| 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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| 12/10/2005 | CA2509385A1 Homogeneous welding via pre-heating for high strength superalloy joining and material deposition |
| 12/08/2005 | WO2005116419A1 Method and apparatus generating multiple pressure signals in a fuel system |
| 12/08/2005 | WO2005116407A2 Gas turbine engine including a low pressure sump seal buffer source and thermally isolated sump |
| 12/08/2005 | WO2005116405A1 A support structure in a turbine or compressor device and a method for assembling the structure |
| 12/08/2005 | WO2005039978A3 Aircraft protection method and system |
| 12/08/2005 | WO2004077400A8 Honeycomb core acoustic unit with metallurgically secured deformable septum, and method of manufacture |
| 12/08/2005 | US20050271505 Turbine engine shroud segment, hanger and assembly |
| 12/08/2005 | US20050271504 Seal system |
| 12/08/2005 | US20050271499 Methods and systems for operating rotary machines |
| 12/08/2005 | US20050269446 Aircraft engine mount |
| 12/08/2005 | US20050269443 Air intake structure for aircraft engine |
| 12/08/2005 | US20050269055 Method and apparatus for production of a cast component |
| 12/08/2005 | US20050268972 Fuel metering unit |
| 12/08/2005 | US20050268619 Method and apparatus for increasing the pressure of cooling fluid within a gas turbine engine |
| 12/08/2005 | US20050268617 Methods and apparatus for low emission gas turbine energy generation |
| 12/08/2005 | US20050268615 Method and apparatus for cooling combustor liner and transition piece of a gas turbine |
| 12/08/2005 | US20050268614 Premixing burner with impingement cooled centerbody and method of cooling centerbody |
| 12/08/2005 | US20050268613 Method and apparatus for cooling combustor liner and transition piece of a gas turbine |
| 12/08/2005 | US20050268612 Engine |
| 12/08/2005 | US20050268594 Fast start-up combined cycle power plant |
| 12/08/2005 | US20050268593 Thermal management for aircraft auxiliary power unit compartment |
| 12/08/2005 | US20050268462 Methods and apparatus for fabricating a turbine nozzle assembly |
| 12/08/2005 | DE102005020376A1 Humidifier for gas flow has means to determine fluid mass flow separated in droplet separator, and regulator to control atomizing pressure as regulating variable and position of operating component as correcting variable |
| 12/08/2005 | DE102004024294A1 Gas turbine plant has compressor drawing air through cooling stretch which incorporates earth heat exchanger consisting of pipe register of parallel pipes and which is bridged by temperature controlled bypass |
| 12/08/2005 | CA2563821A1 Gas turbine engine including a low pressure sump seal buffer source and thermally isolated sump |
| 12/08/2005 | CA2502805A1 Turbine engine shroud segment, hanger and assembly |
| 12/07/2005 | EP1602810A1 Sound absorber for compressor |
| 12/07/2005 | EP1602802A1 Seal system |
| 12/07/2005 | EP1601865A1 Compact compound engine package |
| 12/07/2005 | EP1601864A1 Integral cooling system for rotary engine |
| 12/07/2005 | CN1705815A Gas turbine combustor, and gas turbine with the combustor |
| 12/07/2005 | CN1705524A Method and apparatus for cleaning a turbofan gas turbine engine |
| 12/07/2005 | CN1704574A Premixing burner with impingement cooled centerbody and method of cooling centerbody |
| 12/07/2005 | CN1704573A Method and apparatus for cooling combustor liner and transition piece of a gas turbine |
| 12/07/2005 | CN1704560A Methods and apparatus for fabricating a turbine nozzle assembly |
| 12/06/2005 | US6973193 Fan and compressor noise attenuation |
| 12/06/2005 | US6971241 Dual mode power unit having a combustor bypass system |
| 12/06/2005 | US6971227 System and method to stage primary zone airflow |
| 12/06/2005 | CA2292437C Pulsed-vapor phase aluminide process for high temperature oxidation-resistant coating applications |
| 12/04/2005 | CA2508418A1 Methods and apparatus for low emission gas turbine energy generation |
| 12/02/2005 | CA2508391A1 Methods and apparatus for fabricating a turbine nozzle assembly |
| 12/01/2005 | US20050266266 Nickel aluminide coating with improved oxide stability |
| 12/01/2005 | US20050265844 Cooled rotor blade |
| 12/01/2005 | US20050265842 Cooled rotor blade |
| 12/01/2005 | US20050265841 Cooled rotor blade |
| 12/01/2005 | US20050265840 Cooled rotor blade with leading edge impingement cooling |
| 12/01/2005 | US20050265839 Cooled rotor blade |
| 12/01/2005 | US20050265836 Cooled rotor blade and method for cooling a rotor blade |
| 12/01/2005 | US20050265831 Method for coating gas turbine engine components |
| 12/01/2005 | US20050265825 Spacing arrangement |
