Patents for F01D 21 - Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for (3,351) |
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10/06/2005 | US20050218887 Wear monitor for turbo-machine |
10/06/2005 | US20050218261 Air intake structure for aircraft engine |
10/05/2005 | EP1582702A1 Air intake structure for an airplane engine |
10/05/2005 | EP1582701A1 Air intake structure for an airplane engine |
10/05/2005 | EP1581732A1 Corrected parameter control method for a two-shaft gas turbine |
09/29/2005 | CA2500963A1 Air intake structure for aircraft engine |
09/27/2005 | US6949922 Turbine blade clearance on-line measurement system |
09/22/2005 | WO2005086864A2 Power trailer structural elements for air flow, sound attenuation and fire supression |
09/22/2005 | US20050207882 Air circulating apparatus |
09/22/2005 | US20050204740 System and method of cooling steam turbines |
09/21/2005 | EP1577492A1 Method and apparatus for establishing the state of the rotor of a turbomachine |
09/21/2005 | CN1670347A Turbo-jet engine with fan integral with a drive shaft supported by first and second bearings |
09/20/2005 | US6945124 Measurement system |
09/15/2005 | US20050201611 Non-contact measurement method and apparatus |
09/15/2005 | DE102004009595A1 Verfahren und Vorrichtung zur Identifikation eines Wellenbruchs und/oder einer Überdrehzahl an einer Gasturbine Method and apparatus for identification of a shaft break and / or an overspeed of a gas turbine |
09/14/2005 | EP1574818A2 Non-contact measurement method and apparatus |
09/14/2005 | EP1032811B1 Velocity adaptive control test method |
09/14/2005 | CN1668829A Method and device for regulating the rotational speed of a turbine connected to an electric power supply mains by means of a generator |
09/13/2005 | US6942450 Differential pressure sensing system for airfoils usable in turbine engines |
09/09/2005 | WO2005083237A1 Method and device for identifying a shaft fracture and/or an excessive rotational speed in a gas turbine |
09/08/2005 | US20050193715 Shut-off system for the avoidance of an overspeed condition in the event of a shaft failure |
09/06/2005 | US6941217 Microprocessor-based control system for gas turbine electric powerplant |
09/01/2005 | WO2005080937A1 Non-destructive monitoring of microstructural modifications of a component (layer system, turbine blades, combustion chamber lining) by means of special, simple test methods |
09/01/2005 | US20050191755 Evaluating oxide layer on components of hot CO2/H2O gas turbines; predicting metal fatigue |
08/24/2005 | EP1566523A2 A gas turbine engine blade containment assembly |
08/24/2005 | EP1565655A1 Compressor impeller |
08/23/2005 | US6932560 Apparatus and method for detecting an impact on a rotor blade |
08/17/2005 | EP1564559A1 Signal processing method and apparatus |
08/17/2005 | EP1564537A1 Non destructive monitoring of microstructure changes of a component ( layer system, turbine blades, liners of a combustion chamber ) |
08/17/2005 | EP1564405A1 Test bench for wind turbines |
08/17/2005 | EP1564352A2 Two bearings supported fan shaft in a turbofan engine |
08/17/2005 | EP1563168A1 Turbocharger |
08/11/2005 | WO2005073667A1 Inductive apparatus and method for measuring compressor blade tip clearance in a gas turbine engine |
08/11/2005 | US20050175477 Turbocharger |
08/11/2005 | US20050172729 Test bench for wind turbines |
08/11/2005 | US20050172608 Turbo-jet engine with fan integral with a drive shaft supported by first and second bearings |
08/10/2005 | EP1561907A1 Turboreactor with fan mounted on a drive shaft supported by a first and a second bearing |
08/10/2005 | CN2716510Y Nanosecond class steam turbine emergency trip control device |
08/10/2005 | CN1651746A Methods and apparatus for assembling gas turbine engines |
08/09/2005 | US6925883 Non resonating close coupled probe |
08/04/2005 | WO2005052341A8 Procedure for controlling the useful life of the gas turbines of a plant |
08/04/2005 | DE102004001262A1 Process for depositing a fiber forming element in an open rotationally symmetrical recess on a radial inside end of a component useful in gas turbine technology |
08/03/2005 | EP1558938A2 Turbo engine |
08/03/2005 | CN1650092A Turbo charger with means on the shaft for axially securing of said shaft if the compressor wheel bursts |
07/27/2005 | EP1557538A2 Fan platform for a gas turbine engine |
07/26/2005 | CA2196243C Bearing arrangement for rotating members |
07/21/2005 | US20050155342 Methods and apparatus for assembling gas turbine engines |
07/21/2005 | DE19618313B4 Axialturbine eines Abgasturboladers An axial turbine of an exhaust turbocharger |
07/20/2005 | EP1555395A1 Throttle control system for engine test bench |
07/19/2005 | US6918747 Method and system for detecting damage to the rotor of an aircraft engine |
