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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10/04/2013 | WO2012133774A1 Nozzle, gas turbine combustor and gas turbine |
10/03/2013 | WO2013149252A1 Turbine cooling apparatus |
10/03/2013 | WO2013149249A1 Air blocker ring assembly with radial retention |
10/03/2013 | WO2013148542A1 Gas turbine engine fan drive gear system damper |
10/03/2013 | WO2013148445A1 Blade wedge attachment |
10/03/2013 | WO2013148419A1 Torque frame bushing arrangement for gas turbine engine fan drive gear system |
10/03/2013 | WO2013147973A1 Gas turbine engine, combustor and dome panel |
10/03/2013 | WO2013147968A1 Gas turbine engine shaft bearing configuration |
10/03/2013 | WO2013147953A1 Aircraft propulsion gas turbine engine with heat exchange |
10/03/2013 | WO2013146637A1 Seal member, turbine, and gas turbine |
10/03/2013 | WO2013145402A1 Method for preventing deformation of a gas turbine casing, a purge device for executing same, and a gas turbine provided with purge device |
10/03/2013 | WO2013144512A1 Integration of parts of an afterbody of an aircraft engine |
10/03/2013 | WO2013144485A1 Turbojet engine nacelle air intake structure of laminar type |
10/03/2013 | WO2013144391A1 Brayton cycle with ambient cooling close to the critical isotherm |
10/03/2013 | WO2013144217A1 Steam turbine system and method for starting up a steam turbine |
10/03/2013 | WO2013144111A1 Gas turbine with adjustable cooling air system |
10/03/2013 | WO2013143975A1 Gas turbine power plant with non-homogeneous input gas |
10/03/2013 | US20130259670 Flow path structure and gas turbine exhaust diffuser |
10/03/2013 | US20130259657 Gas turbine engine geared architecture axial retention arrangement |
10/03/2013 | US20130259646 Dual-Intent Locator Pin and Removable Plug for Gas Turbines |
10/03/2013 | US20130256432 Air blocker ring assembly with leading edge configuration |
10/03/2013 | US20130256431 Air blocker ring assembly with blocker ring protrusions |
10/03/2013 | US20130255278 Effusion cooled shroud segment with an abradable system |
10/03/2013 | US20130255277 Gas turbine engine nose cone |
10/03/2013 | US20130255276 Transition Duct Mounting System |
10/03/2013 | US20130255274 Geared architecture with speed change device for gas turbine engine |
10/03/2013 | US20130255271 Fuel Supply System |
10/03/2013 | US20130255270 Passive equilization flow divider valve |
10/03/2013 | US20130255268 Turbine engine heat recuperator system |
10/03/2013 | US20130255267 System and method of improving emission performance of a gas turbine |
10/03/2013 | US20130255261 Swirler for combustion chambers |
10/03/2013 | US20130255260 Resonance damper for damping acoustic oscillations from combustor |
10/03/2013 | US20130255222 Gas combustor installed and detachable ignition module thereof |
10/02/2013 | EP2644868A2 Gas turbine and gas turbine power facilities |
10/02/2013 | EP2644867A2 Aircraft accessory drive multiple speed transmission |
10/02/2013 | EP2644866A2 Multi-shaft power extraction from gas turbine engine |
10/02/2013 | EP2644865A2 Method of startup control for a gas turbine system operating in a fired deceleration shutdown process mode |
10/02/2013 | EP2644864A2 Passive equilization flow divider valve |
10/02/2013 | EP2644847A1 Turbine engine heat recuperator system |
10/02/2013 | EP2644840A1 Steam turbine system and method for starting a steam turbine |
10/02/2013 | EP2644839A1 Gas turbine start with frequency converter |
10/02/2013 | EP2644508A1 System and method for cooling electrical components |
10/02/2013 | EP2643574A1 Monitoring of a filter of the fuel-supply system of an aircraft engine |
10/02/2013 | DE102013205020A1 Steuerung einer Gleichgewichtsdrift in einer rotierenden Baugruppe eines Turboladers Control of an equilibrium drift in a rotating assembly of a turbocharger |
10/02/2013 | DE102013103091A1 Bürstendichtungssystem mit elliptischem Spalt Brush seal system with elliptical gap |
10/02/2013 | CN203223296U Regulating system for synthesis gas heat value of IGCC (integrated gasification combined cycle) power station |
10/02/2013 | CN103339359A Method for operating a gas turbine in the case of load shedding, a device for controlling the operation of a gas turbine and a power plant |
10/02/2013 | CN103334838A Starting ignition oil supplying method of aviation gas turbine engine |
10/02/2013 | CN102011650B Multipoint frequent-explosion hydrogen energy steam turbine |
