| 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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| 09/14/2014 | CA2831315A1 Gas turbine engine fuel system with ecology valve |
| 09/13/2014 | CA2845143A1 Carbon seal assembly |
| 09/12/2014 | WO2014138617A1 Fluid-cooled seal arrangement for a gas turbine engine |
| 09/12/2014 | WO2014138474A1 Filtration system for a gas turbine air intake and methods |
| 09/12/2014 | WO2014138432A1 Oil system debris monitor system for a gas turbine engine |
| 09/12/2014 | WO2014138416A1 Fixturing for thermal spray coating of gas turbine components |
| 09/12/2014 | WO2014138340A1 Gas turbine fuel injector with metering cavity |
| 09/12/2014 | WO2014138320A1 Gas turbine engine component having variable width feather seal slot |
| 09/12/2014 | WO2014138143A1 Non-contacting seals for geared gas turbine engine bearing compartments |
| 09/12/2014 | WO2014138078A1 Flexible finger seal for sealing a gap between turbine engine components |
| 09/12/2014 | WO2014137692A1 Gas turbine engine lubrication system |
| 09/12/2014 | WO2014137688A1 Gas turbine engine nose cone attachment |
| 09/12/2014 | WO2014137687A1 Gas turbine engine component external surface micro-channel cooling |
| 09/12/2014 | WO2014137686A1 Gas turbine engine high lift airfoil cooling in stagnation zone |
| 09/12/2014 | WO2014137685A1 Gas turbine engine inlet |
| 09/12/2014 | WO2014137577A1 Ring-shaped compliant support |
| 09/12/2014 | WO2014137575A1 Gearbox mounting assembly |
| 09/12/2014 | WO2014137574A1 Mid-turbine frame rod and turbine case flange |
| 09/12/2014 | WO2014137571A1 Fan drive gear system spline oil lubrication scheme |
| 09/12/2014 | WO2014137553A1 Exhaust system having a flow path liner supported by structural duct segments |
| 09/12/2014 | WO2014137465A1 Gas turbine engine with a clearance control system and corresponding method of operating a gas turbine engine |
| 09/12/2014 | WO2014137452A1 Multi-shaft gas turbine engine |
| 09/12/2014 | WO2014137451A1 Ram air thermal management system for an aircraft engine |
| 09/12/2014 | WO2014137448A1 Fan blades with protective sheaths and galvanic shields |
| 09/12/2014 | WO2014137446A1 Hybrid fan blades for jet engines |
| 09/12/2014 | WO2014137431A1 Brush seal repair method |
| 09/12/2014 | WO2014137417A1 Gas turbine engine heat exchanger system |
| 09/12/2014 | WO2014137409A1 Flexible bellows igniter seal for a gas turbine with a ceramic combustion liner |
| 09/12/2014 | WO2014136514A1 Gas discharge duct |
| 09/12/2014 | WO2014136235A1 Method for forming aluminide coating film on base |
| 09/12/2014 | WO2014135942A1 Apparatus for protecting aircraft components against foreign object damage |
| 09/12/2014 | WO2014135812A1 Nacelle equipped with an oil-cooling circuit comprising an intermediate heat exchanger |
| 09/12/2014 | WO2014135797A1 Compact dosing device for an injector with two fuel circuits for an aircraft turbomachine |
| 09/12/2014 | CA2844194A1 Lubrication ring |
| 09/11/2014 | US20140255168 Inter-module flow discourager |
| 09/11/2014 | US20140255147 Method of immobilizing low pressure spool and locking tool therefore |
| 09/11/2014 | US20140252769 Gas turbine engine with internal electromechanical device |
| 09/11/2014 | US20140252721 Slotted labyrinth seal |
| 09/11/2014 | US20140252161 De-couple geared turbo-fan engine and aircraft |
| 09/11/2014 | US20140250917 Combustion chamber heat shield and seal assembly and a method of manufacturing a combustion chamber heat shield and seal assembly |
| 09/11/2014 | US20140250916 System and method for aligning a gas turbine engine |
| 09/11/2014 | US20140250915 Centerline support bar for steam turbine component |
| 09/11/2014 | US20140250914 Starter Motor Shared Lubrication System |
| 09/11/2014 | US20140250910 Thermal stress reduction in aircraft motor controllers |
| 09/11/2014 | US20140250909 Series Battery Start Controller |
| 09/11/2014 | US20140250908 Systems and Methods for Controlling Combustion of a Fuel |
| 09/11/2014 | US20140250907 Gas turbine fuel injector with metering cavity |
| 09/11/2014 | US20140250900 Gas turbine power plant with carbon dioxide separation |
| 09/11/2014 | US20140250899 Gas turbine engine thermally controlled flow device |
| 09/11/2014 | US20140250895 Modulated ejector cooling |
| 09/11/2014 | US20140250893 Device and method for preventing leakage of air between multiple turbine components |
| 09/11/2014 | US20140250892 Lean fuel intake gas turbine |
| 09/11/2014 | US20140250860 Multi-shaft gas turbine engine |
| 09/11/2014 | US20140250859 Axial-flow turbine and power plant including the same |
