| 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) |
|---|
| 09/29/2005 | US20050211822 Variable cycle propulsion system with gas tapping for a supersonic airplane, and a method of operation |
| 09/29/2005 | US20050211096 Fuel deoxygenation system |
| 09/29/2005 | US20050211093 Air/oil separation system and method |
| 09/29/2005 | US20050210880 Gas turbine combustor and operating method thereof |
| 09/29/2005 | US20050210864 Device for supplying cooling air to exhaust nozzle flaps |
| 09/29/2005 | CA2560633A1 Air/oil separation system and method |
| 09/29/2005 | CA2500963A1 Air intake structure for aircraft engine |
| 09/28/2005 | EP1580414A2 Turbomachine component with cooling arrangement |
| 09/28/2005 | EP1580401A2 Sealing for transition between cooling passages of two turbomachine components |
| 09/28/2005 | EP1580124A1 Aircraft engine mount |
| 09/28/2005 | EP1579960A1 Method of removing ring-locked studs |
| 09/28/2005 | EP1579902A1 Fuel deoxygenation system |
| 09/28/2005 | EP1579901A1 Method of suppressing coke in endothermic fuel processing |
| 09/28/2005 | EP1185766B1 Concentricity ring |
| 09/28/2005 | CN1675502A Gas turbine combustion chamber |
| 09/28/2005 | CN1675457A 改进的燃料输送系统 Improved fuel delivery system |
| 09/28/2005 | CN1673512A Metal sheet comprising means for fixing to a support and a seal |
| 09/28/2005 | CN1673502A Extended operability aircraft fuel delivery system |
| 09/28/2005 | CN1673491A Soldering structure and soldering method for machinable seal structual parts |
| 09/28/2005 | CN1673034A Fuel deoxygenation system |
| 09/28/2005 | CN1672778A Method of suppressing coke in endothermic fuel processing |
| 09/28/2005 | CN1220845C Flanged hollow structure |
| 09/27/2005 | US6948919 Hermetic motor and gas booster |
| 09/27/2005 | US6948909 Formed disk plate heat exchanger |
| 09/27/2005 | US6948558 Evaporative duplex counterheat exchanger |
| 09/27/2005 | US6948437 Thermal shielding brick for lining a combustion chamber wall, combustion chamber and a gas turbine |
| 09/27/2005 | US6948318 Method and installation for feeding an air separation plant with a gas turbine |
| 09/27/2005 | CA2352041C Turbine inlet scroll |
| 09/24/2005 | CA2496929A1 Fuel deoxygenation system |
| 09/22/2005 | WO2005088122A1 Apparatus and method for storing thermal energy and generating electricity |
| 09/22/2005 | WO2005088104A1 Gas turbine inlet flow straightener with restricting member |
| 09/22/2005 | WO2005088103A1 Device and method for heating a gas flow |
| 09/22/2005 | WO2005063564A3 Air guiding flap of an aircraft comprising control of the pressure forces impinging thereon, process for adjusting the position of an air guiding flap and ram air system including such an air guiding flap |
| 09/22/2005 | US20050207896 Erosion and wear resistant protective structures for turbine engine components |
| 09/22/2005 | US20050207892 Rotating blade body and rotary machine using rotating blade body |
| 09/22/2005 | US20050206343 Power generation system and control method |
| 09/22/2005 | US20050205415 Multi-component deposition |
| 09/22/2005 | US20050205351 Noise reduction tubes |
| 09/22/2005 | US20050205174 Property recovering method |
| 09/22/2005 | US20050204919 Method of suppressing coke in endothermic fuel processing |
| 09/22/2005 | US20050204745 Gas turbine control system |
| 09/22/2005 | US20050204743 Gas turbine inlet flow straightener |
| 09/22/2005 | US20050204741 Turbine combustor transition piece having dilution holes |
| 09/22/2005 | US20050204740 System and method of cooling steam turbines |
| 09/22/2005 | US20050204723 Steam and gas turbine installation |
| 09/22/2005 | US20050204533 Method of removing studs |
| 09/22/2005 | US20050204489 Rotary probe for cleaning an internal cavity |
| 09/22/2005 | DE102005008509A1 Laufschaufelkörper und Rotationsmaschine mit einem Laufschaufelkörper Blade body and rotating machine with a blade body |
| 09/22/2005 | DE102004059560A1 Rotor injector valve for thermal turbo-engines in a fuel supply system in a rotor air mass measuring device comprises a rotor impeller fixed or rotatably arranged upstream |
