| 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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| 08/04/2009 | US7568350 Combustion chamber for a turbomachine |
| 08/04/2009 | US7568347 Method for designing flowfield molded hypersonic inlet for integrated turbojet and ram-scramjet applications |
| 08/04/2009 | US7568335 Gas turbogroup |
| 08/04/2009 | CA2365328C Hydromechanical system for limiting engine overspeed |
| 07/30/2009 | US20090189123 Method and apparatus for a multi purpose data and engineering system 205 |
| 07/30/2009 | US20090188258 Altering a natural frequency of a gas turbine transition duct |
| 07/30/2009 | US20090188255 Combustor end cap assembly |
| 07/30/2009 | US20090188234 Shared flow thermal management system |
| 07/30/2009 | US20090188232 Thermal management system integrated pylon |
| 07/30/2009 | US20090188127 Process and System for Drying and Heat Treating Materials |
| 07/30/2009 | DE102009003377A1 Turbinengehäuse mit einem Hilfsflansch Turbine housings with a auxiliary flange |
| 07/30/2009 | DE102008060055A1 Verfahren zum Bestimmen der Notwendigkeit von mehreren Flügelreinigungsprozeduren A method for determining the necessity of a plurality of wing purification procedures |
| 07/30/2009 | CA2649087A1 Torque transmission for an aircraft engine |
| 07/29/2009 | EP2083150A1 Guiding of a shaft in a turbomachine |
| 07/29/2009 | EP2083147A1 Film cooling structure |
| 07/29/2009 | EP2083097A1 Multilayer alloy coating film, heat-resistant metal member having the same, and method for producing multilayer alloy coating film |
| 07/29/2009 | EP2082959A2 System and method for improving jet aircraft operating efficiency |
| 07/29/2009 | EP1769147B1 Method for operating a gas turbine group |
| 07/29/2009 | EP1692380A4 Hybrid vane island diffuser |
| 07/29/2009 | CN101493048A Starting-up control method for aviation fan engine in escape status |
| 07/29/2009 | CN101493047A Circulating one-pump two-stage low-grade gas internally heating type turbine engine |
| 07/29/2009 | CN101493046A Shunting two-pump two-stage low-grade gas internally heating type turbine engine |
| 07/29/2009 | CN101493045A Shunting one-pump two-stage low-grade gas internally heating type turbine engine |
| 07/29/2009 | CN101493044A One-pump one-stage low-grade gas internally heating type turbine engine |
| 07/29/2009 | CN101493043A Yao type III low-grade gas externally heating type turbine engine |
| 07/29/2009 | CN101493042A Yao type V low-grade gas externally heating type turbine engine |
| 07/29/2009 | CN101493041A Yao type I low-grade gas externally heating type turbine engine |
| 07/29/2009 | CN101493040A Yao type II low-grade gas externally heating type turbine engine |
| 07/29/2009 | CN101493039A Circulating two-pump two-stage low-grade gas externally heating type turbine engine |
| 07/29/2009 | CN101493038A Shunting two-pump two-stage low-grade gas externally heating type turbine engine |
| 07/29/2009 | CN100521604C Method and apparatus for selective data control |
| 07/29/2009 | CN100520012C Easy-to-assemble heat-screening device for connecting cooling tube and through hole |
| 07/29/2009 | CN100520011C Method and apparatus for operating gas turbine engine |
| 07/29/2009 | CN100519055C Metal object having under-pressure and single-end belt, and its mfg. method |
| 07/29/2009 | CA2651080A1 Deoiling device and turbomachine comprising this device |
| 07/28/2009 | US7566992 Method and apparatus for operation of a power station |
| 07/28/2009 | US7566356 Air/oil separation system and method |
| 07/28/2009 | US7566352 Single/multiple guards(s)/cap(s) and/or screen(s) with engine attached apparatus and/or pole with rotational system(s)-centrifuge chamber/manifold particle collector |
| 07/28/2009 | US7565806 Method and system for supplying an air separation unit by means of a gas turbine |
| 07/28/2009 | US7565793 Gas turbine engine fuel control system having start / back up check valve (SBUC) providing a main fuel check valve function |
| 07/28/2009 | CA2425982C Uninterruptible oil supply system |
| 07/28/2009 | CA2347059C Gas turbine electric power generation equipment and air humidifier |
| 07/25/2009 | CA2651013A1 Mounting of a turbojet engine on an aircraft |
| 07/25/2009 | CA2644383A1 Effusion cooling for gas turbine combustors |
| 07/23/2009 | WO2009089921A2 Gas turbine engine with fuel booster |
| 07/23/2009 | US20090183512 Mounting system for a gas turbine engine |
| 07/23/2009 | US20090183511 Swozzle design for gas turbine combustor |
| 07/23/2009 | US20090183491 Internal continuous combustion engine system |
