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)
08/2010
08/19/2010WO2010093531A1 Air vehicle propulsion system with counter rotating fan design and method for noise reduction
08/19/2010WO2010092267A1 Aircraft engine with cooling for an electric starting device
08/19/2010WO2010092094A1 System of compact contra-rotating propellers
08/19/2010WO2010092080A1 Method for monitoring the health status of devices that affect the starting capability of a jet engine
08/19/2010US20100205977 Waste heat utilization for pre-heating fuel
08/19/2010US20100205975 Integral suction device with acoustic panel
08/19/2010US20100205973 Gas turbine with welded combustor liners
08/19/2010US20100205972 One-piece can combustor with heat transfer surface enhacements
08/19/2010US20100205971 Fuel nozzle having aerodynamically shaped helical turning vanes
08/19/2010US20100205970 Systems, Methods, and Apparatus Providing a Secondary Fuel Nozzle Assembly
08/19/2010US20100205927 Apparatus for a nitrogen purge system
08/19/2010DE10153911B4 Befestigungsmittel für Einspritzdüsen in einem Luftansaugkanal einer Strömungsmaschine Fastener for injectors in an air intake duct of a turbomachine
08/19/2010CA2752526A1 Aircraft engine with cooling for an electric starting device
08/19/2010CA2752214A1 System of compact contra-rotating propellers
08/18/2010EP2218890A1 Waste heat utilization for pre-heating fuel
08/18/2010EP2218889A2 Gas turbine plant with preheated combustion air and corresponding operating method
08/18/2010CN101806251A Starting control device of micro gas turbine and starting control method
08/18/2010CN101806250A Waste heat utilization for pre-heating fuel
08/18/2010CN101806247A Combined cycle power plant burning low btu fuel
08/18/2010CN101280723B Method and device for reutilization of natural gas pipe network pressure energy in gas turbine working domain
08/17/2010US7775764 Gas turbine engine rotor ventilation arrangement
08/17/2010US7775053 Heat transfer augmentation in a compact heat exchanger pedestal array
08/17/2010US7775052 Active combustion control system for gas turbine engines
08/17/2010US7775051 Arrangement for a jet engine combustion chamber
08/17/2010US7775050 Method and apparatus for reducing stresses induced to combustor assemblies
08/17/2010US7775049 Integrated strut design for mid-turbine frames with U-base
08/17/2010US7775031 Recuperator for aircraft turbine engines
08/17/2010CA2693314A1 Fluid conduit coupling with leakage detection
08/17/2010CA2462846C Method for removing coating material from a cooling hole of a gas turbine engine component
08/12/2010WO2010089880A1 Turbofan engine
08/12/2010WO2010089498A2 Turbojet engine nacelle
08/12/2010WO2010089497A1 Method for making a network of drainage pipes and acoustic processing panel including such a network of drainage pipes
08/12/2010WO2010089496A1 Acoustic processing panel, more particularly adapted for an air intake in an aircraft nacelle
08/12/2010WO2010089204A1 Method for flushing a section of a fuel system of a gas turbine
08/12/2010US20100202873 Ceramic Matrix Composite Turbine Engine
08/12/2010US20100201080 Seal structure for gas turbine combustor
08/12/2010US20100200699 System for defrosting the leading edge sheath of an air inlet hood for a turboengine
08/12/2010US20100199684 Combustion liner assembly support
08/12/2010US20100199682 Process for the production of hydrogen with total recovery of co2 and reduction of unconverted methane
08/12/2010US20100199681 Fuel system of gas turbine engines
08/12/2010US20100199628 Interlocking Retention Strip
08/12/2010US20100199626 Turbine engine exhaust gas tube mixer
08/12/2010DE102009007736A1 Turbinengehäuse für einen Abgasturbolader eines Antriebsaggregats und Verfahren zum Herstellen eines Turbinengehäuses Turbine casing for an exhaust gas turbocharger of a drive unit and method for manufacturing a turbine housing
08/12/2010DE102009007735A1 Double-flow turbine housing for exhaust gas turbocharger of e.g. internal combustion engine, has guide vane arranged in transfer region between spiral channel and space, and intermediate wall sectionwise integrally designed with vane
08/12/2010DE102009007734A1 Turbine housing i.e. two-vaned turbine housing, for exhaust-gas turbocharger of drive unit, has spiral duct including inner part via which exhaust gas flows, and thermally insulating opening formed between outer shell of duct and inner part
08/12/2010DE102009007696A1 Bearing arrangement for rotor of exhaust gas turbocharger in motor vehicle, has sleeves whose front sides are inclined, and longitudinal channel running transverse to inlet channels and connecting inlet channels and front sides