07/14/2005 | US20050152776 Comprising a shaft end associated with a compressor; used with regard to intermediate pressure compressors of a turbine engine |
07/14/2005 | US20050152626 Bearing support with double stiffener |
07/14/2005 | US20050150206 Throttle control device in particular for turbine aero engine test bench |
07/13/2005 | EP1553324A1 Bearing support with double stiffness |
07/12/2005 | CA2365301C Life management system for high-temperature parts of gas turbine |
07/05/2005 | US6914215 Real time laser shock peening quality assurance by natural frequency analysis |
07/05/2005 | US6913436 Gas turbine engine blade containment assembly |
06/29/2005 | EP1547023A1 Method and device for determination of the condition of a turbine blade, and utilizing the collected information for estimation of the lifetime of the blade |
06/28/2005 | US6910278 Apparatus and method for inspecting and marking repair areas on a blade |
06/16/2005 | WO2005054873A1 Rotation sensor and sensing method |
06/16/2005 | WO2005054646A1 Gas turbine protection device |
06/16/2005 | US20050129498 Apparatus and method for detecting an impact on a rotor blade |
06/16/2005 | US20050129343 Arrangement of bearing supports for the rotating shaft of an aircraft engine and an aircraft engine fitted with such an arrangement |
06/16/2005 | US20050126183 Combustion temperature high speed detection device |
06/15/2005 | EP1540143A1 Rotor recentring after decoupling |
06/09/2005 | WO2005052341A1 Procedure for controlling the useful life of the gas turbines of a plant |
06/09/2005 | US20050122095 Rotation sensor and method |
06/08/2005 | CN2703873Y Oil-way main-break protective velve assembly for steam turbine safety system |
06/02/2005 | US20050117828 Breakable coupling system for a turbojet fan shaft |
06/01/2005 | EP1534936A1 Fan case design with metal foam between kevlar |
06/01/2005 | EP1534935A1 Energy absorber and deflection device |
05/31/2005 | US6899519 Method of detecting a change in the structure of a complex shape article |
05/31/2005 | US6899514 Overspeed safety device |
05/31/2005 | US6898939 Methods for rotor overspeed and overboost protection |
05/31/2005 | US6898935 System and method of cooling steam turbines |
05/26/2005 | US20050109038 Method and apparatus for controlling fuel flow to an engine |
05/25/2005 | EP1533479A2 Method and apparatus for detecting rub in a turbomachine |
05/24/2005 | US6898547 Rotor assembly system and method |
05/19/2005 | US20050106002 Fan blade with embrittled tip |
05/17/2005 | US6892540 System and method for controlling a steam turbine |
04/28/2005 | US20050089391 Liner for a gas turbine engine casing |
04/28/2005 | US20050089390 Abradable device on the blower casing of a gas turbine engine |
04/26/2005 | US6883331 Method and arrangement for providing a gas turbine, and engine-braking therefore |
04/20/2005 | EP1524411A1 Method of measuring and minimising the gap between an (abradable) rotor blade and a turbine housing |
04/19/2005 | US6881024 System for decoupling a fan from a turbojet by means of an explosive charge |
04/14/2005 | US20050079048 Method of minimizing the gap between a rotating turbine blade and a casing of a turbine, a turbine, and a method of determining the wear behavior of a wheel of a rotor |
04/14/2005 | DE10340690A1 Sensor for measuring gas pressure in air inlet in front of compressor stage of a driving mechanism of an aircraft jet engine has pressure measuring line for introducing gas from chamber, and surrounded by water-repelling sensor core |
04/13/2005 | EP1522681A2 Protection system for turbo machine and power generating equipment |
04/07/2005 | US20050074328 Gas turbine engine blade containment assembly |
04/07/2005 | US20050073673 Imaging system for robotically inspecting gas turbine combustion components |
04/06/2005 | EP1520961A2 Methods for controlling lubrication oil draining in gas turbine engines |
03/31/2005 | US20050066648 Multi-mode shutdown system for a fuel metering unit |
03/30/2005 | CN1601057A Protection system for turbo machine and power generating equipment |
03/29/2005 | CA2284474C Combined cycle electric power plant |
03/23/2005 | EP1517007A2 Electrically operated remote trip mechanism and method of shutting down a steam turbine |
03/22/2005 | US6868663 Gas turbine plant with high detection sensitivity of extraordinary state |
03/17/2005 | US20050058536 Rotor brake as well as rotor and rotary-wing aircraft with such a rotor brake |
03/17/2005 | DE10353620B3 Sensor monitoring method for rotating machine e.g. for axial turbocompressor for jet propulsion drive or gas turbine, using ultrasonic pulses for detecting rotor parameters and air temperature between stator and rotor |
03/16/2005 | EP1515005A2 Joint arrangement in particular for turbofan engines |
03/16/2005 | EP1514018A1 A turbine and a component |