| 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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| 07/03/2014 | WO2014105688A1 Turbine exhaust case multi-piece frame |
| 07/03/2014 | WO2014105682A1 Turbine exhaust case multi-piece frame |
| 07/03/2014 | WO2014105668A1 Gas turbine engine nosecone attachment structure |
| 07/03/2014 | WO2014105658A1 Turbine engine component with dual purpose rib |
| 07/03/2014 | WO2014105657A1 Mount with deflectable tabs |
| 07/03/2014 | WO2014105621A1 Split cast vane fairing |
| 07/03/2014 | WO2014105619A1 Multi-function boss for a turbine exhaust case |
| 07/03/2014 | WO2014105617A1 Installation mounts for a turbine exhaust case |
| 07/03/2014 | WO2014105616A1 Turbine exhaust case architecture |
| 07/03/2014 | WO2014105604A1 Angled cut to direct radiative heat load |
| 07/03/2014 | WO2014105603A1 Multi-piece heat shield |
| 07/03/2014 | WO2014105602A1 Heat shield for a casing |
| 07/03/2014 | WO2014105599A1 Heat shield for cooling a strut |
| 07/03/2014 | WO2014105598A1 Slider seal |
| 07/03/2014 | WO2014105577A1 Scupper channelling in gas turbine modules |
| 07/03/2014 | WO2014105573A1 Heat shield based air dam for a turbine exhaust case |
| 07/03/2014 | WO2014105572A1 Combination flow divider and bearing support |
| 07/03/2014 | WO2014105547A1 Gas turbine engine component having suction side cutback opening |
| 07/03/2014 | WO2014105530A1 Multi-piece fairing for monolithic turbine exhaust case |
| 07/03/2014 | WO2014105529A1 Flow diverter to redirect secondary flow |
| 07/03/2014 | WO2014105528A1 Inter-module finger seal |
| 07/03/2014 | WO2014105525A1 Multi-purpose mounting |
| 07/03/2014 | WO2014105522A1 Air stream mixing in inner diameter (id) cavity |
| 07/03/2014 | WO2014105515A1 Cooling architecture for turbine exhaust case |
| 07/03/2014 | WO2014105512A1 Mechanical linkage for segmented heat shield |
| 07/03/2014 | WO2014105496A1 Flow diverter element and assembly |
| 07/03/2014 | WO2014105492A1 Passages to facilitate a secondary flow between components |
| 07/03/2014 | WO2014105482A1 Finger seal |
| 07/03/2014 | WO2014105432A1 Airfoil with variable profile responsive to thermal conditions |
| 07/03/2014 | WO2014105425A1 Turbine frame assembly and method of designing turbine frame assembly |
| 07/03/2014 | WO2014105394A1 Geared gas turbine engine exhaust nozzle with chevrons |
| 07/03/2014 | WO2014105393A1 Non-line of sight electro discharge machined part |
| 07/03/2014 | WO2014105392A1 Gas turbine engine serpentine cooling passage with chevrons |
| 07/03/2014 | WO2014105335A1 Aircraft and a retrofit cryogenic fuel system |
| 07/03/2014 | WO2014105331A1 Turbine engine assembly and dual fuel aircraft system |
| 07/03/2014 | WO2014105328A1 System for temperature and actuation control and method of controlling fluid temperatures in an aircraft |
| 07/03/2014 | WO2014105327A1 Turbine engine assembly comprising a cryogenic fuel system |
| 07/03/2014 | WO2014105325A1 Cryogenic fuel system and method for delivering fuel in an aircraft |
| 07/03/2014 | WO2014105245A1 Integral instrumentation in additively manufactured components of gas turbine engines |
| 07/03/2014 | WO2014105113A1 Gas turbine engine component having vascular engineered lattice structure |
| 07/03/2014 | WO2014105109A1 Gas turbine engine component having vascular engineered lattice structure |
| 07/03/2014 | WO2014105108A1 Gas turbine engine component having vascular engineered lattice structure |
| 07/03/2014 | WO2014105103A1 Platform with curved edges |
| 07/03/2014 | WO2014105102A1 Platform with curved edges adjacent suction side of airfoil |
| 07/03/2014 | WO2014104335A1 Power generation system |
| 07/03/2014 | WO2014103682A1 Exhaust gas processing equipment and gas turbine power generation system using same |
| 07/03/2014 | WO2014102682A1 Nacelle for aircraft, provided with a built-in system for anti-icing protection and acoustic absorption |
| 07/03/2014 | WO2014102441A1 Pre-heating system for a power plant |
| 07/03/2014 | WO2014102407A1 Hybrid plant with a combined solar-gas cycle, and operating method |
| 07/03/2014 | WO2014077909A3 Multi-lobed cooling holes in gas turbine engine components having thermal barrier coatings |
| 07/03/2014 | US20140186656 Spallation-Resistant Thermal Barrier Coating |
| 07/03/2014 | US20140186164 Non-line of sight electro discharge machined part |