| 07/23/2009 | DE102008055529A1 Thermisch isolierte Flanschschraubbolzen Thermally insulated Flanschschraubbolzen |
| 07/23/2009 | DE102008014621A1 Soot deposit cleaning method for variable geometry turbocharger of internal combustion driven system, involves determining turbocharger motor effort for predetermined calibrated maximum number of cycles according to specific formula |
| 07/23/2009 | CA2651052A1 Hanging of a propulsion system from a structural element of an aircraft |
| 07/23/2009 | CA2650771A1 Centering a part inside a shaft |
| 07/23/2009 | CA2650767A1 Guiding a shaft in a turbomachine |
| 07/22/2009 | EP2080880A1 Arrangement of a semi-conductor spark plug in a combustion chamber of a gas-turbine engine |
| 07/22/2009 | EP2080879A2 Mounting system for a gas turbine engine |
| 07/22/2009 | EP2080878A1 Gas turbine power generation system and method of detecting its calorie abnormality |
| 07/22/2009 | EP2079901A1 Turbomachine and method for turning a turbomachine |
| 07/22/2009 | CN201277095Y Fuel oil reversal valve in engine control system |
| 07/22/2009 | CN201277094Y Ground combustion machine based on aircraft engine modification |
| 07/22/2009 | CN101490392A Air intake for an aircraft turbine engine |
| 07/22/2009 | CN101490391A Joint between composite material components for turbine engine of aircraft |
| 07/22/2009 | CN101490390A Turbine engine for aircraft |
| 07/22/2009 | CN101487421A Oil seal control device for aviation turbofan engine in deplaning state |
| 07/22/2009 | CN100516757C Heat exchanger with header tubes |
| 07/22/2009 | CN100515670C Method and device for removing materials from bottom of gas turbine disc dovetail grooves |
| 07/21/2009 | US7563527 Fuel cell-atmospheric-pressure turbine hybrid system |
| 07/21/2009 | US7562532 Method for operating a gas turbine group |
| 07/21/2009 | US7562519 Gas turbine engine with an air cooled bearing |
| 07/18/2009 | CA2643956A1 Transition scrolls for use in turbine engine assemblies |
| 07/16/2009 | WO2009088031A1 Cooling structure of turbine blade |
| 07/16/2009 | WO2009087847A1 Exhaust section structure of gas turbine and gas turbine |
| 07/16/2009 | US20090180861 Cooling arrangement for turbine components |
| 07/16/2009 | US20090178414 Flame holder for minimizing combustor screech |
| 07/16/2009 | US20090178413 Article including environmental barrier coating system |
| 07/16/2009 | US20090178411 Fuel nozzle enclosure |
| 07/16/2009 | US20090178410 Thermally conductive structure |
| 07/16/2009 | US20090178385 Arrangement of a semiconductor-type igniter plug in a gas turbine engine combustion chamber |
| 07/16/2009 | US20090178383 Recoatable exhaust liner cooling arrangement |
| 07/16/2009 | DE102008055590A1 Turbinenschaufel-Deckband Turbine blade shroud |
| 07/15/2009 | EP2078825A2 Turbocharger |
| 07/15/2009 | EP2077963A2 Gas turbine nacelle comprising a passive boundary layer bleed system and method of controlling turbulent airflow |
| 07/15/2009 | CN101481262A Process for modifying the surface of a ceramic core |
| 07/14/2009 | US7559203 Cooled support boss for a combustor in a gas turbine engine |
| 07/14/2009 | US7559202 Reduced thermal stress fuel nozzle assembly |
| 07/14/2009 | CA2477402C Converging pin cooled airfoil |
| 07/09/2009 | WO2009086190A2 Gas turbine systems and methods employing a vaporizable liquid delivery device |
| 07/09/2009 | WO2009085843A2 Ice protection system for a multi-segment aircraft component |
| 07/09/2009 | WO2009085580A2 Turbine nozzle segment and method for repairing a turbine nozzle segment |
| 07/09/2009 | WO2009085380A2 Low shock strength inlet |
| 07/09/2009 | WO2009084587A1 Combustor of gas turbine |
| 07/09/2009 | WO2009083691A1 Aircraft propulsion assembly comprising hot air bleed systems |
| 07/09/2009 | US20090173081 Method and apparatus to facilitate substitute natural gas production |
| 07/09/2009 | US20090173076 Fuel injector |
| 07/09/2009 | US20090173075 Burner and gas turbine combustor |
| 07/09/2009 | DE102008055593A1 Verfahren und Systeme zur neuronalen Netzwerkmodellierung von Turbinenkomponenten Methods and systems for neural network modeling of turbine components |
| 07/09/2009 | CA2710445A1 Aircraft propulsion assembly comprising hot air bleed systems |
| 07/09/2009 | CA2709932A1 Turbine nozzle segment and method for repairing a turbine nozzle segment |
| 07/09/2009 | CA2703748A1 Low shock strength inlet |
| 07/08/2009 | EP2077379A2 High voltage start of an engine from a low voltage battery |
| 07/08/2009 | EP1540157A4 Improved fuel delivery system |