| 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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| 02/26/2015 | US20150052897 Method of recovering energy in a steam-cooled gas turbine |
| 02/26/2015 | US20150052873 Torque connector lubrication scuppers |
| 02/26/2015 | DE112013002712T5 Turbinendämpfer Turbine damper |
| 02/26/2015 | DE112013002453T5 Verdichterabdeckung für Turbolader Compressor cover for turbochargers |
| 02/26/2015 | DE102013216930A1 Lagereinheit eines Turboladers sowie Herstellungsverfahren einer Lagereinheit eines Turboladers Bearing unit of a turbocharger and manufacturing method of a storage unit of a turbocharger |
| 02/26/2015 | DE102013216687A1 Lagereinheit eines Turboladers sowie Verfahren zur Montage einer Lagereinheit eines Turbolader Bearing assembly of a turbocharger, as well as method for assembling a bearing assembly of a turbocharger |
| 02/26/2015 | DE102013214933A1 Verfahren zum Montieren einer Gasturbinenschaufel in einer zugeordneten Aufnahme eines Rotorgrundkörpers A method of assembling a gas turbine blade in an associated receiving a rotor base body |
| 02/26/2015 | DE102013109222A1 Vorrichtung für einen Turbolader Device for a turbocharger |
| 02/26/2015 | CA2859416A1 Aircraft engine constant frequency starter/generator |
| 02/25/2015 | EP2839136A1 Micro gas turbine system having an annular recuperator |
| 02/25/2015 | EP2839135A1 Micro gas turbine system with a pipe-shaped recuperator |
| 02/24/2015 | US8963391 Decoupler shaft for high speed generator |
| 02/24/2015 | US8961634 Filter systems for air intakes of aircraft engines and related methods |
| 02/24/2015 | US8961120 System and method of expanding a fluid in a hermetically-sealed casing |
| 02/24/2015 | US8961118 Structural cooling fluid tube for supporting a turbine component and supplying cooling fluid |
| 02/24/2015 | US8961114 Integrated variable geometry flow restrictor and heat exchanger |
| 02/24/2015 | US8961113 Turbomachine geared architecture support assembly |
| 02/24/2015 | US8960597 Propulsion unit for an aircraft and air intake structure for such a unit |
| 02/24/2015 | US8960589 Panel for an air intake of an aircraft nacelle that ensures optimized acoustic treatment and frost treatment |
| 02/24/2015 | US8959928 Positioning arrangement for components of a pressure vessel and method |
| 02/24/2015 | US8959925 Combustor recovery method and system |
| 02/24/2015 | US8959920 Aircraft engine fuel pump bearing flow and associated system and method |
| 02/24/2015 | US8959919 Gas turbine combustor |
| 02/24/2015 | US8959888 Device to lower NOx in a gas turbine engine combustion system |
| 02/24/2015 | US8959887 System and method for high efficiency power generation using a carbon dioxide circulating working fluid |
| 02/24/2015 | US8959768 Method for making deicing system on a nacelle panel |
| 02/24/2015 | CA2832155C Aircraft engine |
| 02/24/2015 | CA2604272C Heat shield for fuel manifold |
| 02/24/2015 | CA2598259C Simple axial retention feature for abradable members |
| 02/19/2015 | WO2015023863A1 Cooled fuel injector system for a gas turbine engine |
| 02/19/2015 | WO2015023764A1 Gas turbine engine combustor bulkhead assembly |
| 02/19/2015 | WO2015023576A1 Protective panel and frame therefor |
| 02/19/2015 | WO2015023471A1 Flow vortex spoiler |
| 02/19/2015 | WO2015023412A1 Noise absorbing structure comprising a honeycomb with an internal septum |
| 02/19/2015 | WO2015023342A2 Gas turbine engine with dove-tailed tobi vane |
| 02/19/2015 | WO2015023338A2 Gas turbine engine component having trip strips |
| 02/19/2015 | WO2015023334A2 Spline ring for a fan drive gear flexible support |
| 02/19/2015 | WO2015023324A2 Stator vane platform with flanges |
| 02/19/2015 | WO2015023322A2 Method for detecting a compromised component |
| 02/19/2015 | WO2015023321A2 Radial position control of case supported structure with axial reaction member |
| 02/19/2015 | WO2015022786A1 Gas turbine engine optimization control device |
| 02/19/2015 | WO2015022378A1 Purge system and method for a gas turbine |
| 02/19/2015 | WO2015021522A1 Axial turbomachines with rotary housing and fixed central element |
| 02/19/2015 | US20150050140 Intake arrangement in gas turbine power plant |
| 02/19/2015 | US20150050139 Panel attachment system |
| 02/19/2015 | US20150050131 Turbine housing |
| 02/19/2015 | US20150050127 Air with integral spring for a gas turbine engine exhaust drive |
