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
05/08/2014US20140125066 Micro gas turbine
05/08/2014US20140124297 Pressurized reserve lubrication system for a gas turbine engine
05/08/2014US20140123680 Modular drop-in combustor assembly for industial gas turbine and method for installation
05/08/2014US20140123679 Flexible heat shield for a gas turbine engine
05/08/2014US20140123676 Gas turbine engine end-wall component
05/08/2014US20140123675 Air injection system in a gas turbine engine
05/08/2014US20140123674 Inlet Bleed Heat System with Integrated Air Knife/Silencer Panels
05/08/2014US20140123673 A method of starting a turbomachine while reducing thermal unbalance
05/08/2014US20140123669 System and method for diffusion combustion with oxidant-diluent mixing in a stoichiometric exhaust gas recirculation gas turbine system
05/08/2014US20140123668 System and method for diffusion combustion with fuel-diluent mixing in a stoichiometric exhaust gas recirculation gas turbine system
05/08/2014US20140123658 System for Reducing Vibrational Motion in a Gas Turbine System
05/08/2014US20140123657 External cooling fluid injection system in a gas turbine engine
05/08/2014US20140123656 Modular drop-in transition assembly for industrial gas turbine and method for installation
05/08/2014US20140123654 Fuel metering valve system
05/08/2014US20140123653 Enhancement for fuel injector
05/08/2014US20140123651 System for providing fuel to a combustor assembly in a gas turbine engine
05/08/2014US20140123650 Micro-mixer nozzle
05/08/2014US20140123649 Acoustic damping system for a combustor of a gas turbine engine
05/08/2014US20140123623 Gas turbomachine system including an inlet chiller condensate recovery system
05/08/2014US20140123621 Actuated bypass hood for gas turbine air inlet system and methods
05/08/2014DE102013222067A1 Ölablenker Ölablenker
05/08/2014DE102013112159A1 Brennstoffdosierungs-Ventilsystem Fuel metering valve system
05/08/2014DE102013111874A1 Manufacturing method of component for gas turbine engine involves forming grooves, each with cross-sectional are in predetermined ranged with respect to area derived from product of width of opening and depth of re-entrant shaped groove
05/08/2014DE102013111872A1 Einführleitdüsen Einführleitdüsen
05/08/2014DE102013111810A1 Schalldämpfendes Schornsteinelement für ein Turbomaschinensystem The acoustic damping element chimney for a turbo machine system
05/08/2014DE102012211950A1 Abgasturbine Exhaust gas turbine
05/07/2014EP2728145A2 Systems and methods for generating a predictable load upon completion of a start sequence of a turbine
05/07/2014EP2728144A2 Recuperator for gas turbine engine
05/07/2014EP2728143A2 Inlet bleed heat system with integrated air knife/siliencer panels
05/07/2014EP2728141A2 An electrical generation arrangement for an aircraft
05/07/2014EP2727102A1 Acoustic panel and associated assembly method
05/07/2014EP2726785A1 Bypass steam line
05/07/2014EP2726713A1 Improved housing for the accessory relay of a gas turbine
05/07/2014CN203584579U 改善燃气-蒸汽联合循环机组高温环境下出力的装置 Improve gas - steam combined cycle unit at a high temperature environment output device
05/07/2014CN203584578U 一种燃机防冰冻装置的循环加热系统 Hydronic heating system for internal combustion engine anti-freeze device
05/07/2014CN203584577U 一种压气机与涡轮的连接结构 Connection structure of a compressor and the turbine
05/07/2014CN103782064A 利用黏弹性补片减振的小齿轮 Use of viscoelastic damping patches pinion
05/07/2014CN103782012A 燃料歧管冷却流再循环 Fuel manifold cooling flow recirculation
05/07/2014CN103782011A 用于流体机械的冷却装置 Means for cooling the fluid machine
05/07/2014CN103775215A 操作具有顺序燃烧的燃气涡轮的方法及燃气涡轮 Method of operating a gas turbine having sequential combustion gas turbine and
05/07/2014CN103775214A 燃机吹扫管线监控装置 Gas Turbine purge line monitoring device
05/07/2014CN103775213A 燃烧器过渡件 Combustor transition piece
05/07/2014CN103775212A 一种航空发动机的风扇失效制动装置 Aeroengine fan brake failure
05/07/2014CN103775211A 一种主动调控型燃气轮机分布式冷热电联供系统 An active-control-type gas turbine distributed CCHP system
05/07/2014CN103775209A 增压叶轮发动机 Supercharged engine impeller
05/07/2014CN102400786B 油漆膜减轻系统 The paint film to reduce the system
05/07/2014CN102301107B 燃烧器结构部件的制造方法、燃烧器结构部件、燃气轮机用燃烧器及燃气轮机 The method of manufacturing the structural component burner, the burner structural components, the gas turbine and a gas turbine burner
05/07/2014CN102235266B 排气消声器对流冷却 Convection cooled exhaust muffler
05/07/2014CN102177326B 控制燃烧产物的方法与装置 Control method and apparatus for combustion products
05/07/2014CN102042088B 湿气分离系统和组装该系统的方法 Moisture separation system and method for assembling the system,