10/01/2013 | US8544255 Device for reducing turboprop infrared emissions |
10/01/2013 | US8544254 Turbine generator system |
10/01/2013 | CA2673139C Diffuser case removal apparatus and method |
10/01/2013 | CA2562290C Reversible gas turbine gearbox |
09/30/2013 | CA2810523A1 Gas turbine engine nose cone |
09/30/2013 | CA2810134A1 Turbine engine heat recuperator system |
09/27/2013 | CA2806951A1 Passive equilization flow divider valve |
09/26/2013 | WO2013142460A1 Trailing edge cooling |
09/26/2013 | WO2013141943A1 Gas turbine engine combustor |
09/26/2013 | WO2013141931A1 Gas turbine engine with geared architecture |
09/26/2013 | WO2013141930A1 Gas turbine engine with low fan pressure ratio |
09/26/2013 | WO2013140867A1 Turbine |
09/26/2013 | WO2013140655A1 Gas turbine |
09/26/2013 | WO2013139974A1 Ignition unit for turbojet engine |
09/26/2013 | WO2013139938A1 Cooled wall |
09/26/2013 | WO2013139904A1 Method for determining at least one firing temperature for controlling a gas turbine and gas turbine for performing the method |
09/26/2013 | WO2008071651A3 Turbine engine lubrication method and system |
09/26/2013 | US20130251538 Trailing edge cooling |
09/26/2013 | US20130251523 Intershaft Seal with Centrifugal Compensation |
09/26/2013 | US20130251504 Turbine bypass system |
09/26/2013 | US20130247587 Bi-metallic actuator for selectively controlling air flow between plena in a gas turbine engine |
09/26/2013 | US20130247585 Non-combustion energy source and configuration for brayton cycle heat engines |
09/26/2013 | US20130247584 Active control of compressor extraction flows used to cool a turbine exhaust frame |
09/26/2013 | US20130247581 Systems and Methods for Dampening Combustor Dynamics in a Micromixer |
09/26/2013 | US20130247580 System and method for recirculating a hot gas flowing through a gas turbine |
09/26/2013 | US20130247579 Method of startup control for a gas turbine system operating in a fired deceleration shutdown process mode |
09/26/2013 | US20130247578 Method for operating a fixed gas turbine, device for regulating the operation of a gas turbine and power plant |
09/26/2013 | US20130247576 Apparatus, system and method for observing combustor flames in a gas turbine engine |
09/26/2013 | US20130247575 Combustor heat shield |
09/26/2013 | US20130247541 Gas turbine intake anti-icing device |
09/26/2013 | US20130247540 Inspection device for an internal combustion engine |
09/26/2013 | US20130247538 Oil discharge device and turbomachine comprising such a device |
09/26/2013 | DE102012005770A1 Wärmekraftanlage mit gekühlter Supraleiterstruktur Thermal power plant with cooled superconductor structure |
09/26/2013 | CA2810032A1 Fuel manifold heat shield for a gas turbine engine |
09/26/2013 | CA2809818A1 Gas turbine start with frequency convertor |
09/25/2013 | EP2642648A1 Thermal energy device with cooled superconductor structure |
09/25/2013 | EP2642100A2 Method for removing particulate matter during operation of a gas turbine engine |
09/25/2013 | EP2642099A1 Method for determining at least one firing temperature for the control of a gas turbine and gas turbine for carrying out the method |
09/25/2013 | EP2642098A1 Gas turbine power plant with non-homogeneous input gas |
09/25/2013 | EP2642092A1 Method for operating a combined cycle power plant and plant to carry out such a method |
09/25/2013 | CN203214172U High-energy solid-state discharge ignition module |
09/25/2013 | CN203214171U Floating supporting and fixing device of stressing insulating screen |
09/25/2013 | CN203214170U Floating supporting and fixing structure of reinforcing heat screen |
09/25/2013 | CN103328800A Nacelle for an aircraft bypass turbojet engine |
09/25/2013 | CN103328787A Generating power using an ion transport membrane |
09/25/2013 | CN103328786A Mixing element for gas turbine units with flue gas recirculation |
09/25/2013 | CN103328772A 膨胀涡轮机 Expansion turbine |
09/25/2013 | CN103321753A Force-bearing cavity structure of gas turbine main bearing |
09/25/2013 | CN103321752A Independent apparatus used for flushing and oil sealing of gas turbine lubricating oil system |
09/25/2013 | CN103321751A Method for meeting a purge flow requirement for a power plant and a power plant having a purge control system |
09/25/2013 | CN103321750A Method for operating a combined cycle power plant and plant to carry out such a method |