Patents
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)
07/2010
07/14/2010EP2206884A2 Rotor cooling circuit
07/14/2010EP2206882A2 Centrifugal Compressor Forward Thrust and Turbine Cooling Apparatus
07/14/2010EP2205843A2 Fuel supply system
07/14/2010CN1864042B Method for efficient nonsynchronous LNG production
07/14/2010CN101779171A Plant state monitoring method, plant state monitoring computer program, and plant state monitoring device
07/14/2010CN101779002A Turbine blade
07/14/2010CN101776016A Late lean injection control strategy
07/14/2010CN101776015A Premixed partial oxidation syngas generation and gas turbine system
07/14/2010CN101776014A Late lean injection with expanded fuel flexibility
07/14/2010CN101776013A Method and apparatus to enhance transition duct cooling in a gas turbine engine
07/14/2010CN101776012A System and method for removing a foreign object from an airstream entering a turbomachine
07/14/2010CN101776010A Method and equipment for cleaning turbofan gas turbine engine
07/13/2010US7752851 Fastening a combustion chamber inside its casing
07/13/2010US7752849 Arrangement for controlling flow of fluid to a component of a gas turbine engine
07/13/2010US7752847 Liquid injection in a gas turbine during a cooling down phase
07/13/2010CA2487199C Method for repairing components using environmental bond coatings and resultant repaired components
07/13/2010CA2466562C Zero twist carrier
07/13/2010CA2458458C Sealing method and device for a gas turbine shaft
07/13/2010CA2453916C Modular metal working tooling apparatus
07/08/2010WO2010077766A2 Method and systems for an engine starter/generator
07/08/2010WO2010077241A1 Engine air particle separator
07/08/2010US20100173225 Compositions and methods for hydrogen generation
07/08/2010US20100170267 Burner for a gas turbine
07/08/2010US20100170266 Method and apparatus for controlling a heating value of a low energy fuel
07/08/2010US20100170264 Turbine shroud thermal distortion control
07/08/2010US20100170263 Vortex Combustor for Low NOX Emissions when Burning Lean Premixed High Hydrogen Content Fuel
07/08/2010US20100170262 Aircraft power and thermal management system with electric co-generation
07/08/2010US20100170255 Methods and systems to enhance flame holding in a gas turbine engine
07/08/2010US20100170254 Late lean injection fuel staging configurations
07/08/2010US20100170253 Method and apparatus for fuel injection in a turbine engine
07/08/2010US20100170251 Late lean injection with expanded fuel flexibility
07/08/2010US20100170249 Method and apparatus to facilitate cooling of a diffusion tip within a gas turbine engine
07/08/2010US20100170219 Late lean injection control strategy
07/08/2010US20100170218 Method for expanding compressor discharge bleed air
07/08/2010US20100170216 Late lean injection system configuration
07/08/2010DE19882244B4 Combined cycle power plant - has vapour stop valve which immediately closes vapour entrance of vapour cooling system, after gas turbine stoppage
07/08/2010DE102009059330A1 Verfahren und Vorrichtung zur Kühlung eines Übergangsstücks Method and apparatus for cooling a transition piece
07/08/2010DE102008062355A1 Turboverdichterstrang und Verfahren zum Betreiben desselben sowie Erdgasverflüssigungsanlage mit dem Turboverdichterstrang The same turbo compressor train and methods of operating and natural gas liquefaction plant with the turbo compressor train
07/08/2010CA2748257A1 Method and systems for an engine starter/generator
07/07/2010EP2204595A1 Methods, apparatus and/or systems relating to fuel delivery systems for industrial machinery
07/07/2010EP2204563A2 Operating a turbine at baseload on cold fuel with hot fuel combustion hardware
07/07/2010EP2204551A1 Gas turbine for electric power generation
07/07/2010CN101772628A Fuel control method and fuel control apparatus for gas turbine and gas turbine
07/07/2010CN101772586A Ni-base alloy-high chromium steel structure and process for producing the ni-base alloy-high chromium steel structure
07/07/2010CN101769204A Methods, apparatus and/or systems relating to fuel delivery systems for industrial machinery
07/07/2010CN101769203A Methods, systems and/or apparatus relating to inducers for turbine engines
07/07/2010CN101769202A Apparatus for starting a steam turbine against rated pressure
07/06/2010US7751943 Protection process and control system for a gas turbine
07/06/2010US7748209 Small single use gas turbine engine with oil-less bearing arrangement
07/06/2010US7748208 Compact recirculating lubrication system for a miniature gas turbine engine
