Patents
Patents for F01D 25 - Component parts, details, or accessories, not provided for in, or of interest apart from, other groups (22,148)
07/2001
07/31/2001US6267556 Steam turbine
07/31/2001US6267555 Sheet metal casing for multistage pump and method for manufacturing the same
07/31/2001US6267147 Accumulator/oil tank for journal oil supply
07/31/2001US6266954 Double wall bearing cone
07/31/2001US6266953 Method of operating a gas and steam turbine plant
07/31/2001CA2070435C Vane line with axially positioned heat shields
07/31/2001CA2012234C Gamma titanium alloys modified by chromium and silicon and method of preparation
07/26/2001WO2001053729A1 Thermally stressable wall and method for sealing a gap in a thermally stressed wall
07/26/2001US20010009643 Steam turbine
07/26/2001US20010009592 Bearing damper
07/25/2001EP1118920A1 Machine protection system for rotating equipment and method
07/25/2001EP1118806A1 Thermally charged wall structure and method to seal gaps in such a structure
07/24/2001US6263998 Exhaust silencer panel
07/24/2001CA2234922C Cooled shroud of gas turbine stationary blade
07/19/2001WO2001051772A1 Turbine blade and method of repair
07/19/2001WO2001051771A2 Array for regulating the diameter of a stator of a gas turbine
07/19/2001US20010008070 Air impingement cooling system
07/19/2001US20010008069 Method for supplying lift and hydraulic fluid for a gas turbine
07/18/2001EP1116861A2 A cooling circuit for and method of cooling a gas turbine bucket
07/17/2001US6261061 Method and apparatus for mounting a bearing
07/17/2001US6261056 Ceramic turbine nozzle including a radially splined mounting surface
07/17/2001US6261055 Exhaust flow diffuser for a steam turbine
07/17/2001US6261053 Cooling arrangement for gas-turbine components
07/17/2001US6260658 Silencer for a gas turbine
07/17/2001US6260352 Turbofan aircraft engine
07/17/2001US6260269 Method for overhauling a steam turbine to increase its power
07/17/2001CA2104632C Air cycle machine with magnetic bearings
07/12/2001WO2000009861A3 sUPPORT DEVICES FOR THE VANES OF POWER UNITS
07/12/2001DE19963371A1 Gekühltes Hitzeschild Cooled Heat Shield
07/11/2001EP1114991A2 Methods and systems for estimating engine faults
07/10/2001US6257834 Method and arrangement for the indirect cooling of the flow in radial gaps formed between rotors and stators of turbomachines
07/10/2001US6257829 Computerized method for positioning support jacks underneath industrial gas turbines
07/10/2001US6257588 Brush seal and rotary machine including such brush seal
07/10/2001US6257366 Exhaust device for a turbine engine
07/10/2001US6256990 Exhaust manifold integrally cast with turbine housing for turbocharger
07/05/2001US20010006278 Sealing configuration, in particular for a rotary machine
07/04/2001EP1113160A1 Control lever for a machine test bench
07/04/2001EP1113146A2 Rotatory machine having a seal assembly
07/04/2001EP1112141A1 Method for repairing and producing integrally bladed rotors for a hydraulic engine
07/03/2001US6254341 Engine having resistance to particle deposits
06/2001
06/28/2001WO2001046576A1 Method for operating a steam turbine, and a turbine system provided with a steam turbine that functions according to said method
06/28/2001WO2001045825A1 A method and a device for gas treatment
06/28/2001US20010005555 Heat shields for stator of gas turbine; ensures sufficient cooling of the segment edges near the gaps even when the gaps are closed
06/28/2001US20010005480 Apparatus and methods for relieving thermally induced stresses in inner and outer bands of thermally cooled turbine nozzle stages
06/28/2001US20010004828 Gas turbine fuel system comprising fuel oil distribution control system, fuel oil purge system, purging air supply system and fuel nozzle wash system
06/28/2001DE19960895A1 Multi-stage axial turbine for turbine engine, with boiler in space between rotor disks which has input and output apertures for cooling air flow
