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)
12/2006
12/05/2006US7144218 Anti-rotation lock
12/05/2006US7143585 Turbine power plant, installation process and removal process of the turbine power plant
12/05/2006US7143584 Gas turbine apparatus
12/05/2006US7143581 Gas turbine plant
12/05/2006US7143573 Gas turbine set
12/05/2006US7143572 Gas turbine system comprising closed system of fuel and combustion gas using underground coal layer
12/02/2006CA2548138A1 Methods and apparatus for operating gas turbine engines
11/2006
11/30/2006US20060271311 On-line system and method for processing information relating to the wear of turbine components
11/30/2006US20060269391 Gas turbine engine
11/30/2006US20060266050 Gas turbine disk slots and gas turbine engine using same
11/30/2006US20060266048 Fluid catalytic cracking flue gas utility optimizing system and process
11/30/2006US20060266047 Reduced-weight fuel system for gas turbine engine, gas turbine engine having a reduced-weight fuel system, and method of providing fuel to a gas turbine engine using a reduced-weight fuel system
11/30/2006US20060266045 Protection process and control system for a gas turbine
11/30/2006DE19819267B4 Seitenkanalverdichter Side channel blowers
11/29/2006EP1726879A2 Reduced-weight fuel system for a gas turbine engine, gas turbine engine including such a system, and method of providing fuel to such a gas turbine engine
11/29/2006EP1726804A2 Shroud for an Air Turbine Starter
11/29/2006EP1726803A2 Hydraulic lock for axial motion output device
11/29/2006EP1726788A2 A rotor blade containment assembly for a gas turbine engine
11/29/2006EP1726004A1 Assembly for reducing noise in turbofan engines
11/29/2006EP1725769A1 Apparatus and method for storing thermal energy and generating electricity
11/29/2006EP1725755A1 Internal fuel manifold for gas turbine engine or gas turbine fuel nozzle assembly
11/29/2006EP1478836B1 Gearless electric thrust reverser actuator and actuation system incorporating the same
11/29/2006EP1472447B1 Method for operating a gas turbine group
11/29/2006EP1440223B1 Gas turbine group
11/29/2006EP1438486B1 Device for filtering particles out of a coolant flow in a turbo machine
11/29/2006EP0975435B1 Modular coating fixture
11/29/2006CN1869419A Oil supply and scavenge system
11/29/2006CN1869409A Platform of gas turbine moving blade, a method of forming the moving blade, a sealing plate, and a gas turbine having these elements
11/29/2006CN1287075C Gas turbine state diagnostic method and system
11/28/2006US7140840 Turboshaft engine comprising two elements connected to each other with the interposition of a seal
11/28/2006US7140834 Turbine and a component
11/28/2006US7140240 Electric engine start system with inspection mode
11/28/2006US7140189 Gas turbine floating collar
11/28/2006US7140188 Gas turbine engine with intake air flow control mechanism
11/28/2006US7140186 Method and apparatus for monitoring the performance of a gas turbine system
11/28/2006US7140184 Fuel injection method and apparatus for a combustor
11/28/2006US7140183 Premixed exit ring pilot burner
11/27/2006CA2547486A1 Expansion joint and method of assembling same
11/24/2006CA2546524A1 Thermal imaging method and apparatus
11/23/2006WO2006124800A2 Confocal scanning microscope having optical and scanning systems which provide a handheld imaging head
11/23/2006US20060263204 Sealing arrangement, in particular for the blade segments of gas turbines
11/23/2006US20060260321 Cogeneration method and device using a gas turbine comprising a post-combustion Chamber
11/23/2006US20060260319 NOx ADJUSTMENT METHOD FOR GAS TURBINE COMBUSTORS
11/23/2006US20060260317 Nested channel ducts for nozzle construction and the like
11/23/2006US20060260292 Gas turbine exhaust diffuser
11/23/2006DE19845147B4 Vorrichtung und Verfahren zur Kühlung einer einseitug von Heißgas umgebenen Wand Apparatus and method for cooling a hot gas einseitug surrounding wall
11/23/2006DE102005057995A1 Steuerungsanlage für Brennstoffgaserwärmung und damit ausgerüstete Gasturbinen-Kraftwerkseinrichtung Control system for fuel gas heating and thus equipped gas turbine power generation facility