07/06/2010CA2429425C Combustor turbine successive dual cooling
07/06/2010CA2373188C Manufacturing process of panel with adapted acoustic impedance layer and acoustic panel thus obtained
07/01/2010WO2010075393A2 Gas turbine engine and system for servicing a gas turbine engine
07/01/2010WO2010075390A2 System for supporting and servicing a gas turbine engine
07/01/2010WO2010074895A1 Method and systems for adaptive ignition energy
07/01/2010WO2010073657A1 One-stage stator vane cooling structure and gas turbine
07/01/2010WO2010072911A1 Aircraft propulsion equipment with an improved reduction gear transmission device
07/01/2010WO2010072472A1 Power plant comprising a turbine unit and a generator
07/01/2010US20100167139 Process for the conversion of natural gas to hydrocarbon liquids
07/01/2010US20100167138 Process for the conversion of natural gas to hydrocarbon liquids
07/01/2010US20100167137 Process for the conversion of natural gas to hydrocarbon liquids
07/01/2010US20100167136 Process for the conversion of natural gas to hydrocarbon liquids
07/01/2010US20100167135 Process for the conversion of natural gas to hydrocarbon liquids
07/01/2010US20100167134 Process for the conversion of natural gas to hydrocarbon liquids
07/01/2010US20100166546 Apparatuses, systems, and methods of gas turbine engine component interconnection
07/01/2010US20100163671 A mounting element for a gas turbine engine, and a structure and an aircraft with such a mounting element
07/01/2010US20100162726 Mobile platform system for a gas turbine engine
07/01/2010US20100162725 Gas turbine engine device
07/01/2010US20100162723 Gas turbine engine shaft coupler
07/01/2010US20100162722 Tip clearance control
07/01/2010US20100162721 Apparatus for starting a steam turbine against rated pressure
07/01/2010US20100162717 Shielding for a gas turbine engine component
07/01/2010US20100162716 Paneled combustion liner
07/01/2010US20100162714 Fuel nozzle with swirler vanes
07/01/2010US20100162712 Quench jet arrangement for annular rich-quench-lean gas turbine combustors
07/01/2010US20100162710 Pre-Mix Combustion System for a Gas Turbine and Method of Operating of operating the same
07/01/2010US20100162709 Fuel supply system
07/01/2010US20100162683 Turbofan engine
07/01/2010DE102009059316A1 Vorrichtung zum Starten einer Dampfturbine gegen Nenndruck Means for starting a steam turbine rated pressure
07/01/2010DE102009059222A1 DLN-Zweibrennstoff-Primärdüse DLN Two fuel primary nozzle
07/01/2010DE102009055881A1 Hochtemperatur-Dichtungsanordnung für optischen Sensor High-temperature sealing arrangement for optical sensor
07/01/2010DE102008063212A1 Shaft unit for turbocharger, has shaft which is arranged in bearing bush unit, where shaft unit is connected with lever element at side, and one or multiple sealing devices are provided between lever element and bearing bush unit
06/2010
06/30/2010EP2202396A1 Fuel control method and fuel control system for gas turbine, and gas turbine
06/30/2010EP2202395A2 Coupling for generator/starter
06/30/2010EP2202394A2 Gas turbine engine operations support systems and methods with model-based torque estimates
06/30/2010EP2202387A1 Control-free isolation valve for the oil circuit of an airplane engine
06/30/2010EP2201234A2 Hydraulic drive, hydraulic supply device, airplane with a hydraulic supply device and method for configuring a hydraulic supply device
06/30/2010CN101765744A 燃气轮机 Gas turbine
06/30/2010CN101765708A Intake air heating control device for gas turbine
06/30/2010CN101761395A Hot gas turbine
06/30/2010CN101761394A Negative overload resistant double-chamber oil supply device and method thereof
06/30/2010CN101761389A Circulatory thermal power generation method and device of working medium phase-change gas turbine
06/30/2010CA2689176A1 Gas turbine engine with ejector
06/29/2010US7745950 Generator-starter system for a multi-shaft engine
06/29/2010US7744827 reacts the dissolved dioxygen with the sulfur compounds typically present within fuel to form oxidized sulfur compounds like sulfoxides and sulfones; second stage reacts the most active organic moieties with remaining di-oxygen to form hydroperoxides; decomposed to non-coke inducing organic oxygenates
06/29/2010US7744096 Seal device
06/29/2010US7743742 Cylinder head cover with oil separator
06/29/2010US7743600 Gas turbine engine telemetry module
06/29/2010US7743598 Sealing system for the rear lubricating chamber of a jet engine
06/29/2010CA2430915C Fluid and fuel delivery systems reducing pressure fluctuations and engines including such systems