| 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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| 08/04/2011 | DE102011000144A1 Prozess und System zum Erzeugen geformter Luftlöcher Process and system for producing molded air holes |
| 08/04/2011 | DE102010016902A1 Turbinenbrennstoffdüse mit Vormischer mit Zusatzleitschaufel Turbinenbrennstoffdüse with pre-mixer with Zusatzleitschaufel |
| 08/04/2011 | DE102010001414A1 Method for repairing labyrinth-sealing strips made of nickel-base-material consists of components of a gas turbine engine, comprises completely separating the upper worn components of the sealing strips |
| 08/04/2011 | DE102010001413A1 Method for repairing labyrinth-sealing strips made of nickel base alloy consists of components of a gas turbine engine, comprises completely separating the upper worn components of the sealing strips |
| 08/04/2011 | CA2730852A1 Brake mechanism for air turbine starter |
| 08/03/2011 | EP2351915A1 Combined cycle power plant and method of operating such power plant |
| 08/03/2011 | EP2350503A1 Hydrodynamic circumferential seal system for large translations |
| 08/03/2011 | EP2350445A2 Method and system for altering engine air intake geometry |
| 08/03/2011 | EP2350444A1 Gas turbine engine accessory system |
| 08/03/2011 | EP2349694A2 Perforated composite structures and methods therefore |
| 08/03/2011 | CN201916074U 喷气轮发动机 Jet turbine engine |
| 08/03/2011 | CN102144100A Compressor casing resistant to titanium fire, high pressure compressor including such a casing, and aircraft engine including such a compressor |
| 08/03/2011 | CN102143889A Method for making an acoustic panel for the air intake lip of a nacelle |
| 08/03/2011 | CN102143888A Method for making a nacelle de-icing element |
| 08/03/2011 | CN102140965A Fuel heater system including hot and warm water sources |
| 08/03/2011 | CN102140964A Structure for improving cooling efficiency of gas film of discrete hole |
| 08/03/2011 | CN101078368B Method for gas turbine operation during under-frequency operation through use of air extraction |
| 08/02/2011 | US7987678 Hot gas duct and duct splitter arrangement |
| 08/02/2011 | US7987660 Gas turbine, method of controlling air supply and computer program product for controlling air supply |
| 08/02/2011 | CA2672457C Heat shield sealing for gas turbine engine combustor |
| 08/02/2011 | CA2431574C Metallic material susceptible to wear by abrasion; parts, housing; procedure for fabricating such material |
| 08/01/2011 | CA2729261A1 Axial load damping system for rotor shaft |
| 07/28/2011 | WO2011090561A1 Jet engine shield and deicer |
| 07/28/2011 | WO2011089957A1 Method for repairing wall member with passage |
| 07/28/2011 | WO2011089729A1 Gas turbine control device and gas turbine starting method |
| 07/28/2011 | US20110179805 Rotor containment structure for gas turbine engine |
| 07/28/2011 | US20110179804 Radial turbine engine floating ring seal |
| 07/28/2011 | US20110179803 Bled diffuser fed secondary combustion system for gas turbines |
| 07/28/2011 | US20110179802 System and method for gas turbine startup control |
| 07/28/2011 | US20110179801 Methods and apparatus for diluent nitrogen saturation |
| 07/28/2011 | US20110179800 Method for operating a gas turbine and gas turbine |
| 07/28/2011 | US20110179798 Sealing between a combustion chamber and a turbine nozzle in a turbomachine |
| 07/28/2011 | US20110179797 Burner and method for operating a burner |
| 07/28/2011 | US20110179796 Helmholtz damper for a combustor of a gas turbine and a method for installing the helmholtz damper |
| 07/28/2011 | US20110179795 Injector with integrated resonator |
| 07/28/2011 | DE102011000148A1 System und Verfahren zum Steuern eines Hochfahrvorgangs einer Gasturbine System and method for controlling a start-up operation of a gas turbine |
| 07/28/2011 | DE102010005846A1 Device for e.g. drying hybrid combustion air, supplied to gas turbine, has flow switch provided in secondary circuit, where switch of airflow is provided for switching counter current to direct current between circuit and airflow |
| 07/28/2011 | DE102010005845A1 Device for conditioning of compressed air, particularly wetting, drying, cooling or heating of air, has air conditioning unit that is formed as hybrid heat exchanger and is permeable for air flow |
| 07/28/2011 | DE102010005421A1 Vorrichtung und Verfahren zur Reinigung einer Stirndichtung eines Strahltriebwerks Apparatus and method for cleaning a face seal of a jet engine |
| 07/28/2011 | CA2727815A1 Pressure flush process for cooled turbine blades |
| 07/27/2011 | EP2348211A1 Aircraft propulsion unit with a cooler installed at engine nacelle |
| 07/27/2011 | EP2348210A1 Aircraft propulsion unit with a cooler installed at engine nacelle |
| 07/27/2011 | EP2346736A2 Integrated inlet design |
| 07/27/2011 | CN201908725U Measuring device for total pressure and total temperature of inlet airflow of aircraft engine |
| 07/27/2011 | CN1704573B Apparatus for cooling combustor liner and transition piece of a gas turbine |
