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)
05/2014
05/20/2014US8727702 Hoop snap spacer
05/20/2014US8726675 Scalloped flexure ring
05/20/2014US8726674 Propulsion unit
05/20/2014US8726665 Internal mixing of a portion of fan exhaust flow and full core exhaust flow in aircraft turbofan engines
05/20/2014US8726663 Combined cycle system employing phase change material
05/20/2014US8726631 Dual walled combustors with impingement cooled igniters
05/20/2014US8726629 Compressed air energy system integrated with gas turbine
05/20/2014US8726627 Gas turbine equipment utilizing high humidity
05/20/2014US8726626 Combustor for a gas turbine engine
05/20/2014US8726609 Modular turbine enclosure
05/20/2014DE202013005524U1 Vorrichtung zum Reinigen der Core Engine eines Strahltriebwerks Device for cleaning the core engine of a jet engine
05/20/2014CA2799933C Method and device for implementing a fitness monitor for a turbine engine in an aircraft equipped with at least one turbine engine
05/20/2014CA2754703C Turbine engine support arms
05/20/2014CA2602172C Blowing conduit for a turbine engine
05/20/2014CA2557104C Process for assembling a turbine engine
05/20/2014CA2554933C Sealing system for the rear lubrication chamber of a turbojet
05/20/2014CA2504173C Methods and apparatus for assembling a bearing assembly
05/15/2014WO2014074792A1 Split intermediate case
05/15/2014WO2014074617A2 Actuated bypass hood for gas turbine air inlet system and methods
05/15/2014WO2014074371A1 System for providing fuel to a combustor assembly in a gas turbine engine
05/15/2014WO2014074262A2 Local heat treatment and thermal management system for engine components
05/15/2014WO2014074196A2 Singlet vane cluster assembly
05/15/2014WO2014074195A2 Turbine engine support assembly including self anti-rotating bushing
05/15/2014WO2014073732A1 Dual swirling flow combustion device for gas turbine
05/15/2014WO2014072842A1 Reducing the load consumed by gas turbine compressor and maximizing turbine mass flow
05/15/2014WO2014072652A1 Method for monitoring an ignition sequence of a turbomachine engine
05/15/2014WO2014072643A2 Air exhaust tube holder in a turbomachine
05/15/2014WO2014072626A2 Air exhaust tube holder in a turbomachine
05/15/2014WO2014072575A1 Cooling arrangement for a gas turbine
05/15/2014WO2014072433A1 Gas turbine in mechanical drive applications and operating methods
05/15/2014WO2014035517A3 Gas turbine engine turbine vane platform core
05/15/2014WO2014028085A3 Fundamental gear system architecture
05/15/2014WO2014021981A3 Vortex generators for improved film effectiveness
05/15/2014US20140133967 Split intermediate case
05/15/2014US20140133964 Acoustic structure with internal thermal regulators
05/15/2014US20140133958 Flexible Support Structure For A Geared Architecture Gas Turbine Engine
05/15/2014US20140130889 Air inlet structure for turbojet engine nacelle
05/15/2014US20140130508 Powerplant and related control system and method
05/15/2014US20140130505 Cross-fire tube purging arrangement and method of purging a cross-fire tube
05/15/2014US20140130502 Gas turbine assembly and method therefor
05/15/2014US20140130478 Gas turbomachine including a fuel pre-heat system
05/15/2014US20140130477 Turbomachine and staged combustion system of a turbomachine
05/15/2014US20140130468 Filter assembly, and pre-filter device and pre-filter mounting plate therefor
05/15/2014DE112004001587B4 Kraftwerksanlage und Verfahren zum Betrieb Power plant and method of operation
05/15/2014DE102013112410A1 Drehdichtungsanordnung und Verfahren zur Abdichtung eines drehenden Bauteils in einem Gehäuse Rotary seal assembly and method for sealing a rotating member in a housing
05/15/2014DE102012220641A1 Cooling circuit for reactor core in nuclear power plant, has a first device coupled thermal conductively to a second device such that temperature difference is present between devices during movement of drive for moving cooling medium
05/15/2014DE102012017314A1 System for increasing efficiency of two-stage or multi-stage compressor assembly for compression of process gas, circulates cooling agent to absorption-type refrigeration machine and intercooler
05/14/2014EP2730768A1 Gas turbine arrangement for a locomotive
05/14/2014EP2730767A2 Systems and methods for active component life management for gas turbine engines
05/14/2014EP2730766A1 Heat exchange arrangement for a gas turbine
05/14/2014EP2730749A2 Apparatus and method for measuring gas flow through a rotary seal