| 09/22/2005 | DE102004010422A1 Dichtungskörper Seal body |
| 09/22/2005 | CA2500678A1 Method of removing studs |
| 09/22/2005 | CA2497129A1 Method of suppressing coke in endothermic fuel processing |
| 09/21/2005 | EP1577549A1 Apparatus for storing thermal energy and generating electricity |
| 09/21/2005 | EP1577548A1 Apparatus and method for storing thermal energy and generating electricity |
| 09/21/2005 | EP1577506A1 Axial maintenance device to support the strut of a stator ring of the high-pressure turbine of a turbomachine |
| 09/21/2005 | EP1577505A2 Support bracket for turboprop engine nozzle |
| 09/21/2005 | EP1577501A1 High pressure turbine stator of a turbo-engine and his assembling process |
| 09/21/2005 | EP1577500A2 Turbine transition duct having dilution holes |
| 09/21/2005 | EP1577499A2 Turbine components with thermal barrier coatings |
| 09/21/2005 | EP1577498A1 Microcircuit cooling for a turbine airfoil |
| 09/21/2005 | EP1577495A1 Turbomachine rolling bearing assembly having a reduced space requirement |
| 09/21/2005 | EP1577422A1 Erosion and wear resistant protective structures for turbine engine components |
| 09/21/2005 | EP1577417A1 Multi-component deposition |
| 09/21/2005 | EP1577027A1 Rotary probe for cleaning an internal cavity |
| 09/21/2005 | EP1576267A1 Gas turbine power plant |
| 09/21/2005 | EP1427915B1 Turbine no-load speed limiter |
| 09/21/2005 | EP1301697B1 Gas turbine and method for operating a gas turbine |
| 09/21/2005 | EP1234144B1 Simple low cost fuel nozzle support |
| 09/21/2005 | CN1671956A System for cooling cooling air in a gas turbine, and method for cooling cooling air |
| 09/21/2005 | CN1671465A Evaporative duplex counterheat exchanger |
| 09/21/2005 | CN1670433A Turbine transition duct having dilution holes |
| 09/21/2005 | CN1670349A Gas turbine engine component having bypass circuit |
| 09/21/2005 | CN1670348A Controlled pressure fuel nozzle system |
| 09/21/2005 | CN1670347A Turbo-jet engine with fan integral with a drive shaft supported by first and second bearings |
| 09/21/2005 | CN1670337A Turbine components with thermal barrier coatings |
| 09/21/2005 | CN1670336A Microcircuit cooling for a turbine airfoil |
| 09/21/2005 | CN1670253A Multi-component deposition |
| 09/21/2005 | CN1219995C Burner apparatus for burning fuel and air |
| 09/20/2005 | US6945494 Variable position intake for an aircraft mounted gas turbine engine |
| 09/20/2005 | US6945030 Gas turbine control system |
| 09/20/2005 | CA2228777C Gasket with stacked leaves sliding in receiving slots |
| 09/19/2005 | CA2500933A1 Multi-component deposition |
| 09/18/2005 | CA2498486A1 Rotating shaft scavenging scoop |
| 09/18/2005 | CA2498459A1 Gas turbine inlet flow straightener |
| 09/17/2005 | CA2500753A1 Turbine components with thermal barrier coatings |
| 09/16/2005 | CA2497755A1 Microcircuit cooling for a turbine airfoil |
| 09/15/2005 | WO2005085721A1 Silencer for ventilation system and methods |
| 09/15/2005 | WO2005085622A1 Exhaust-gas turbocharger for internal combustion engine |
| 09/15/2005 | WO2005085615A1 Radial turbine and method of cooling nozzle of the same |
| 09/15/2005 | WO2005085606A1 Cylinder head cover with oil separator |
| 09/15/2005 | WO2005084780A1 A fluid separation device |
| 09/15/2005 | WO2005084779A1 Oil separator |
| 09/15/2005 | WO2005060371A3 Common radial plane motor cooling |
| 09/15/2005 | WO2005059331A3 Bearing system for high-speed rotating machinery |
| 09/15/2005 | US20050201859 Gas turbine ventilation circuitry |
| 09/15/2005 | US20050201857 Mounting arrangement for turbine blades |
| 09/15/2005 | US20050200349 Method and apparatus of determining gas turbine shaft speed |
| 09/15/2005 | US20050200336 Method for acceleration of a shaft run, as well as an apparatus for carrying out the method |
| 09/15/2005 | US20050199840 High recovery sonic gas valve |
| 09/15/2005 | US20050199683 Method of joining material |