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)
11/2010
11/24/2010EP2253807A1 Gas turbine cycle or combined steam-gas cycle for production of power from solid fuels and waste heat
11/24/2010EP2253804A2 System and method of assessing thermal energy levels of a gas turbine engine component
11/24/2010EP2252511A1 Locking system for air intake structure for turbojet engine nacelle
11/24/2010CN201650465U Gas turbine bearing case
11/24/2010CN201650463U Combustion gas turbine
11/24/2010CN201650462U Gas turbine
11/24/2010CN201650376U Single-inlet double-outlet hole structure applied to turbine blade air film cooling technology
11/24/2010CN101893255A One-piece can combustor with heat transfer surface enhancements
11/24/2010CN101893154A Isothermic delivery of a cooling fluid through a passageway
11/24/2010CN101892911A Gas turbine having seal assembly with side plate and seal
11/24/2010CN101892910A Cold-heat compatible aircraft ignition circuit
11/24/2010CN101892909A Turbine fuel nozzle having premixer with auxiliary vane
11/24/2010CN101892908A System and method for cooling a wall of a gas turbine combustor
11/24/2010CN101892907A Combined locking silencer for gas turbine intake duct
11/24/2010CN101892906A Filter retainer for turbine engine
11/24/2010CN101892870A Turbine engine shroud ring
11/24/2010CN101146930B Surface treatment method and repair method
11/23/2010US7840333 Event-driven starter controller
11/23/2010US7837925 Method for laser drilling a component made of a ceramic matrix composite, the method including a step of trepanning and a step of removing slag by enlarging the laser beam, hold obtained by this method, component made of a ceramic matrix composite containing it, and turbojet comprising such a component
11/23/2010US7836703 Reciprocal cooled turbine nozzle
11/23/2010US7836702 Gas turbine combustor exit duct and HP vane interface
11/23/2010US7836675 Supercore sump vent pressure control
11/23/2010US7836596 Turbine engine rotor retaining methods
11/19/2010CA2664559A1 Jet engine protector screen
11/18/2010WO2010110936A3 Variable actuation pressure system for independent pressure control
11/18/2010WO2009151701A3 Gas turbine engine systems with fairing
11/18/2010US20100288890 wing-engine combination, an aircraft, and a wing section of an aircraft comprising an engine bleed-air duct arrangement
11/18/2010US20100287950 Support links with lockable adjustment feature
11/18/2010US20100287949 Fastening Arrangement of a Pipe on a Circumferential Surface
11/18/2010US20100287948 Unloaded speed control for availability improvements to heavy fuel fired gas turbines
11/18/2010US20100287947 Acoustically Tuned Combustion for a Gas Turbine Engine
11/18/2010US20100287946 Lean direct injection atomizer for gas turbine engines
11/18/2010US20100287943 Methods and systems for inducing combustion dynamics
11/18/2010US20100287942 Dry Low NOx Combustion System with Pre-Mixed Direct-Injection Secondary Fuel Nozzle
11/18/2010US20100287940 Burner of a gas turbine
11/18/2010US20100287939 Flameless combustion systems for gas turbine engines
11/18/2010US20100287938 Cross flow vane
11/18/2010US20100287937 Automatic fuel nozzle flame-holding quench
11/18/2010US20100287906 Fiber-optic dynamic sensing modules and methods
11/18/2010DE102010016820A1 Komponentenkühlung durch Dichtungen Component cooling by seals
11/18/2010DE102010016680A1 Unterbrechungsfreie Säuberung eines Turbinenheissgaspfades von Ablagerungen durch Druckstösse Uninterruptible cleaning a turbine hot gas path deposits by pressure surges
11/18/2010DE102010016658A1 Verfahren und Vorrichtung für Turbinenmotoren Method and apparatus for turbine engines
11/17/2010EP2251540A2 Turbofan mounting system
11/17/2010EP2251535A2 A damping assembly
11/17/2010EP2251534A1 Method of operating a gas turbine which uses a compressor station for gaseous fuel
11/17/2010EP2251445A1 Tial-based alloy, process for production of the same, and rotor blade comprising the same
11/17/2010EP2250357A1 Air intake structure for an aircraft nacelle
11/17/2010EP2250348A1 Fastening device for an exhaust-gas turbocharger
11/17/2010CN201635840U Reverse oil-injection type jet engine
11/17/2010CN1676902B Controlled pressure fuel nozzle system
11/17/2010CN101889133A Gas turbine controlling method, and gas turbine power generating apparatus
11/17/2010CN101886575A Availability improvements to heavy fuel fired gas turbines
