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)
09/2012
09/05/2012CN101694181B Seal structure of gas turbine combustor
09/05/2012CN101611218B Method for demounting blade ring and member for demounting blade ring
09/05/2012CN101280694B Thermal insulation board, bearing casing and turbo casing for exhaust-gas-turbine, and exhaust-gas-turbine
09/05/2012CN101149019B Gas turbine helicopter engine soundproofing device and the resulting engine
09/04/2012US8256222 Direct metering fuel control with integral electrical metering pump and actuator servo pump
09/04/2012DE202012102965U1 Gasturbinenstrahlmotor A gas turbine jet engine
09/04/2012CA2645954C Radial staging method and configuration of a liquid injection system for power plants
09/04/2012CA2629961C Reduced thermal stress assembly and process of making same
08/2012
08/30/2012WO2012114832A1 Gas turbine
08/30/2012WO2012114367A1 Gas turbine system utilizing solar heat
08/30/2012WO2012114029A1 Driveshaft for the gearbox of auxiliary machines of a turbojet engine
08/30/2012WO2012114025A1 Turbomachine comprising a privileged injection device and corresponding injection method
08/30/2012WO2012114024A1 Privileged injection device and method
08/30/2012US20120219415 Metallic annular connection structure for aircraft turbomachine
08/30/2012US20120216549 System, propulsion system and vehicle
08/30/2012US20120216548 Systems and methods involving multiple torque paths for gas turbine engines
08/30/2012US20120216546 Method and device for turbo generator cooling
08/30/2012US20120216544 Swirl reducing gas turbine engine recuperator
08/30/2012US20120216543 Diffusing gas turbine engine recuperator
08/30/2012US20120216506 Gas turbine engine recuperator with floating connection
08/30/2012US20120216505 Aircraft
08/30/2012CA2827014A1 Driveshaft for the gearbox of auxiliary machines of a turbojet engine
08/30/2012CA2826639A1 Turbomachine comprising a privileged injection device and corresponding injection method
08/29/2012EP2492628A1 Swirl reducing gas turbine engine recuperator
08/29/2012EP2492472A1 Diffusing Gas Turbine Engine Recuperator
08/29/2012EP2492471A2 Gas Turbine Engine Recuperator with Floating Connection
08/29/2012EP2492455A2 A gas turbine joint assembly
08/29/2012EP2492451A2 Low pressure spool emergency generator
08/29/2012EP2491310A1 A method of operating a multi-fuel combustion system
08/29/2012CN202402166U Low-entropy multifuel fired cycle thermal power system
08/29/2012CN202402140U Gas turbine module with fire control, heat insulation, ventilation and sound insulation functions
08/29/2012CN202402139U Inter-shaft sealing device
08/29/2012CN102650237A Joint assembly
08/29/2012CN102650236A Sealing device and method for providing a seal in a turbine system
08/29/2012CN102650235A Gas turbine intercooler with tri-lateral flash cycle
08/29/2012CN102650221A Explosion-welded gas turbine shroud and a process of forming an explosion-welded gas turbine
08/29/2012CN101878395B Combustion burner
08/28/2012CA2768905A1 Swirl reducing gas turbine engine recuperator
08/28/2012CA2768884A1 Diffusing gas turbine engine recuperator
08/28/2012CA2767702A1 Rotor centralization for turbine engine assembly
08/28/2012CA2767685A1 Gas turbine engine recuperator with floating connection
08/28/2012CA2475145C Lightened interblade platform for a turbojet blade support disk
08/25/2012CA2767488A1 A joint assembly
08/23/2012WO2012112889A2 Fluid flow devices with vertically simple geometry and methods of making the same
08/23/2012WO2012112514A1 Radiation shield for a gas turbine combustor
08/23/2012US20120213628 Gas turbine engine with geared architecture
08/23/2012US20120210729 Method and apparatus for mounting transition piece in combustor
08/23/2012US20120210728 Fluid Flow Devices with Vertically Simple Geometry and Methods of Making the Same
08/23/2012US20120210724 Method of matching thermal response rates between a stator and a rotor and fluidic thermal switch for use therewith
08/23/2012US20120210723 Gas turbine generator set
08/23/2012US20120210722 Apparatus, method, and system for separating particles from a fluid stream
