Patents
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)
06/2008
06/17/2008CA2356766C Method and apparatus for supporting rotor assemblies during unbalances
06/12/2008WO2008068098A1 Method and apparatus for conditioning sensor signals for the purpose of inductively measuring a turbocharger speed
06/10/2008US7383679 Air intake structure for aircraft engine
06/04/2008EP1927731A2 Methods for making structures having mounting flanges
06/04/2008EP1927728A2 Methods for reducing stress on composite structures
06/04/2008EP1700019B1 Procedure for controlling the useful life of the gas turbines of a plant
05/2008
05/29/2008DE102007052831A1 Turbokompressor-Abschaltmechanismus Turbo Compressor shutdown
05/28/2008EP1926001A2 Reducing gas turbine performance tracking estimation non-repeatability
05/28/2008CN101187317A Corrected parameter control method for a two-shaft gas turbine
05/22/2008WO2008060164A1 A method and a device for detection of rubbing between a stator and a rotor of a turbo-machine
05/21/2008EP1923633A2 Active combustion control system for gas turbine engines
05/21/2008EP1922472A1 Gas turbine comprising a unit for detecting a shaft rupture
05/21/2008DE102006051342A1 Safety and/or control device for turbine i.e. exhaust gas turbine, has switchable dissipative unit for discharging portion of power delivered from turbine, where unit includes throttle point arranged in fluid passage between pump and motor
05/20/2008US7373823 Method for determination of the stress on blades of a turbine machine during operation and corresponding device for carrying out said method
05/15/2008WO2008055717A1 Housing connection of an exhaust gas turbocharger
05/15/2008CA2608304A1 Assembly procedure for the adjustable pin-valve, fuel shut-off
05/14/2008EP1921274A1 Overspeed limitation device for the turbine of a turbomachine and corresponding turbomachine
05/08/2008US20080107518 Method for Determining a Parameter Characteristic of the Fatigue State of a Part
05/08/2008DE102006052498A1 Sicherungsring für das Fangehäuse eines Gasturbinentriebwerks Retaining ring for the fan casing of a gas turbine engine
05/07/2008EP1918531A2 Containment ring for the fan case of a gas turbine engine
05/07/2008EP1918530A2 Method and system for testing the overspeed protection system of a turbomachine
05/07/2008CN201057059Y Multifunctional steam turbine overspeed protection forwork capable of accurate measuring low revolution speed
05/07/2008CN101173617A Method and system for testing the overspeed protection system of a turbomachine
05/06/2008US7369965 System and method for turbine engine anomaly detection
05/06/2008US7367774 System for protecting a main shaft of an engine having a fusible bearing
05/06/2008CA2467710C Gas turbine engine broken shaft detection system
05/06/2008CA2453665C Turbine controls testing device
05/02/2008WO2008049716A2 Method for determining the rotational speed of a turbocharger of an internal combustion engine, and internal combustion engine
05/01/2008US20080101917 Device for limiting turbine overspeed in a turbomachine
04/2008
04/30/2008EP1916391A1 Method and device for reducing speed in the event of breakage of the turbine shaft of a gas-turbine engine
04/30/2008EP1915639A1 Method for determining the layer thickness of a tbc coating of at least one blade of a non-positive-displacement machine, a corresponding tbc layer thickness measuring device for carrying out the method and use of the method and the tbc layer thickness measuring device
04/30/2008EP1759092B1 Device for detecting a fracture in the shaft of a gas turbine, and gas turbine
04/30/2008CN100385092C Rapid power producing system and method for steam turbine
04/30/2008CA2608267A1 Device for limiting turbine overspeed in turbomachinery
04/26/2008CA2607245A1 Bearing arrangement of a rotating shaft and turbojet equipped with such an arrangement
04/25/2008CA2607244A1 Method for reducing speed in the case of the breakage of a turbine shaft in a gas turbine engine
04/24/2008WO2008048290A1 Direct acting hydraulic trip block with majority voting
04/24/2008CA2662456A1 Direct acting hydraulic trip block with majority voting
04/23/2008CN100383505C High speed detecting equipment for combustion temperature
04/22/2008US7360986 System for blocking a main shaft of an engine having a fusible bearing
04/22/2008CA2352852C Impeller containment system
04/17/2008WO2008045080A1 Variable area fan nozzle for accommodating a foreign object strike event
04/17/2008WO2008045068A1 Turbofan engine with variable area fan nozzle and low spool generator for emergency power generation and method for providing emergency power.