05/07/2014CN102042045B 具有阻挡件的护罩组件 A barrier member having a shield assembly
05/07/2014CN101769203B 与用于涡轮发动机的导流器有关的方法、系统和/或装置 Methods and deflector for a turbine engine related systems and / or devices
05/07/2014CN101321940B 燃气涡轮发动机的辅助部件安装 An auxiliary gas turbine engine component mounting
05/06/2014US8714906 Method and apparatus for gas turbine engine temperature management
05/06/2014US8713908 Fuel injector arrangement having an igniter
05/02/2014CA2832076A1 System and method of protecting an engine and other aircraft components from damage that may otherwise occur from a fuel control unit failure
05/01/2014WO2014066566A1 Gas turbine engine rotor drain feature
05/01/2014WO2014066210A1 Gas turbine engine variable bleed valve for ice extraction
05/01/2014WO2014066199A1 Reduction of equally spaced turbine nozzle vane excitation
05/01/2014WO2014065281A1 Cylindrical case and process for producing cylindrical case
05/01/2014WO2014065280A1 Cylindrical case and method for manufacturing cylindrical case
05/01/2014WO2014065185A1 Sunlight-utilizing gas turbine power generation system provided with hydrogen-generating unit
05/01/2014WO2014064390A1 Power take-off gearbox on a turbomachine, consisting of an assembled housing
05/01/2014WO2014028090A3 Blade outer air seal for a gas turbine engine
05/01/2014WO2014028082A3 Shield slot on side of load slot in gas turbine engine rotor
05/01/2014WO2014018142A3 Gas turbine engine with high speed low pressure turbine section and bearing support features
05/01/2014US20140119891 Turboshaft engines having improved inlet particle scavenge systems and methods for the manufacture thereof
05/01/2014US20140116066 Combustor cap assembly
05/01/2014US20140116065 Turbine nozzle guide in a turbine enging
05/01/2014US20140116064 Ventilation of an accessory gear box, and turbojet engine comprising such a gear box
05/01/2014US20140116061 Coupling element for torque transmission in a gas turbine engine
05/01/2014US20140116060 Combustor and a method for cooling the combustor
05/01/2014US20140116058 Assemblies and apparatus related to combustor cooling in turbine engines
05/01/2014US20140116054 Radial flow fuel nozzle for a combustor of a gas turbine
05/01/2014US20140116053 Fuel injection assemblies in combustion turbine engines
04/2014
04/30/2014EP2725214A1 Rotor for turbine, process for producing same, method for bonding ni-based superalloy material to steel material, and structure
04/30/2014EP2725213A2 Atomizing air heat for attemperation
04/30/2014EP2723995A1 Accessory relay having an extended service life
04/30/2014EP2723993A1 Method for running up a stationary gas turbine
04/30/2014DE102012219520A1 Prozessgasverdichter-Gasturbinenstrang Process gas compressor gas turbine shafting
04/30/2014DE102012110328A1 Exhaust gas turbocharger of internal combustion engine, has relief device which self-adjusts compensation of turbine wheel, such that compressor wheel is operated by axial forces
04/30/2014DE102012107411B4 Verfahren zum Steuern einer Korona-Zündeinrichtung A method of controlling a corona ignition device
04/30/2014CN203571028U Rotor sealing structure of sealing clamping ring and combustion gas turbine
04/30/2014CN203570434U Exhaust unit of gas turbine and connecting piece thereof
04/30/2014CN203570433U Engine fuel oil heating device and carrier
04/30/2014CN103765099A Staged cooling flow nozzle valve
04/30/2014CN103765098A Bypass steam line
04/30/2014CN103765037A Turbo engine comprising damping fluid film for damping guide bearing of shaft of turbo engine and method of adjusting thickness of such damping fluid film
04/30/2014CN103764974A Combustor tail pipe, gas turbine with tail pipe, and method for manufacturing tail pipe
04/30/2014CN103758578A Gas turbine and method of operating gas turbine
04/30/2014CN102325981B System for supporting and servicing a gas turbine engine
04/30/2014CN102046984B Compressor cover for turbine engine having axial abutment
04/30/2014CN101960121B Gas turbine and method for maintaining and inspecting the same
04/30/2014CA2831519A1 Recuperator for gas turbine engine
04/30/2014CA2830925A1 Hot gas segment arrangement
04/29/2014US8708696 Swirl-counter-swirl microjets for thermoacoustic instability suppression
04/29/2014US8707713 Cooling hole with crenellation features
04/29/2014US8707712 Gas turbine engine turbine vane airfoil profile
04/29/2014US8707710 Tailorable design configuration topologies for aircraft engine mid-turbine frames
04/29/2014US8707707 Late lean injection fuel staging configurations
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