05/14/2014EP2729687A1 Gas turbine auxiliaries relay gearbox incorporating uncoupling means
05/14/2014EP2729686A1 Cooling for a fluid flow machine
05/14/2014EP2729668A1 Turbine engine drive shaft device
05/14/2014CN203594516U 自适应对接与自动分离发动机起动气源的装置 Automatic separation of the adaptive engine start docking gas source means
05/14/2014CN203594515U 燃机电厂余热锅炉中压给水梯级利用加热天然气系统 Gas turbine power plant waste heat boiler feed water pressure cascade utilization of natural gas heating system
05/14/2014CN203594514U 一种地面燃气轮机燃气发生器机匣支撑结构 A floor the gas generator turbine casing support structure
05/14/2014CN103797229A 用于调整超音速进气道的方法 A method for adjusting the supersonic inlet
05/14/2014CN103790712A 热气区段布置 Hot zone arrangement
05/14/2014CN103790711A 一种滑油分配装置 One kind of oil dispensing device
05/14/2014CN103790710A 一种火箭基组合循环发动机变结构进气道 Rocket based combined cycle engine intake variable structure
05/14/2014CN103790709A 涡轮轮盘 Turbo Roulette
05/14/2014CN102828832B 一种提高定几何二元混压式进气道起动能力的方法 A method for a given geometry binary mixed compression inlet ability to start improving
05/14/2014CN102575581B 燃气轮机静叶片的插入件去除装置及燃气轮机静叶片的插入件去除方法 A gas turbine stationary blade removal insert device and the gas turbine stationary blade insert removal method
05/14/2014CN102444476B 一种燃气轮机波浪形扩压器 A gas turbine diffuser wavy
05/14/2014CN102395772B 设置有轴间轴承的双主体气体涡轮引擎 Is provided between the main shaft bearing twin gas turbine engine
05/14/2014CN102301122B 用于飞行器发动机机舱的声衰减板 For aircraft engine nacelle acoustic attenuation plate
05/14/2014CN102084105B 具有CO<sub>2</sub>封存能力的热力发电设备 With a CO <sub> 2 </ sub> sequestration capacity thermal power generation equipment
05/13/2014US8725384 Detection system and method to detect flame holding event
05/13/2014US8720204 Resonator system with enhanced combustor liner cooling
05/13/2014US8720179 Power plant including an exhaust gas recirculation system for injecting recirculated exhaust gases in the fuel and compressed air of a gas turbine engine
05/13/2014CA2697741C Combined acoustic absorber and heat exchanging outlet guide vanes
05/13/2014CA2641614C Adhesive bonded attachment assembly for an insulation blanket
05/13/2014CA2569948C Auxiliary machine drive system for a turbine engine with a double body
05/13/2014CA2517772C High thrust gas turbine engine having improved core system
05/13/2014CA2507977C Method and apparatus for operating an intercooler for a gas turbine engine
05/08/2014WO2014071121A1 System and method for a turbine combustor
05/08/2014WO2014071118A1 System and method for reheat in gas turbine with exhaust gas recirculation
05/08/2014WO2014071088A1 System and method for protecting components in a gas turbine engine with exhaust gas recirculation
05/08/2014WO2014071037A2 System and method for oxidant compression in a stoichiometric exhaust gas recirculation gas turbine system
05/08/2014WO2014070882A1 In-situ pressure enhanced processing of composite articles
05/08/2014WO2014070849A1 Bore cavity thermal conditioning system
05/08/2014WO2014070817A1 Blade outer air seal
05/08/2014WO2014070698A1 Turbine rotor assembly
05/08/2014WO2014070695A1 Damper for a turbine rotor assembly
05/08/2014WO2014070691A1 Gas turbine engine with bearing compartment wall cooling
05/08/2014WO2014070436A2 Temperature control within a cavity of a turbine engine
05/08/2014WO2014069286A1 Securing part structure of turbine nozzle and turbine using same
05/08/2014WO2014068261A1 Turbomachine casing
05/08/2014WO2014035513A3 Igniter for a turbomachine and mounting assembly therefore
05/08/2014WO2014035512A3 Non-interrupted turbomachine fluid supply
05/08/2014WO2014031205A3 Seal land for static structure of a gas turbine engine
05/08/2014WO2014031198A3 Variable blade outer air seal
05/08/2014WO2014031194A3 Direct feed auxiliary oil system for geared turbofan engine
05/08/2014WO2014021982A3 Turbomachinery component cooling scheme
05/08/2014US20140127008 Transition duct having airfoil and hot gas path assembly for turbomachine
05/08/2014US20140127001 Gas-turbine engine with a telescopic air inlet in the engine lining
05/08/2014US20140127000 Gas turbine accessory gearbox incorporating decoupling means
05/08/2014US20140126993 Device and a method for measuring the times of passage of blade tips in a turbine engine
05/08/2014US20140126992 Turbine engine comprising a floating bearing for guiding a shaft of the turbine engine
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