08/12/2010DE102009007666A1 Verfahren zur Herstellung einer verschleißfesten Beschichtung auf einem Bauteil A process for producing a wear resistant coating on a component
08/12/2010DE102009007164A1 Verfahren zum Ausbilden einer Kühlluftöffnung in einer Wand einer Gasturbinenbrennkammer sowie nach dem Verfahren hergestellte Brennkammerwand A method for forming a cooling air opening in a wall of a gas turbine combustor as well as prepared by the process chamber wall
08/12/2010CA2751121A1 Turbojet engine nacelle
08/12/2010CA2692877A1 Fuel delivery system with reduced heat transfer to fuel manifold seal
08/11/2010EP2216530A2 Aircraft electric generation system
08/11/2010EP2216529A1 Method for purging a section of a fuel system of a gas turbine
08/11/2010EP2216505A2 Turbine coverplate systems
08/11/2010EP2215341A2 Low shock strength propulsion system
08/11/2010EP2215340A1 Heat shield and turbocharger having a heat shield
08/11/2010CN201546818U Electronic starter of turbine jet
08/11/2010CN101802368A Hydraulic drive, hydraulic supply device, airplane with a hydraulic supply device and method for configuring a hydraulic supply device
08/11/2010CN101802367A Intake silencer for gas turbine
08/11/2010CN101802366A Turbine facility and power generating apparatus
08/11/2010CN101802243A Heat-shielding coating material
08/11/2010CN101798961A Two-stage beveled supersonic speed air inlet lip
08/11/2010CN101798960A A system for catalytic combustion
08/11/2010CN101798959A Gas turbine
08/11/2010CN101798958A Inner culvert turbofan engine
08/11/2010CN101392662B Oil pipe filter for steam turbine and gas turbine
08/10/2010US7770401 Combustor and component for a combustor
08/10/2010US7770400 Non-linear fuel transfers for gas turbines
08/10/2010US7770377 Turbofan arrangement
08/10/2010CA2496543C Recirculation structure for a turbocompressor
08/10/2010CA2484432C Methods and apparatus for assembling gas turbine engines
08/10/2010CA2413641C Method of restoration of mechanical properties of cast inconel 718 for serviced aircraft components
08/05/2010WO2010086422A1 Assembly including an agb and an oil tank
08/05/2010WO2010086287A1 Ignition laser
08/05/2010US20100196684 Turbine Element Repair
08/05/2010US20100192594 Compressed air starter for turbomachine
08/05/2010US20100192592 Combined catalysts for the combustion of fuel in gas turbines
08/05/2010US20100192591 Burner for a gas turbine and method for feeding a gaseous fuel in a burner
08/05/2010US20100192586 Gas turbine combustor
08/05/2010US20100192584 Gas turbine combustor
08/05/2010US20100192579 Apparatus for Fuel Injection in a Turbine Engine
08/05/2010US20100192577 System and method for reducing combustion dynamics in a turbomachine
08/05/2010US20100192537 Methods and apparatus for a nitrogen purge system
08/05/2010DE102010000254A1 Landgestütztes Einfachzyklus-Hybridtriebwerk auf der Basis eines Pulsdetonationsbrenners zur Energieerzeugung Land Based simple-cycle hybrid engine based on a pulse detonation combustor for energy
08/05/2010DE102007002422B4 Gestufte Kraftstoffeinspritzvorrichtung und Verfahren zum Kühlen einer gestuften Kraftstoffeinspritzvorrichtung Staged fuel injection apparatus and method for cooling a staged fuel injector
08/05/2010CA2750490A1 Assembly including an agb and an oil tank
08/04/2010EP2213866A2 Gas turbine engine assembly with gear and method of assembling same
08/04/2010EP2213864A2 Linear quadratic regulator control for bleed air system fan air valve
08/04/2010EP2213862A1 Device and method for controlling emissions of an electric power plant
08/04/2010EP2213848A1 Integrated coal gasification combined cycle facility
08/04/2010EP2213846A1 Method for demounting blade ring and member for demounting blade ring
08/04/2010EP2213845A1 Method and apparatus for cleaning a turbofan gas turbine engine
08/04/2010CN101796304A Fluid intake assembly
08/04/2010CN101793409A Systems and methods for mitigating a flashback condition in a premixed combustor
08/04/2010CN101793269A Compressor clearance control system using bearing oil waste heat
08/04/2010CN101793197A Method and apparatus for controlling a heating value of a low energy fuel
08/04/2010CN101793196A System and method for automatic fuel bending and control for combustion gas turbine
08/04/2010CN101793195A Method and system for enhancing the heat transfer of turbine engine components
08/04/2010CN101793194A Inset bleed heat system thermal lag mitigation using compressor interstage bleeds
08/03/2010US7767076 Adding vanadium-containing heavy oil and supercritical water containing an oxidizing agent to a reactor;reforming the heavy oil; oxidizing the vanadium,producing the vanadium oxide
08/03/2010US7766992 Producing metallic articles by reduction of nonmetallic precursor compounds and melting