Patents
Sitemap › F02 - Combustion engines; Hot-gas or combustion-product engine plants › F02C - Gas-turbine plants; Air intakes for jet-propulsion plants; Controlling fuel supply in air-breathing jet-propulsion plants › F02C 7 - Features, component parts, details or accessories, not provided for in, or of interest apart from, groups; Air intakes for jet-propulsion plants
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
11/04/2010US20100279180 Process for the utilization of ruminant animal methane emissions
11/04/2010US20100276895 Seal arrangement and a method of repairing a seal arrangement
11/04/2010US20100275614 Structural reinforcement strut for gas turbine case
11/04/2010US20100275612 Direct transfer axial tangential onboard injector system (tobi) with self-supporting seal plate
11/04/2010US20100275611 Distributing Fuel Flow in a Reaction Chamber
11/04/2010US20100275608 Systems and Methods for Rapid Turbine Deceleration
11/04/2010US20100275607 Thermal Management Using Topological Isomerization of Fuel
11/04/2010US20100275605 Gas-Turbine Burner
11/04/2010US20100275604 High volume fuel nozzles for a turbine engine
11/04/2010US20100275603 Combustor of gas turbine
11/04/2010US20100275602 Burner for a gas turbine engine
11/04/2010US20100275601 Turbine air flow conditioner
11/04/2010US20100275574 Borescope plug with bristles
11/04/2010US20100275572 Oil line insulation system for mid turbine frame
11/04/2010US20100275404 On-line cleaning of turbine hot gas path deposits via pressure pulsations
11/04/2010DE102010016441A1 Endoskopstopfen mit Borsten Endoscope plug with bristles
11/04/2010DE102010016429A1 Turbinentriebwerk mit Kühlstopfbuchse Turbine engine with cooling gland
11/04/2010DE102009017356A1 Magnetizable axial-thrust bearing disk for turbocharger of internal combustion engine, has rotor shaft, and magnetic bearing arrangement provided with electromagnet device, where thickness and width of disk are variable
11/04/2010CA2760378A1 Method and device for feeding a turbine engine combustion chamber with a controlled fuel flow
11/04/2010CA2702591A1 Bearing support
11/03/2010EP2246544A1 Gas turbine, and interior opening method for the gas turbine
11/03/2010EP2246530A1 Connection structure of exhaust chamber, support structure of turbine, and gas turbine
11/03/2010EP2246526A1 Turbine disc and gas turbine
11/03/2010EP2246525A1 Gas turbin and disc and method for forming radial passage of disc
11/03/2010EP2246106A1 Filter cassette, filter arrangement, and gas turbine with such filter cassette
11/03/2010EP2245285A1 System and method for the reduction of harmful substances in engine exhaust gases
11/03/2010EP2244944A2 Aircraft engine assembly comprising downwardly offset engine mounts on the fan casing
11/03/2010EP2244943A2 Aircraft engine assembly comprising an annular load-transfer structure surrounding the central casing of a turbojet engine
11/03/2010EP2244942A2 Aircraft engine assembly comprising a turbojet engine with reinforcing structures connecting the fan casing to the central casing
11/03/2010EP1893484B1 Anti-icing and de-icing system for aircraft engine pod with resistive mat
11/03/2010EP1828574B1 Close coupled gearbox assembly for a tip turbine engine
11/03/2010EP1588048B1 System and method for generating and sustaining a corona electric discharge for igniting a combustible gaseous mixture
11/03/2010EP1520102B1 Methods for starting a combustion turbine and combustion turbine generator configured to implement same methods
11/03/2010CN101878395A Combustion burner
11/03/2010CN101878359A Heat shield and turbocharger having a heat shield
11/03/2010CN101878317A Alloy material having high-temperature corrosion resistance, heat-shielding coating material, turbine member, and gas turbine
11/03/2010CN101876270A Turbine engine having cooling pin
11/03/2010CN101230801B Regulation of the temperature of hot gas of a gas turbine
11/02/2010US7823392 Turbomachine combustion chamber arrangement having a collar deflector
11/02/2010US7823391 Turbine engine arrangement
11/02/2010US7823375 Infrared suppression system
11/02/2010US7823374 Heat transfer system and method for turbine engine using heat pipes
11/02/2010CA2492530C Evaporative duplex counterheat exchanger
10/2010
10/30/2010CA2701313A1 Oil line insulation system for mid turbine frame
10/28/2010WO2010123415A1 An annular gas turbine housing component and a gas turbine comprising the component
10/28/2010WO2010122122A1 Elbow support for aeronautical equipment
10/28/2010WO2010122120A1 One-piece mounting for aeronautical apparatuses
10/28/2010WO2010075390A3 System for supporting and servicing a gas turbine engine