08/23/2012US20120210717 Apparatus for injecting fluid into a combustion chamber of a combustor
08/23/2012US20120210716 Pumping Arrangement
08/23/2012US20120210694 Turbo machine spool parameter detection
08/23/2012DE10330829B4 Lageranordnung für eine Gasturbine Bearing assembly for a gas turbine
08/23/2012CA2830001A1 Radiation shield for a gas turbine combustor
08/22/2012EP2489858A2 Gas turbine engine generator system with torsional damping coupling
08/22/2012EP2489857A2 Pumping arrangement
08/22/2012EP2489856A2 Micro-perforated acoustic liner
08/22/2012EP2489835A1 Turbine blade
08/22/2012EP2488740A1 Device for filtering the intake air of an internal combustion engine having ventilation means
08/22/2012EP2488739A1 Gas turbine engine air intake in a nacelle
08/22/2012EP2488728A1 Turbine for converting energy and method for operating the same
08/22/2012EP2488727A1 Sealing assembly on a steam turbine housing, comprising a fixable sealing ring
08/22/2012EP2488726A1 Sealing assembly on a steam turbine housing, comprising an adjustable sealing ring
08/22/2012CN102648055A Method and device for gas cleaning
08/22/2012CN102641626A Apparatus, method and system for separating particles from fluid stream
08/22/2012CN101806251B Starting control device of micro gas turbine and starting control method
08/22/2012CN101798961B Two-stage beveled supersonic speed air inlet lip
08/22/2012CN101622433B Blast furnace gas burning facility and its operation method
08/21/2012US8245519 Laser shaped film cooling hole
08/21/2012US8245518 Mid turbine frame system for gas turbine engine
08/21/2012US8245517 Gas turbine starting with stepping speed control
08/21/2012US8245494 Gas turbine engine with eductor and eductor flow distribution shield
08/21/2012US8245493 Power plant and control method
08/21/2012US8245492 Power plant and method of operation
08/21/2012CA2604540C Reduced stress internal manifold heat shield attachment
08/21/2012CA2501349C Formation of corrosion-resistant coatings
08/21/2012CA2495862C Device for indicating a residual power margin of aircraft turbine engines
08/21/2012CA2483043C Labyrinth gasket device for gas turbine engine
08/16/2012WO2012084347A3 Gas turbine and method for oparating said gas turbine
08/16/2012US20120204967 Device For Ventilating A Compartment
08/16/2012US20120204575 Fuel injector mounting system
08/16/2012US20120204574 Gas turbine engine
08/16/2012US20120204572 Method and device for determining the capacity of an aircraft pump to deliver a predetermined fuel output
08/16/2012US20120204571 Combustor and method for introducing a secondary fluid into a fuel nozzle
08/16/2012US20120204569 Apparatus and methods for eliminating cracking in a turbine exhaust shield
08/16/2012US20120204568 Turbine Inlet Air System
08/16/2012US20120204567 Fuel mixing device for turbine engine combustion chamber comprising improved air feed means
08/16/2012US20120204531 High altitude combustion system
08/16/2012DE102011003906A1 Abgasturbolader mit gekühltem Turbinengehäuse und reduziertem Druckverlust Exhaust gas turbocharger with cooled turbine housing and reduced pressure loss
08/16/2012DE102011003905A1 Abgasturbolader mit gekühltem Turbinengehäuse und gekühltem Lagergehäuse und gemeinsamer Kühlmittelzufuhr Exhaust gas turbocharger with cooled turbine housing and cooled bearing housing and common coolant supply
08/16/2012DE102011003901A1 Abgasturbolader mit gekühltem Turbinengehäuse und gekühltem Lagergehäuse und gemeinsamer Kühlmittelzufuhr Exhaust gas turbocharger with cooled turbine housing and cooled bearing housing and common coolant supply
08/15/2012EP2487349A2 Turbine Inlet Air System
08/15/2012EP2487332A1 Turbine
08/15/2012EP2486262A1 Circuit for supplying fuel to an aircraft engine
08/15/2012EP2486261A1 Circuit for supplying fuel to an aircraft engine
08/15/2012EP1567756B1 Method for controlling the injection of liquid into an inflow channel of a prime mover or machine
08/15/2012CN202381173U Low-voltage high-energy electric ignition plug sealing member
08/15/2012CN202381172U Multi-working medium turbine engine
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