04/17/2008WO2008045066A1 Controlling the aerodynamic drag of a gas turbine engine during a shutdown state
04/17/2008WO2008045052A1 Method and device to avoid turbofan instability in a gas turbine engine
04/17/2008US20080087339 Direct acting hydraulic trip block
04/16/2008CN101163863A Fan case reinforcement in a gas turbine jet engine
04/10/2008US20080083228 Apparatus, system and method for observing combustion conditions in a gas turbine engine
04/10/2008DE102004002712B4 Turbinenschaufel-Ermüdungslebensdauer-Bewertungsverfahren und Turbinenschaufel-Kriechdehnungsverformungs-Messvorrichtung Turbine blade fatigue life assessment procedures and turbine blade Kriechdehnungsverformungs measuring device
04/09/2008CN100379940C Fan vane with same shape as its seat
04/02/2008CA2602994A1 Annular gas turbine engine case and method of manufacturing
04/02/2008CA2602981A1 Annular gas turbine engine case and method of manufacturing
04/02/2008CA2601659A1 Annular gas turbine engine case and method of manufacturing
04/01/2008CA2329715C Containment system for containing blade burst
03/2008
03/25/2008CA2602319A1 Blade containment system for a gas turbine engine
03/20/2008US20080069685 Device for Detecting a Fracture in the Shaft of a Gas Turbine, and Gas Turbine
03/18/2008US7344362 Turbocharger
03/13/2008US20080063508 Fan case abradable
03/11/2008US7340882 Turbomachine with means for axial retention of the rotor
03/06/2008WO2008003571A3 Method for operating a gas turbine and gas turbine for carrying out said method
03/04/2008US7338250 Gas turbine engine blade containment assembly
02/2008
02/28/2008US20080049887 Method for Monitoring the State of Turbines Based on their Coasting Time
02/27/2008EP1891449A1 Magnet orientation and calibration for small package turbocharger speed sensor
02/27/2008EP1891335A2 Radial fan
02/27/2008CN201027550Y Vapor driven draught fan interlocking system of phthalic anhydride apparatus
02/26/2008US7334413 Apparatus, system and method for observing combustion conditions in a gas turbine engine
02/20/2008EP1890012A1 Method for running a gasturbine
02/20/2008EP1547023B1 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
02/20/2008CN100370117C Online controlling method for steam turbine rotator equivalent stress safety margin coefficient
02/20/2008CN100370116C controlling method for steam turbine high and medium pressure rotator equivalent stress
02/14/2008WO2008017519A1 Method for operating a turbine
02/14/2008US20080038108 Axial Flow Turbine with Overspeed Preventing Device
02/13/2008EP1886000A1 Detection of gas turbine airfoil failure
02/07/2008US20080031721 Fan variable immersion system
02/06/2008EP1884639A2 Ice strike sheathing ring for the fan casing of an aircraft engine
02/06/2008EP1884626A2 Gas turbine stator vane comprising a probe inspection port
02/06/2008EP1883789A1 An instrumentation arrangement
02/05/2008US7327857 Non-contact measurement method and apparatus
02/04/2008CA2555480A1 Clearance measurement system and method of operation
01/2008
01/31/2008US20080025836 Overspeed Safety Device for a Rotation Motor
01/30/2008CN201013679Y Oil pressure reservoir used for steam turbine control oil pressure resistance pulsation
01/30/2008CN201013407Y Fermentation tank exhaust stream energy reclaimer
01/29/2008US7322788 Protection system for turbo machine and power generating equipment
01/29/2008US7322270 Safety circuit for media-operated consumers and process for its operation
01/29/2008US7322181 Turbofan engine with the fan fixed to a drive shaft supported by a first and a second bearing
01/29/2008US7322180 Turbo-jet engine with fan integral with a drive shaft supported by first and second bearings
01/23/2008EP1881159A1 A fan blade for a gas turbine engine
01/23/2008EP1880242A1 Endoscope with cam track for following a predetermined path
01/23/2008CN100363595C Compressor casing
01/16/2008EP1878878A2 Cooling system for a gas turbine engine
01/16/2008CN101107424A Fan case improvement in a gas turbine jet engine
01/16/2008CN101105429A Turbine blade fatigue life evaluating method
01/15/2008US7318685 Tension decoupler device
01/10/2008WO2008003571A2 Method for operating a gas turbine and gas turbine for carrying out said method
01/10/2008CA2656418A1 Method for operating a gas turbine and also gas turbine for carrying out the method
01/09/2008EP1876324A2 Gas turbine blade
01/09/2008EP1451448B1 Gas turbine engine broken shaft detection system
01/09/2008CN201003415Y Emergency governor throttle
01/03/2008WO2007035184A8 Fan case reinforcement in a gas turbine jet engine
01/03/2008DE102006049516B3 Turbo-engine, e.g. for operating as turbo-compressor, has a rotor with radial and axial bearings in a casing with a shaft and a rotor disk fastened on the shaft
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