11/17/2010CN101886557A Component cooling through seals
11/17/2010CN101886552A Coupling for rotary components
11/17/2010CN101268266B Control system and control method of gas turbine
11/16/2010US7832684 Ram air channel for the supply of ambient air in an aircraft
11/16/2010US7832211 Gas turbine combustor and a gas turbine equipped therewith
11/16/2010US7832192 Method for injecting a liquid mist into an intake duct
11/15/2010CA2702901A1 Support links with lockable adjustment feature
11/15/2010CA2702501A1 Turbofan mounting system
11/11/2010WO2010128900A1 Supporting structure for a gas turbine engine
11/11/2010WO2010128896A1 A strut and a gas turbine structure comprising the strut
11/11/2010WO2010128241A2 Electric generator disposed on a rotating turboprop part
11/11/2010WO2010052434A3 System and method for washing and purging the liquid fuel system of a turbine with water
11/11/2010US20100284788 Duct wall for a fan of a gas turbine engine
11/11/2010US20100281881 Gas turbine combustor and fuel manifold mounting arrangement
11/11/2010US20100281879 Multi-source gas turbine cooling
11/11/2010US20100281876 Fuel blanketing by inert gas or less reactive fuel layer to prevent flame holding in premixers
11/11/2010US20100281872 Airblown Syngas Fuel Nozzle With Diluent Openings
11/11/2010US20100281871 Airblown Syngas Fuel Nozzle with Diluent Openings
11/11/2010US20100281870 System and method for heating fuel for a gas turbine
11/11/2010US20100281869 Airblown Syngas Fuel Nozzle With Diluent Openings
11/11/2010US20100281848 Three-point fixing arrangement of ignition electrodes of a burner
11/11/2010US20100281689 Methods and apparatus for fabricating a turbine nozzle assembly
11/11/2010DE202010011921U1 Demontagevorrichtung zur Demontage von Turbinenschaufeln A disassembling apparatus for disassembling turbine blades
11/11/2010DE19924067B4 Verfahren und Vorrichtung zur Aufbereitung von Eintrittsluft für eine Gasturbine Method and apparatus for treating the inlet air for a gas turbine
11/11/2010DE102010016548A1 System und Verfahren zur Brennstofferwärmung für eine Gasturbine System and method for heating fuel for a gas turbine
11/11/2010DE102009020632A1 Verfahren zur Reinheitsprüfung eines Schmiermittelsystems in einem Turbinenbauteil A method for purity testing of a lubricant system in a turbine component
11/10/2010EP2249003A1 Gas turbine and method of opening casing of gas turbine
11/10/2010EP2247906A2 Heat accumulator
11/10/2010EP2247830A1 Turbine comprising a flexible seal and corresponding flexible seal for a gas turbine engine
11/10/2010CN101881453A Airblown syngas fuel nozzle with diluent openings
11/10/2010CN101881452A Airblown syngas fuel nozzle with diluent openings
11/10/2010CN101881451A Airblown syngas fuel nozzle with diluent openings
11/10/2010CN101881220A System and method for heating fuel for gas turbine
11/10/2010CN101881219A Preheating inlet air and reducing outward overflow by external flame heater
11/10/2010CN101881218A On-line cleaning of turbine hot gas path deposits via pressure pulsations
11/10/2010CN101879938A Air-independent submarine-propelling method and device
11/09/2010US7827778 Power plants that utilize gas turbines for power generation and processes for lowering CO2 emissions
11/09/2010CA2449263C Row of long and short chord length and high and low temperature capability turbine airfoils
11/09/2010CA2435559C Tubular sound attenuation part for the engine air intake of an aircraft
11/09/2010CA2435360C Aircraft gas turbine engine with control vanes for counter rotating low pressure turbines
11/09/2010CA2432816C Easy-fit heat screening device for connecting a cooling pipe and a through-hole formed in a nozzle support ring of a gas turbine
11/04/2010WO2010126980A2 Transcritical thermally activated cooling, heating and refrigerating system
11/04/2010WO2010125711A1 Plate-shaped bodies, manufacturing method therefor, gas turbine combustor, and gas turbine
11/04/2010WO2010125273A1 Method and device for feeding a turbine engine combustion chamber with a controlled fuel flow
11/04/2010WO2010124698A1 The silenced aspirator anergy amplified/driven air compressor/turbine
11/04/2010WO2010058356A3 Valves for gas-turbines and multipressure gas-turbines
11/04/2010WO2009113058A3 Method and system for enhancing start of a turbine engine
11/04/2010US20100280731 Systems and methods for controlling fuel flow to a turbine component