| 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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| 06/27/2001 | EP1111219A2 Mounting an igniter in an augmenter |
| 06/27/2001 | EP1111195A1 A structured surface used as grazing layer in turbomachines |
| 06/27/2001 | EP1111194A2 Composite abradable material |
| 06/27/2001 | EP1111189A2 Cooling air path for the rotor of a gas turbine engine |
| 06/27/2001 | EP1111091A1 Method of forming an active-element containing aluminide as stand alone coating and as bond coat and coated article |
| 06/27/2001 | EP1111085A1 Method for producing ceramic coatings |
| 06/27/2001 | EP1109948A1 Multilayer thermal barrier coating systems |
| 06/26/2001 | US6251504 Ceramic heat barrier coating having low thermal conductivity, and process for the deposition of said coating |
| 06/26/2001 | US6251315 Method for disposing a laser blocking material on the interior of an airfoil |
| 06/26/2001 | US6251270 Fuel circuit with protected main filter |
| 06/26/2001 | US6250894 Load sharing valve and system for operating centrifugal pumps in parallel |
| 06/26/2001 | US6250878 Method and assembly for connecting air ducts in gas turbine engines |
| 06/26/2001 | US6250082 Combustor rear facing step hot side contour method and apparatus |
| 06/26/2001 | US6250068 Gas turbine installation |
| 06/26/2001 | US6250065 Gas turbine combustion system and combustor ignition method therefor |
| 06/26/2001 | US6250064 Gas turbine inlet air integrated water saturation and supersaturation system and related process |
| 06/26/2001 | US6250063 Fuel staging apparatus and methods for gas turbine nozzles |
| 06/26/2001 | US6250061 Compressor system and methods for reducing cooling airflow |
| 06/26/2001 | CA2229324C Gas turbine tip shroud blade cavity |
| 06/21/2001 | US20010004436 Profiled surface used as an abradable in flow machines |
| 06/21/2001 | US20010003897 Device for discharging hot air for a jet engine air inlet cowl, with a deicing circuit |
| 06/21/2001 | DE19961565A1 Coolant flow at a turbine paddle is adjusted by an inserted body into an opening in the coolant channel which reduces its cross section to give the required coolant flow vol |
| 06/21/2001 | DE19961014A1 Starter for compact jet engine has motor mounted on extension of turbine shaft so as to transfer required torque via centrifugal force and/or overrun coupling to turbine shaft |
| 06/21/2001 | DE19959485A1 Exhaust gas turbocharger lubricating oil parameter control/regulation system determines control value from control parameter determined by sensor, sets value via regulating devices |
| 06/20/2001 | EP1108870A2 Process and apparatus for achieving power augmentation in gas turbines via wet compression |
| 06/20/2001 | EP1108858A2 Double wall bearing cone |
| 06/20/2001 | EP1108857A2 Abradable seal |
| 06/20/2001 | EP1108129A2 Control systems and methods for water injection in a turbine engine |
| 06/20/2001 | EP1108117A1 Microturbine power generating system including variable-speed gas compressor |
| 06/20/2001 | EP1107867A1 Removal of thermal barrier coatings |
| 06/20/2001 | CN1299927A Magnetic fluid accelerator and magnetic fluid jet engine therewith |
| 06/20/2001 | CN1067460C Pumping device |
| 06/19/2001 | US6247895 Locking member for processing a flow directing assembly |
| 06/19/2001 | US6247302 Gas turbine power plant |
| 06/19/2001 | US6247300 Gas turbine engine |
| 06/19/2001 | US6247299 Method for feeding a gas turbine with both liquid and gaseous fuels |
| 06/14/2001 | WO2001043119A1 A device at an acoustic liner |
| 06/14/2001 | WO2001042631A1 Exhaust system |
| 06/14/2001 | US20010003242 Gas turbine generator plant |
| 06/13/2001 | EP1106928A1 Fuel system configuration and method for staging fuel for gas turbines utilizing both gaseous and liquid fuels |
| 06/13/2001 | EP1105622A1 Mismatch proof variable stator vane |
| 06/13/2001 | CN1299436A Gas and steam turbine installation |
| 06/13/2001 | CN1299435A High efficiency low pollution hybrid brayton cycle combustor |
| 06/13/2001 | CN1299032A Shaping method and apparatus for stairs-like heating side of hurner back lining |
| 06/12/2001 | US6244818 Fan guard structure for additional supercharging function |
| 06/12/2001 | US6244037 Method of operating a combustion turbine using supplemental compressed air |
| 06/12/2001 | US6244036 Control for augment mode JP-air emergency power unit |
| 06/12/2001 | US6244035 Gas and steam-turbine plant and method of operating the plant |
| 06/12/2001 | US6244034 Compressor bleed pressure storage for controlled fuel nozzle purging of a turbine power generating system |
| 06/07/2001 | WO2001040710A1 Simple low cost fuel nozzle support |
| 06/07/2001 | WO2001040548A1 Chemical cleaning solution for gas turbine blades |