| 09/11/2014 | DE102014103078A1 Systeme und Verfahren zur Lieferung einer Spülluftströmung und einer einstellbaren Kühlluftströmung in einer Gasturbinenanwendung Systems and methods for providing a purge airflow, and an adjustable flow of cooling air in a gas turbine application |
| 09/11/2014 | DE102014102778A1 Strömungshülse zur thermischen Steuerung eines doppelwandigen Turbinengehäuses und zugehöriges Verfahren Flow sleeve for thermal control of a double turbine housing and associated method |
| 09/11/2014 | DE102013203780A1 Turboladeranordnung und Verfahren zum Herstellen einer Turboladeranordnung Turbocharger assembly and method of manufacturing a turbocharger assembly |
| 09/11/2014 | DE102013005167B3 Abgasturbolader Exhaust gas turbocharger |
| 09/11/2014 | DE102013003444A1 Prall-effusionsgekühlte Schindel einer Gasturbinenbrennkammer mit verlängerten Effusionsbohrungen Impact-effusionsgekühlte shingle a gas turbine combustor with prolonged effusion holes |
| 09/11/2014 | DE102004010620B4 Brennkammer zur wirksamen Nutzung von Kühlluft zur akustischen Dämpfung von Brennkammerpulsation Combustion chamber for efficient use of cooling air to the acoustic attenuation of Brennkammerpulsation |
| 09/11/2014 | CA2846156A1 Series battery start controller |
| 09/11/2014 | CA2845161A1 Lubrication oil system for a reduction gearbox |
| 09/11/2014 | CA2844212A1 Method of immobilizing low pressure spool and locking tool therefore |
| 09/11/2014 | CA2844173A1 Method of assembling an electromechanical device in a gas-turbine engine |
| 09/11/2014 | CA2844171A1 Gas turbine engine with internal electromechanical device |
| 09/10/2014 | EP2775120A1 Gas turbine system |
| 09/10/2014 | EP2773873A1 Bearing system for a turbocompressor and turbocompressor having the bearing system |
| 09/10/2014 | EP2773851A1 Tie-rod nut including a nut flange with a plurality of mounting apertures |
| 09/09/2014 | US8827651 Annulus filler |
| 09/09/2014 | US8827638 Connection assembly for joining a turbine housing and a bearing housing and exhaust gas turbocharger |
| 09/09/2014 | US8827633 Gas turbine engine fan drive gear system damper |
| 09/09/2014 | US8826671 Control system for a gas turbine power plant |
| 09/09/2014 | US8826669 Gas turbine exhaust case |
| 09/09/2014 | US8826641 Thermal management system integrated pylon |
| 09/09/2014 | US8826639 High efficiency power generation system and system upgrades |
| 09/09/2014 | US8826637 Arrangement for the discharge of oil-venting air on a gas-turbine engine |
| 09/09/2014 | CA2656282C Air intake for an aircraft turbine engine |
| 09/09/2014 | CA2656206C Turbine engine for aircraft |
| 09/09/2014 | CA2656137C Turbine engine for aircraft |
| 09/09/2014 | CA2643598C Integration of a starter/generator module in a gas turbine transmission housing |
| 09/09/2014 | CA2643325C Internal fuel manifold with turned channel having a variable cross-sectional area |
| 09/09/2014 | CA2626119C Inter-turbine housing with cooling circuit and jet engine comprising same |
| 09/09/2014 | CA2593868C Process for treating oil emissions in a gas turbine engine |
| 09/08/2014 | CA2844675A1 Combustor heat shield with carbon avoidance feature |
| 09/08/2014 | CA2838464A1 Device and method for preventing leakage of air between multiple turbine components |
| 09/06/2014 | CA2844966A1 Lubrication system for turboprop |
| 09/04/2014 | WO2014134536A1 Method and apparatus for selectively collecting pre-diffuser airflow |
| 09/04/2014 | WO2014134529A1 Method and apparatus for handling pre-diffuser airflow for cooling high pressure turbine components |
| 09/04/2014 | WO2014134523A1 Method and apparatus for handling pre-diffuser flow for cooling high pressure turbine components |
| 09/04/2014 | WO2014134519A1 Method and apparatus for collecting pre-diffuser airflow and routing it to combustor pre-swirlers |
| 09/04/2014 | WO2014134517A1 Method and apparatus for handling pre-diffuser airflow for cooling high pressure turbine components |
| 09/04/2014 | WO2014134513A1 Method and apparatus for handling pre-diffuser airflow for use in adjusting a temperature profile |
| 09/04/2014 | WO2014134478A1 Gas turbine inlet filter with replaceable media cartridges |
| 09/04/2014 | WO2014134262A1 Repair of surface damage at edges of cellular panels |
| 09/04/2014 | WO2014134256A1 Low spool starter system for gas turbine engine |
| 09/04/2014 | WO2014134040A1 Integrated thermal management with nacelle laminar flow control for geared architecture gas turbine engine |
| 09/04/2014 | WO2014133958A1 Assembly for sealing a gap between components of a turbine engine |
| 09/04/2014 | WO2014133952A1 Cooled seal assembly for arranging between a stator and a rotor |
| 09/04/2014 | WO2014133836A1 Self cleaning debris filter for fan drive gear system |
| 09/04/2014 | WO2014133804A1 Split airfoil cluster and method therefor |