operation
09/19/2006US7107773 Turbine engine sequenced combustion
09/19/2006CA2224877C Non-polluting, open brayton cycle automotive power unit
09/14/2006WO2006095799A1 Surface treatment method and repair method
09/14/2006WO2006095767A1 Jig
09/14/2006WO2006094391A1 Method and apparatus for utilising fugitive gases as a supplementary fuel source
09/14/2006US20060201257 Turbine blade fatigue life evaluating method
09/14/2006US20060201160 Multi-shaft arrangement for a turbine engine
09/14/2006US20060201132 Gas turbine control system
09/14/2006US20060201131 Turbine exhaust water recovery system
09/14/2006DE19545311B4 Verfahren zur Betrieb einer mit Vormischbrennern bestückten Brennkammer Method for operating a lamp equipped with premix combustion chamber
09/14/2006CA2601027A1 Method and apparatus for utilising fugitive gases as a supplementary fuel source
09/13/2006EP1701028A2 Acoustic liner with a nonuniform depth backwall
09/13/2006EP1701019A1 Two-spool turbomachine with driving module on low pressure and high pressure rotors, driving module for the turbomachine and turbomachine assembly method
09/13/2006EP1701018A1 Air turbine starter enhancement for clearance seal utilization
09/13/2006EP1701017A1 Variable arc gap plasma igniter element
09/13/2006EP1701016A1 Acoustic liner with nonuniform impedance
09/13/2006EP1700018A1 High accuracy fuel metering system for turbine engines