| 12/01/2005 | US20050265822 Method of operating a compressor near the compressor pumping limit and compressor |
| 12/01/2005 | US20050263643 Cowl structure for a gas turbine engine |
| 12/01/2005 | US20050262849 Gas turbine control apparatus and gas turbine system using the same |
| 12/01/2005 | US20050262848 Methods and apparatus for operating gas turbine engines |
| 12/01/2005 | US20050262843 Gas turbine engine combustor mixer |
| 12/01/2005 | US20050262824 Fuel supply system |
| 12/01/2005 | US20050262683 Manufacturing cell using tooling apparatus |
| 12/01/2005 | DE4226666B4 Wärmetauscher für die Kühlung eines heißen Gases Heat exchanger for cooling a hot gas |
| 12/01/2005 | DE102005021664A1 Process for modifying the surface of a ceramic core used on turbine parts comprises applying a ceramic-based material to the surface of the ceramic core using a direct scribing method according to a previously selected pattern |
| 12/01/2005 | DE102004018585A1 Gas turbine engine inlet cone, has upper surface whose structure varies in axial direction such that surface applies force on inflowing particles, relative to rotation axis, so that particles are conducted radially outwards along trajectory |
| 12/01/2005 | CA2549091A1 Durable thermal barrier coating having low thermal conductivity |
| 11/30/2005 | EP1600693A2 Gas turbine engine combustor mixer |
| 11/30/2005 | EP1600615A2 Intercooler system for gas turbine engines |
| 11/30/2005 | EP1600614A2 Lubrication system for gas turbine |
| 11/30/2005 | EP1600608A2 Device and method to extend impingement cooling |
| 11/30/2005 | EP1600607A2 Device to control the radial clearance of the rotor of a gas turbine |
| 11/30/2005 | EP1600605A2 Cooled rotor blade |
| 11/30/2005 | EP1600604A1 Cooler rotor blade and method for cooling a rotor blade |
| 11/30/2005 | EP1600518A2 Nickel aluminide coating with improved oxide stability |
| 11/30/2005 | EP1600240A1 Method for stopping off, using friction welding, of a hole in a metallic part, use of a metallic bar and a support assembly for performing the method. |
| 11/30/2005 | EP1599663A1 Control of a gas turbine with hot-air reactor |
| 11/30/2005 | EP1599657A1 Device for effecting heat transfer to rotating equipment, in particular gas turbines |
| 11/30/2005 | EP0911504B1 Combined cycle power generating plant and method of supplying cooling steam for gas turbine in same |
| 11/30/2005 | CN1703574A Combustor controller |
| 11/30/2005 | CN1703573A Atmospheric pressure combustion turbine system |
| 11/30/2005 | CN1701951A Bi-layer hvof coating with controlled porosity for use in thermal barrier coatings |
| 11/29/2005 | US6969826 repairing a compressor rear frame (CRF) of a gas turbine engine; welding a new seal flange to a compressor rear frame in a single pass using gas tungsten arc welding (GTAW) process that includes a penetration-enhancing flux |
| 11/29/2005 | US6969340 Control apparatus and control method for automatic transmission |
| 11/29/2005 | US6969237 Turbine airfoil cooling flow particle separator |
| 11/29/2005 | US6969236 Fluid-cooled mechanical face seal rotor |
| 11/29/2005 | US6969235 Air turbine starter with angular contact thrust bearing |
| 11/29/2005 | US6969233 Gas turbine engine turbine nozzle segment with a single hollow vane having a bifurcated cavity |
| 11/29/2005 | US6969232 Flow directing device |
| 11/29/2005 | US6969231 Rotary machine sealing assembly |
| 11/29/2005 | US6968991 Diffusion bond mixture for healing single crystal alloys |
| 11/29/2005 | US6968721 Method of manufacturing blade retainer and manufacturing devices therefor |
| 11/29/2005 | US6968701 Engine integrated auxiliary power unit |
| 11/29/2005 | US6968698 Gas turbine engine |
| 11/29/2005 | US6968697 Integral compressor housing of gas turbine engines |
| 11/29/2005 | US6968696 Part load blade tip clearance control |
| 11/29/2005 | US6968693 Method and apparatus for reducing gas turbine engine emissions |
| 11/29/2005 | US6968692 Fuel premixing module for gas turbine engine combustor |
| 11/29/2005 | US6968672 Collar for a combustion chamber of a gas turbine engine |
| 11/29/2005 | US6968608 Method and apparatus to decrease combustor emissions |
| 11/29/2005 | CA2123135C Aluminide - silicide coatings, coating compositions, process for coating and improved coated products |
| 11/28/2005 | CA2507977A1 Method and apparatus for operating an intercooler for a gas turbine engine |
| 11/25/2005 | CA2507192A1 Method for coating gas turbine engine components |
| 11/24/2005 | WO2005111382A1 Turbocharger support |
| 11/24/2005 | US20050260434 Bi-layer HVOF coating with controlled porosity for use in thermal barrier coatings |
| 11/24/2005 | US20050260076 Gas turbine blade cooling circuit having a cavity with a high aspect ratio |