| 02/19/2015 | US20150048202 Firewall, pylon of aircraft, and aircraft |
| 02/19/2015 | US20150047370 Method for holding an adapter piece on a tubular housing of a turbo engine, and corresponding adapter piece and holding system |
| 02/19/2015 | US20150047367 Composite heat exchanger |
| 02/19/2015 | US20150047365 Sequential combustion with dilution gas mixer |
| 02/19/2015 | US20150047363 High Frequency-Stabilized Combustion in Aircraft Gas Turbines |
| 02/19/2015 | US20150047361 Nozzle with multi-tube fuel passageway for gas turbine engines |
| 02/19/2015 | US20150047359 Axial flow machine cooling system |
| 02/19/2015 | US20150047315 Gas turbine engine flow duct having integrated heat exchanger |
| 02/19/2015 | US20150047314 Intake arrangement in gas turbine power plant |
| 02/19/2015 | DE102014111007A1 Inneres Zylinderelement mit integriertem Diffusor für eine Gasturbomaschine Inner cylindrical element with integrated diffuser for a gas turbine engine |
| 02/19/2015 | DE102013216400A1 Leitschaufel mit einer Borsten umfassenden Dichteinrichtung Vane with a comprehensive bristles sealing device |
| 02/19/2015 | DE102013216060A1 Brennkraftmaschine mit zweiflutiger Radialturbine und gruppierten Zylindern Internal combustion engine with twin-scroll turbine radial and grouped cylinders |
| 02/19/2015 | DE102013213834A1 Verfahren zum Herstellen eines Isolationselements und Isolationselement für ein Gehäuse eines Flugtriebwerks A method for manufacturing an insulation element, and insulation member for a housing of an aircraft engine |
| 02/19/2015 | DE102013013571A1 Abgasturbolader Exhaust gas turbocharger |
| 02/19/2015 | DE102007032933B4 Turbomaschine Turbomachine |
| 02/18/2015 | EP2837860A1 Brush seal |
| 02/18/2015 | EP2837858A1 Brush seal |
| 02/18/2015 | EP2837811A1 A panel attachment system |
| 02/18/2015 | EP2837799A1 Engine fuel control system |
| 02/18/2015 | EP2837798A1 Heated bypass valve for heat exchanger |
| 02/18/2015 | EP2837797A1 Particle separator |
| 02/18/2015 | EP2837796A1 Method for manufacturing coupled turbine blades, and coupled turbine blades |
| 02/18/2015 | EP2837795A1 Improved intake arrangement in gas turbine power plant |
| 02/18/2015 | EP2837794A1 Improved intake arrangement in gas turbine power plant |
| 02/18/2015 | EP2837776A1 A panel attachment system |
| 02/18/2015 | EP2836694A1 Gearbox and turbine engine with geared fan |
| 02/18/2015 | EP2836685A1 Device for sealing between the coaxial shafts of a turbomachine |
| 02/18/2015 | EP2836683A2 Tie shaft arrangement for turbomachine |
| 02/17/2015 | US8956106 Adaptive eductor system |
| 02/17/2015 | US8955794 Bleed air systems for use with aircrafts and related methods |
| 02/17/2015 | US8955403 Accessory gearbox device for a jet engine |
| 02/17/2015 | US8955335 System, propulsion system and vehicle |
| 02/17/2015 | US8955334 Systems and methods for controlling the startup of a gas turbine |
| 02/17/2015 | US8955328 Burner arrangement |
| 02/17/2015 | US8955327 Micromixer heat shield |
| 02/17/2015 | US8955324 Combustion arrangement and turbine comprising a damping facility |
| 02/17/2015 | CA2735321C Multi passage fuel manifold and methods of construction |
| 02/17/2015 | CA2647058C Sealing of a hub cavity in the exhaust casing of a turbine engine |
| 02/17/2015 | CA2602311C Method and system to facilitate enhanced local cooling of turbine engines |
| 02/17/2015 | CA2598379C Oil bearing and tube assembly concept |
| 02/17/2015 | CA2594062C Oil strainer for a gas turbine engine |
| 02/16/2015 | CA2859441A1 Particle separator |
| 02/12/2015 | WO2015021247A1 High porosity abradable coating |
| 02/12/2015 | WO2015021222A1 Clearance control assembly |
| 02/12/2015 | WO2015021029A1 Boas with radial load feature |
| 02/12/2015 | WO2015020892A1 Diffuser case mixing chamber for a turbine engine |
| 02/12/2015 | WO2015020806A1 Airfoil trailing edge tip cooling |
| 02/12/2015 | WO2015020775A1 Gas turbine engine aft seal plate geometry |
| 02/12/2015 | WO2015020708A2 Gas turbine rapid response clearance control system with annular piston |
| 02/12/2015 | US20150044030 Long-Duct, Mixed-Flow Nozzle System for a Turbofan Engine |
| 02/12/2015 | US20150044028 Low pressure ratio fan engine having a dimensional relationship between inlet and fan size |
| 02/12/2015 | US20150043851 Tapered oil feed bearing cage |
| 02/12/2015 | US20150042086 Mounting structure of intercooler pipe |