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)
06/2002
06/11/2002US6402469 Fan decoupling fuse
06/06/2002DE10059701A1 Sonde zur Messung von Druckschwingungen Probe for measuring pressure vibrations
06/05/2002EP1211498A1 Probe for measuring pressure vibrations
06/05/2002EP0890030B1 Safety circuit
05/2002
05/29/2002EP1209320A2 Fan disk configuration
05/28/2002US6394746 Gas turbine engine blade containment assembly
05/23/2002US20020059791 Combustion system and method
05/21/2002US6393353 Self-testable architecture for overspeed limitation and cutoff systems when the turbojet stops
05/16/2002DE10054369A1 Anordnung zum Erfassen messtechnischer Daten eines Rotors einer rotierenden Maschine Means for detecting metrological data of a rotor of a rotary machine
05/15/2002CN1084824C Turbine control device and method for regulating load alternation process in turbine
04/2002
04/30/2002US6379108 Controlling a rabbet load and air/oil seal temperatures in a turbine
04/24/2002EP1199441A2 Frangible coupling ring for a fan rotor
04/23/2002US6375410 Frangible cover for turbofan engine blade removal and access
04/18/2002WO2002031332A1 Methods and apparatus for rotor overspeed and overboost protection
04/17/2002EP1114279A4 Dynamic control system and method for catalytic combustion process and gas turbine engine utilizing same
04/16/2002US6371721 Gas turbine engine blade containment assembly
04/11/2002WO2002029225A1 Method of shutting-down a turbine engine and system for carrying out said method
04/10/2002EP0882236B1 Positioning a measuring probe
04/04/2002WO2002027150A1 Emergency system
04/03/2002CN1082131C Device for monitoring turbomachine radial gaps
04/02/2002US6364603 Fan case for turbofan engine having a fan decoupler
04/02/2002US6364602 Method of air-flow measurement and active operating limit line management for compressor surge avoidance
03/2002
03/28/2002WO2002025064A2 Steam turbine inlet bell seal inspection apparatus and method
03/27/2002EP1191191A2 Turbine bearing
03/19/2002CA2283862C Rotational speed control method in gas turbine stopping process
03/14/2002US20020029557 Gas turbine system
03/12/2002US6354073 Combined cycle electric power plant
02/2002
02/27/2002EP1181520A1 Inspection device for an annular combustion chamber of a gas turbine and method of inspecting an annular combustion chamber of a gas turbine
02/20/2002EP1180577A2 Cooling method for a turbine rotor
02/13/2002EP0937194B1 Turbine control device and method for regulating the load alternation process in a turbine
01/2002
01/29/2002US6341936 FOD inspection of laser shock peened gas turbine engine airfoils
01/16/2002EP1172524A2 Method for deploying shroud segments of different thickness in a turbine engine
01/16/2002EP1171691A1 Frangible cover for turbofan engine blade removal and access
01/10/2002US20020004005 Gas turbine engine blade containment assembly
01/08/2002CA2016216C Turbine generator shaft torsion monitor
12/2001
12/18/2001US6331078 Turbine engine bearing
12/13/2001US20010051095 Turbine nozzle stage having thermocouple guide tube
12/12/2001CN1076075C Method and device for cooling the low-pressure stage of a steam turbine
12/06/2001WO2001057364A8 Frangible cover for turbofan engine blade removal and access
12/04/2001US6325546 Fan assembly support system
11/2001
11/06/2001US6312215 Turbine engine windmilling brake
11/06/2001CA2215276C Method and apparatus for detecting burner blowout
10/2001
10/31/2001EP1149229A1 Hardwall fan case with structured bumper
10/31/2001EP1096122A4 Method for detecting sensor failures and for controlling the operation conditions of an object
10/31/2001EP0847482B1 Method and device for cooling the low-pressure stage of a steam turbine
10/24/2001EP1146987A1 Apparatus for performing operations on a workpiece at an inaccessible location
10/23/2001US6305899 Gas turbine engine
10/18/2001US20010031198 Frangible cover for turbofan engine blade removal and access