| 07/03/2014 | US20140186158 Gas turbine engine shaft bearing configuration |
| 07/03/2014 | US20140186152 Blade outer air seal system for controlled tip clearance |
| 07/03/2014 | US20140183825 Finger seal |
| 07/03/2014 | US20140182972 Case with integral lubricant scavenge passage |
| 07/03/2014 | US20140182697 Adjustable supersonic air inlet |
| 07/03/2014 | US20140182309 Geared gas turbine engine exhaust nozzle with chevrons |
| 07/03/2014 | US20140182308 Gas turbine engine with v-band clamp connection for collector box |
| 07/03/2014 | US20140182305 System and method for a turbine combustor |
| 07/03/2014 | US20140182303 System and method for a turbine combustor |
| 07/03/2014 | US20140182301 System and method for a turbine combustor |
| 07/03/2014 | US20140182292 Integral instrumentation in additively manufactured components of gas turbine engines |
| 07/03/2014 | US20140182264 Aircraft engine systems and methods for operating same |
| 07/03/2014 | US20140182263 Maphbe Turbine |
| 07/03/2014 | DE202014102623U1 Flügel einer Turbine mit veränderlicher Geometrie Wings of a turbine with variable geometry |
| 07/03/2014 | DE102010061186B4 Zwangdurchlaufdampferzeuger mit Wandheizfläche und Verfahren zu dessen Betrieb Forced once-through steam generator with Wandheizfläche and method for its operation |
| 07/02/2014 | EP2749795A1 Shaft sealing device and rotating machine comprising same |
| 07/02/2014 | EP2749753A2 Electricity generating gas turbine |
| 07/02/2014 | EP2749739A2 Axial compressor and operation method of the same |
| 07/02/2014 | CN203685396U 燃机电厂利用天然气降压冷量的节能系统 Gas turbine power plant utilizing natural energy system down cold |
| 07/02/2014 | CN203685395U 用于燃气轮机进气加热与冷却的集成系统 For gas turbine inlet air heating and cooling systems integration |
| 07/02/2014 | CN203685394U 一种均匀燃气温度场的扰流环结构 Spoiler ring structure of a uniform gas temperature field |
| 07/02/2014 | CN203685317U 包括密封构件的涡轮机部件 Turbine component comprising a sealing member |
| 07/02/2014 | CN103906910A 具有可变总压力比的燃气涡轮发动机 Having a variable total pressure ratio gas turbine engine |
| 07/02/2014 | CN103899419A 轴流压缩机以及轴流压缩机的运转方法 Operation method of axial compressor and axial compressor |
| 07/02/2014 | CN102705083B 用于涡轮发动机的密封结构 A sealing structure for a turbine engine |
| 07/02/2014 | CN102362107B 轴封及具有其的旋转机械 Seal and rotary machine having the same |
| 07/02/2014 | CN101981162B 低排放发电和烃采收系统及方法 Low emission power generation and hydrocarbon recovery system and method |
| 07/02/2014 | CN101972749B 用于清洗飞行器燃气涡轮发动机的喷射设备和清洗系统 Aircraft gas turbine engines used for cleaning spray equipment and cleaning system |
| 07/02/2014 | CN101769204B 关于工业机械的燃料输送系统的方法、装置和/或系统 On industrial machinery, fuel delivery system methods, devices and / or systems |
| 07/01/2014 | US8765070 System and method for rejecting heat from equipment via endothermic isomerization |
| 07/01/2014 | US8764867 Aircraft oil flow management system for inverted flight |
| 07/01/2014 | US8764414 System for detecting contaminants in an intake flow of a compressor |
| 07/01/2014 | US8764383 Assembly for driving gas turbine accessories |
| 07/01/2014 | US8763631 Gas turbine metering valve |
| 07/01/2014 | US8763406 Turbomachine combustion chamber |
| 07/01/2014 | US8763405 Gas turbine engine rotary injection system and method |
| 07/01/2014 | US8763400 Aerodynamic pylon fuel injector system for combustors |
| 07/01/2014 | US8763359 Apparatus for combusting fuel within a gas turbine engine |
| 06/26/2014 | WO2014100817A1 Turbine engine gearbox mount with multiple fuse joints |
| 06/26/2014 | WO2014100684A1 Thermally compliant dual wall liner for a gas turbine engine |
| 06/26/2014 | WO2014100677A1 Egress seal assembly |
| 06/26/2014 | WO2014100650A1 Ignitor plug isolation chamber (ipic) for a gas turbine engine |
| 06/26/2014 | WO2014100553A1 Turbine disc with reduced neck stress concentration |
| 06/26/2014 | WO2014100347A1 Manufacture of full ring strut vane pack |
| 06/26/2014 | WO2014100316A1 Segmented seal for a gas turbine engine |
| 06/26/2014 | WO2014100203A1 Root spacer for arranging between a rotor disk and a root of a rotor blade |
| 06/26/2014 | WO2014100193A1 Rotor blade root spacer with a fracture feature |
| 06/26/2014 | WO2014100164A1 Vane carrier temperature control system in a gas turbine engine |