| 06/06/2001 | EP1104872A1 Method for decreasing a heat load on a combustor liner |
| 06/06/2001 | EP1104871A1 Combustion chamber for a gas turbine engine |
| 06/06/2001 | CN1066823C High temperature detecting head |
| 06/06/2001 | CN1066799C Cooling method of heating parts of gas turbine |
| 06/05/2001 | US6242715 Progressive hot twisting apparatus for use in a process for manufacturing a hollow turbomachine blade |
| 06/05/2001 | US6241189 Protective device for a jet engine air inlet cowl equipped with a deicing system |
| 06/05/2001 | US6240859 Cement, reduced-carbon ash and controlled mineral formation using sub- and supercritical high-velocity free-jet expansion into fuel-fired combustor fireballs |
| 06/05/2001 | US6240732 Fluid manifold |
| 06/05/2001 | US6240719 Fan decoupler system for a gas turbine engine |
| 05/31/2001 | WO2001038727A2 Induction static start for a turbine generator with a brushless exciter and associated methods |
| 05/31/2001 | WO2001038707A1 Gas turbine equipment, gas turbine sealing device, and gas turbine cooling air leakage suppressing method |
| 05/31/2001 | WO2001038699A1 Sequential use of steam |
| 05/31/2001 | WO2001037968A1 Engine with upstream and rotationally attached guard |
| 05/31/2001 | WO2001020148A3 Variable speed fuel pumping system for a gas turbine and method of operation |
| 05/31/2001 | WO2000068461A3 Thermal barrier coating |
| 05/31/2001 | DE19956919A1 Gasturbinen-Triebwerk mit einer Lagerkammer Gas turbine engine with a storage chamber |
| 05/30/2001 | EP1103706A2 Bearing chamber for a gas turbine engine |
| 05/30/2001 | EP1103699A2 Gas turbine combined cycle system |
| 05/30/2001 | EP1103628A2 A coating system for providing environmental protection to a metal substrate |
| 05/30/2001 | EP1103627A2 Method for thermal barrier coating |
| 05/30/2001 | EP1103462A1 Method and apparatus for aircraft inlet ice protection |
| 05/30/2001 | EP1102926A1 Fuel gas turbo-expander for oxygen blown gasifiers and related method |
| 05/29/2001 | US6238743 Removal yttria-stabilized zirconia layer on gas turbine engine; using aqueous solution of ammonium bifluoride |
| 05/29/2001 | US6238520 Manufacture of paper |
| 05/29/2001 | US6237344 Dimpled impingement baffle |
| 05/29/2001 | US6237337 Retrofit equipment for reducing the consumption of fossil fuel by a power plant using solar insolation |
| 05/29/2001 | US6237322 Oil pump |
| 05/29/2001 | US6237320 Removal of inert gases from process gases prior to compression in a gas turbine or combined cycle power plant |
| 05/29/2001 | CA2246218C Gas turbine combustor |
| 05/29/2001 | CA2229317C Cooling medium path structure for gas turbine blade |
| 05/25/2001 | WO2001036790A1 Turbine blade and method for producing a turbine blade |
| 05/25/2001 | WO2001036566A1 System and method for oil fuel burning integrated combined cycle power generation |
| 05/24/2001 | US20010001680 A metal piece having a cooling hole along a central axis, includes spraying a bond coat and a thermal barrier coating (TBC) on the bond coat; fluid jet of particulate free water removes bond coat and TBC from hole without removing metal |
| 05/23/2001 | EP1101902A2 Damped torque shaft assembly |
| 05/23/2001 | EP1101897A2 Methods for disassembling, replacing and assembling parts of a steam cooling system for a gas turbine |
| 05/23/2001 | EP1101833A1 Repair of coated turbine components |
| 05/23/2001 | EP1101024A1 Quasi-isothermal brayton cycle engine |
| 05/23/2001 | DE10009655C1 Air cooling system for the paddles of a high pressure gas turbine has flow chambers at each paddle for the leading and trailing edges and the center profile with a heat exchanger to cool the air flow to the paddle edges |
| 05/23/2001 | CN1295900A Turbine inlet guiding section and repairing method thereof |
| 05/22/2001 | US6234746 Apparatus and methods for cooling rotary components in a turbine |
| 05/22/2001 | US6233940 Dual-pressure stem injection partial-regeneration-cycle gas turbine system |
| 05/22/2001 | US6233917 Method of controlling the temperature of intake air, temperature-control device for carrying out the method and gas turbine having the temperature-control device |
| 05/22/2001 | US6233822 Repair of high pressure turbine shrouds |
| 05/17/2001 | WO2001034956A1 Gas turbine equipment and gas turbine cooling method |
| 05/17/2001 | WO2001034955A1 Method for optimizing industrial gas turbine operation subject to emissions controls |
| 05/17/2001 | WO2001034278A1 Filter arrangement and methods |
| 05/17/2001 | US20010001171 Coal gasification combined cycle power generation plant and an operating method thereof |
| 05/17/2001 | CA2390663A1 Filter arrangement and methods |
| 05/16/2001 | EP1099825A1 Turbine blade and production method therefor |