10/11/2001US20010028840 Gas turbine engine blade containment assembly
10/10/2001EP1143112A1 A gas turbine engine blade containment assembly
10/04/2001EP1137866A1 Impeller containment system
09/2001
09/25/2001US6293085 Shaft decouple logic for gas turbine engine
09/18/2001US6290465 Rotor blade
09/18/2001US6290455 Contoured hardwall containment
09/13/2001WO1995005528A3 Elbow guide tube assembly
09/13/2001US20010020361 Ducted fan gas turbine engine
09/11/2001US6286361 Method and apparatus for remotely detecting pressure, force, temperature, density, vibration, viscosity and speed of sound in a fluid
08/2001
08/28/2001US6279400 Apparatus and method for measuring and selectively adjusting a clearance
08/22/2001EP1126137A2 Turbine engine windmilling brake
08/16/2001US20010013582 Apparatus and method for measuring and selectively adjusting a clearance
08/09/2001WO2001057366A1 Method for operating a turbine and turbine installation
08/09/2001WO2001057364A1 Frangible cover for turbofan engine blade removal and access
08/07/2001US6272422 Method and apparatus for use in control of clearances in a gas turbine engine
07/2001
07/25/2001EP1118920A1 Machine protection system for rotating equipment and method
07/24/2001US6264424 Relating to compressors and turbines
07/17/2001CA2021913C Rotor bore inspection system
07/12/2001US20010007633 Configuration for axial retention of blades in a disc
07/11/2001EP1114916A1 Device for the axial retention of blades in a rim
07/11/2001EP1114279A1 Dynamic control system and method for catalytic combustion process and gas turbine engine utilizing same
07/03/2001US6253537 Revolution speed control method in gas turbine shutdown process
06/2001
06/21/2001WO2001044625A1 Fan case with flexible conical ring
06/06/2001EP1104837A2 Contoured hardwall containment
06/05/2001US6240719 Fan decoupler system for a gas turbine engine
05/2001
05/29/2001US6239504 Turbine guide and a method for regulating a load cycle process of a turbine
05/24/2001US20010001845 Method and apparatus for use in control of clearances in a gas turbine engine
05/08/2001US6227794 Fan case with flexible conical ring
05/02/2001EP1096122A1 Method for detecting sensor failures and for controlling the operation conditions of an object
05/01/2001US6224321 Impeller containment system
04/2001
04/25/2001EP1093542A1 Impact resistant composite shell for gas turbine engine fan case
04/17/2001US6217277 Turbofan engine including improved fan blade lining
04/12/2001WO2001025598A1 Tip sealing configuration for a fan
04/10/2001US6213720 High strength composite reinforced turbomachinery disk
04/10/2001CA2035985C Engaging lever lock for rotor turning gear
04/05/2001WO2001023725A1 Service life management system for high-temperature part of gas turbine
04/05/2001US20010000090 Shaft decouple logic
04/04/2001EP1088966A2 Turbine nozzle stage having thermocouple guide tube
04/04/2001EP1088965A1 A pyrometer mount for a closed-circuit thermal medium cooled gas turbine
03/2001
03/28/2001EP1087105A2 A gas turbine engine blade containment assembly
03/28/2001EP1087104A2 A gas turbine engine blade containment assembly
03/27/2001US6206631 Turbomachine fan casing with dual-wall blade containment structure
03/21/2001EP1084328A1 Shaft breakage detection apparatus
03/14/2001EP1083300A2 Turbo-machine fan casing with dual-wall blade containment structure
03/07/2001EP1042597A4 Start, shutoff and overspeed system
02/2001
02/27/2001US6192930 Valve device
02/07/2001EP1074700A2 Rotor blade
02/07/2001EP1073828A1 Containment system for containing blade burst
02/06/2001US6182531 Containment ring for flywheel failure
02/06/2001US6182521 Device for positioning a measuring probe
01/2001
01/30/2001US6179551 Gas turbine containment casing
01/23/2001US6176074 Shaft decouple logic for gas turbine
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