11/22/2006EP1724455A2 Drive arrangement
11/22/2006EP1724454A1 Fuel supply with bend for a gas turbine
11/22/2006EP1724445A2 Apparatus for scavenging lubricating oil
11/22/2006EP1724444A2 Bypass air metering valve
11/22/2006EP1723328A2 Fuel control on apu's
11/22/2006EP1356235B1 Burner unit and method for operation thereof
11/22/2006EP1253378B1 Gas turbine combustor having bypass passage
11/21/2006US7138183 Environmental barrier coating material and coating structure and ceramic structure using the same
11/21/2006US7137783 Cooled gas turbine blades
11/21/2006US7137782 Turbulator on the underside of a turbine blade tip turn and related method
11/21/2006US7137776 Film cooling for microcircuits
11/21/2006US7137255 Compact swirl augmented afterburners for gas turbine engines
11/21/2006US7137245 High area-ratio inter-turbine duct with inlet blowing
11/21/2006US7137242 Fuel system
11/21/2006US7137241 Transition duct apparatus having reduced pressure loss
11/21/2006CA2416663C Gas turbine combined plant and method of operating the same
11/16/2006WO2006120168A2 Fuel supply for a gas turbine, comprising a deviation zone
11/16/2006US20060259156 Control arrangement
11/16/2006US20060257260 Turbomachine blade, in particular a fan blade, and its method of manufacture
11/16/2006US20060257256 Turbulator on the underside of a turbine blade tip turn and related method
11/16/2006US20060254283 Power plant
11/16/2006US20060254282 Control logic for fuel controls on apus
11/16/2006US20060254281 Mobile gas turbine engine and generator assembly
11/16/2006US20060254279 Method of tuning individual combustion chambers in a turbine based on a combustion chamber stratification index
11/16/2006US20060254250 Drain tube for a low-pressure shaft of a turbomachine
11/16/2006DE102005021781A1 Gas turbine, especially aviation engine, has at least one oscillatory element positioned in region of exhaust duct and is excitable into oscillations in such way that noise radiated from especially low pressure turbine is minimized
11/16/2006DE10102606B4 Kühlung von Gehäusen, Rotor, Schaufeln und/oder Brennern von Turbinen Cooling of housings, rotor blades and / or turbine burners
11/15/2006EP1722071A2 Gas turbine engine air valve assembly and a method for reengineering an engine configuration
11/15/2006EP1115967B1 Fan noise reduction from turbofan engines using adaptive herschel-quincke tubes
11/15/2006CN1864042A Method for efficient nonsynchronous lng production
11/15/2006CN1863703A Annular acoustic panel
11/15/2006CN1861243A Method for suppressing oxidative coke formation in liquid hydrocarbons containing metal
11/15/2006CN1284923C Composite bi-fuel turbine device and its operating method thereof
11/14/2006US7135240 Thermal spray compositions for abradable seals
11/14/2006US7134287 Turbine combustor endcover assembly
11/14/2006US7134286 Gas turbine floating collar arrangement
11/14/2006US7134285 Adiabatic power generating system
11/14/2006US7134284 Modular fuel conditioning system
11/14/2006US7134269 Gas turbine engine
11/14/2006CA2376810C Gas turbine combustor having bypass passage
11/09/2006WO2006119409A2 West compression apparatus and method
11/09/2006WO2006117847A1 Micro gas turbine
11/09/2006US20060249332 Oil supply and scavenge system
11/09/2006US20060248899 Method for producing gas turbines and gas turbine assembly
11/09/2006US20060248897 Method for operating a power plant
11/09/2006US20060248896 Method for operation of a gas turbine group
11/09/2006US20060248893 Method and system for determining lean blow out condition for gas turbine combustion cans
11/09/2006US20060248865 Air/oil separation system and method
11/09/2006DE102006007763A1 Exhaust gas diffuser for gas turbine has an inner guide duct for hot gasses and with a ring shaped exhaust duct with outer cladding
11/09/2006CA2823766A1 Wet compression apparatus and method
11/09/2006CA2606756A1 Wet compression apparatus and method
11/08/2006EP1719890A1 Gas turbine plant
11/08/2006EP1719888A2 Fuel supplying device of a combustion chamber in a turbomachine