| 07/27/2011 | CN102137950A Coating structure and surface treating method |
| 07/27/2011 | CN102135036A Heat exchanger mounting assembly in a gas turbine |
| 07/27/2011 | CN102135035A Aircraft propulsion unit with a cooler installed at engine nacelle |
| 07/27/2011 | CN102135034A Bled diffuser fed secondary combustion system for gas turbines |
| 07/27/2011 | CN101509426B Turbine shaft engine |
| 07/26/2011 | CA2671718C Particle separator and separating method for gas turbine engine |
| 07/26/2011 | CA2603370C Internal fuel manifold and fuel fairing interface |
| 07/26/2011 | CA2444979C Explosive decoupling system for a turbojet nozzle |
| 07/26/2011 | CA2443979C Turbine premixing combustor |
| 07/21/2011 | WO2011086993A1 Seal structure and gas turbine engine provided therewith |
| 07/21/2011 | WO2011086962A1 Insert removal device for gas turbine stationary blade and insert removal method for gas turbine stationary blade |
| 07/21/2011 | WO2011046580A3 Bird deflector and air replacement system |
| 07/21/2011 | US20110173990 Intermediate casing for a gas-turbine engine |
| 07/21/2011 | US20110173989 Combined cycle power plant with split compressor |
| 07/21/2011 | US20110173986 Adaptive Gas Turbine Vane Separator System and Method |
| 07/21/2011 | US20110173983 Premix fuel nozzle internal flow path enhancement |
| 07/21/2011 | US20110173982 Gas turbine engine fuel conveying member |
| 07/21/2011 | US20110173947 System and method for gas turbine power augmentation |
| 07/21/2011 | DE102010061628A1 System und Verfahren zur Leistungssteigerung von Gasturbinen System and method for performance improvement of gas turbines |
| 07/21/2011 | DE102010061627A1 Luftbypassbandanordnung für ein Gasturbinenübergangsstück Air bypass belt assembly for a gas turbine transition piece |
| 07/21/2011 | DE102010004936A1 Compressor e.g. multistage axial compressor operating method for fluid-flow machine, involves impinging angle of attack of turbo-compressor stages with fluid such that front stages are more heavily loaded in relation to dry operation |
| 07/21/2011 | DE102010001034A1 Entspannungs-Turbine zur Entspannung von Gas Relaxation of gas turbine for expanding |
| 07/21/2011 | DE102006036284B4 Gasturbine Gas turbine |
| 07/21/2011 | CA2786321A1 Sealing arrangement and gas turbine engine with the sealing arrangement |
| 07/20/2011 | EP2345805A1 Inlet air heating and cooling system for the compressor of a gasturbine |
| 07/20/2011 | EP2344738A1 Methods and systems for controlling the products of combustion |
| 07/20/2011 | EP2344383A1 Air intake structure for a turbine engine nacelle |
| 07/20/2011 | CN201902264U Fuel regulation system of heavy combustion engine |
| 07/20/2011 | CN1740523B Turbo machine with axial retention means for the rotor |
| 07/20/2011 | CN102132010A Fixed vane assembly for turbine engine having reduced weight, and turbine engine including at least one such fixed vane assembly |
| 07/20/2011 | CN102128086A Ejector-OBB Scheme for a Gas Turbine |
| 07/20/2011 | CN102128085A System and method for gas turbine power augmentation |
| 07/20/2011 | CN102128084A Thermal power device for turbine fan engine |
| 07/20/2011 | CN102128058A Adaptive gas turbine vane separator system and method |
| 07/20/2011 | CN101479455B Turboreactor for aircraft |
| 07/20/2011 | CN101273191B Two-shackle aircraft engine rear attachment and aircraft engine assembly |
| 07/19/2011 | US7980056 Methods and apparatus for controlling air flow within a pulse detonation engine |
| 07/19/2011 | US7980055 Gas turbine exhaust diffuser |
| 07/19/2011 | CA2467846C Method of manufacturing a hollow blade for a turbine engine |
| 07/14/2011 | WO2011084941A2 Dual-pump supply system with by-pass-controlled flow regulator |
| 07/14/2011 | WO2011084551A2 Gas turbine generator |
| 07/14/2011 | WO2011083628A1 Gas turbine |
| 07/14/2011 | WO2011083137A1 Contra-rotating propeller system for an aircraft turbine engine |
| 07/14/2011 | WO2011082949A2 Combined cycle power plant and method of operating such power plant |
| 07/14/2011 | WO2011059587A3 Valve sequencing system and method for controlling turbomachine acoustic signature |
| 07/14/2011 | WO2011041049A3 Internally nested variable-area fuel nozzle |
| 07/14/2011 | US20110171019 Locking device comprising a telescopic connecting rod equipped with return means |
| 07/14/2011 | US20110168839 Device for connecting an air inlet with an aircraft nacelle actuator assembly |
| 07/14/2011 | US20110167832 Method for operating a premix burner, and a premix burner for carving out the method |
| 07/14/2011 | US20110167830 Vibration damper |
| 07/14/2011 | US20110167829 Fuel control arrangements |
| 07/14/2011 | US20110167828 Combustor assembly for a turbine engine that mixes combustion products with purge air |
| 07/14/2011 | US20110167783 Gas turbine device |
| 07/14/2011 | US20110167781 Turbomachine nacelle and anti-icing system and method therefor |
| 07/14/2011 | DE102010061638A1 Flügelschalldämpfer im Bogenstück für eine Gasturbine Wing silencer in the elbow for a gas turbine |