10/28/2010US20100272557 Gas turbine optical imaging system
10/28/2010US20100270427 Bird collision prevention device for an aircraft
10/28/2010US20100269514 Fluidizable algae-based powdered fuel and methods for making and using same
10/28/2010US20100269508 Combustion burner
10/28/2010US20100269507 Radial lean direct injection burner
10/28/2010US20100269506 Fuel spray apparatus for gas turbine engine
10/28/2010US20100269504 Coating system and method for reducing coking and fuel system fouling
10/28/2010US20100269482 Gas turbine system using high-humidity air
10/28/2010US20100269480 Gas turbine exhaust diffuser
10/28/2010DE112008003529T5 Turbinenleitapparatsegment und Verfahren zur Reparatur eines Turbinenleitapparatsegments Turbine nozzle and method of repairing a turbine nozzle segment
10/28/2010DE102010016442A1 Flanschgekühlte Turbinendüse Flanschgekühlte turbine nozzle
10/28/2010DE102010003706A1 Method for designing of engine geometry of internal combustion engine, involves defining design-constraint for engine geometry, and defining design-target dimension for engine geometry
10/28/2010DE102009018583A1 Verbrennungskraftmaschine sowie Verfahren zum Betreiben einer Verbrennungskraftmaschine Internal combustion engine and method of operating an internal combustion engine
10/28/2010CA2759652A1 Elbow support for aeronautical equipment
10/28/2010CA2759542A1 One-piece mounting for aeronautical apparatuses
10/27/2010EP2243534A1 Filter washing system for gas turbine engines
10/27/2010EP2242916A1 Gas turbine
10/27/2010EP2242915A1 Gas turbine having an improved cooling architecture
10/26/2010US7819224 Assembly for reducing noise in turbofan engines
10/26/2010US7819038 Gear with integral overcouple protection
10/26/2010CA2628350C Method and apparatus for production of a cast component
10/26/2010CA2476803C Heat exchanging wall, gas turbine using the same, and flying body with gas turbine engine
10/26/2010CA2418357C Arrangement for the attachment of distributor sectors supporting vanes around an arc of a circle
10/24/2010CA2701512A1 Load distribution system for gas turbine engine
10/24/2010CA2699938A1 Deflector for a gas turbine strut and vane assembly
10/22/2010CA2696625A1 Vane assembly with removable vanes
10/21/2010WO2010119709A1 Nickel-base single-crystal superalloy and turbine wing using same
10/21/2010WO2010119215A1 Method for detecting an icing condition of or the need for servicing a fuel circuit of a turbine engine
10/21/2010WO2010119115A1 Double-body gas turbine engine provided with an inter-shaft bearing
10/21/2010WO2010084023A4 Device for large-scale media conditioning
10/21/2010US20100263964 Intake silencer for gas turbine
10/21/2010US20100263388 Vapor cooled static turbine hardware
10/21/2010US20100263387 Air Filtration Sampling Point Adaptor
10/21/2010US20100263386 Turbine engine having a liner
10/21/2010US20100263384 Combustor cap with shaped effusion cooling holes
10/21/2010US20100263383 Gas turbine premixer with internal cooling
10/21/2010US20100263381 Premixed combustion burner for gas turbine
10/21/2010US20100263374 Internal combustion engine
10/21/2010US20100263348 Additive injection system for improving thermal stability of jet fuel
10/21/2010DE102005002527B4 Kraftstoffzuführungsdurchgang und Verfahren zu dessen Ausbildung im Zuführungsarm eines Kraftstoff-Injektors Fuel supply passage and method of education in the feed arm of a fuel injector
10/21/2010DE102004057985B4 Gasturbinenverbrennungsvorrichtung A gas turbine combustion apparatus
10/21/2010CA2758867A1 Ni-based single crystal superalloy and turbine blade incorporating the same
10/21/2010CA2758651A1 Method for detecting an icing condition of or the need for servicing a fuel circuit of a turbine engine
10/21/2010CA2758175A1 Double-body gas turbine engine provided with an inter-shaft bearing
10/21/2010CA2700019A1 Flange cooled turbine nozzle
10/20/2010EP2241783A1 Drivetrain and method for driving a mechanical system through this drivetrain
10/20/2010EP2241738A1 Inlet cone made of compound fibre material for a gas turbine engine
10/20/2010EP2241728A2 Apparatus and method for cooling a turbine using heat pipes
10/20/2010EP2241727A1 Method of regenerating gas turbine blade and gas turbine blade regenerating apparatus
10/20/2010EP2240691A1 Engine-driven hydraulic pump
10/20/2010CN201610771U 航空发动机涡轮叶片的零冷气消耗超强度冷却装置 Aeroengine turbine blades consume zero super-strength air-conditioning cooling device
10/20/2010CN1755081B Spark detecting sensor of igniter in gas turbine engine
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