06/27/2001CN1067740C Exhaust gas turbo-supercharger
06/26/2001US6250897 Integral ball bearing turbocharger rotor assembly
06/26/2001US6250880 Rotary pump with exclusively hydrodynamically suspended impeller
06/26/2001US6250068 Gas turbine installation
06/21/2001US20010004435 Rotary pump with hydrodynamically suspended impeller
06/21/2001DE19961565A1 Coolant flow at a turbine paddle is adjusted by an inserted body into an opening in the coolant channel which reduces its cross section to give the required coolant flow vol
06/20/2001EP1108926A1 Rotary machine containing a brush seal
06/20/2001EP1108901A2 Seal retainer assembly
06/20/2001EP1108858A2 Double wall bearing cone
06/20/2001EP1108803A2 Method and apparatus for removing a coating from a passage hole in a metal substrate
06/20/2001CN1067460C Pumping device
06/19/2001US6247895 Locking member for processing a flow directing assembly
06/14/2001WO2001042654A1 Turbocharger with design for improved mechanical performance
06/14/2001US20010003242 Gas turbine generator plant
06/13/2001EP1106787A2 Turbine nozzle segment band cooling
06/13/2001EP1106785A1 Channel for leakage air in the rotor of a turbomachine
06/13/2001EP1105623A1 Turbine housing
06/13/2001EP1105250A2 High temperature bolting system
06/13/2001DE19959665A1 Flow channel wall segment fixing device for axial flow machine uses projection segments provided by machine housing
06/13/2001DE19958809A1 Leckstromkanal Leakage current channel
06/13/2001CN1299436A Gas and steam turbine installation
06/13/2001CN1299435A High efficiency low pollution hybrid brayton cycle combustor
06/12/2001US6246138 Microturbine cooling system
06/12/2001US6244819 Adjustable supporting assembly for turbine flowpath components and method thereof
06/12/2001US6244818 Fan guard structure for additional supercharging function
06/12/2001US6244816 Gland portion deformation preventing structure of low pressure steam turbine
06/07/2001WO2001040548A1 Chemical cleaning solution for gas turbine blades
06/07/2001US20010002975 Air-driven rotating and cutting device for use in medical and dental procedures
06/07/2001US20010002963 Thread and screw connection for high application temperatures
06/07/2001DE10060152A1 Mit Luft betriebene Rotations- und Schneidevorrichtung zur Verwendung bei medizinischen und zahnmedizinischen Prozeduren Air-operated rotary and cutting apparatus for use in medical and dental procedures
06/06/2001EP1104836A2 Vane sector seating spring and method of retaining same
06/06/2001CN1298470A Turbo machine with an inner housing and an outer housing
06/05/2001US6241465 Housing for a turbomachine
06/05/2001US6240730 Steam turbogenerator set having a steam turbine and a driven machine for producing electrical power, and method for operation of the steam turbogenerator set
06/05/2001US6240719 Fan decoupler system for a gas turbine engine
05/2001
05/31/2001US20010002234 Rotary pump with exclusively hydrodynamically suspended impeller
05/31/2001US20010001897 Method of forming hollow channels within a component
05/31/2001DE19956919A1 Gasturbinen-Triebwerk mit einer Lagerkammer Gas turbine engine with a storage chamber
05/30/2001EP1103706A2 Bearing chamber for a gas turbine engine
05/30/2001EP1103699A2 Gas turbine combined cycle system
05/30/2001CN2432338Y Support device for bearing box of steam turbine
05/29/2001US6238617 Method for forming a ceramic matrix composite turbocharger housing
05/29/2001US6238180 Leak reducing structure in a steam turbine
05/29/2001US6237921 Nested bridge seal
05/29/2001US6237543 Sealing-steam feed
05/29/2001US6237395 Annular after reactor for use with a jet engine test cell
05/29/2001US6237344 Dimpled impingement baffle
05/29/2001US6237341 Boiler scale collecting device before steam turbine
05/29/2001US6237338 Flexible inlet tube for a high and intermediate pressure steam turbine
05/29/2001US6237322 Oil pump
05/25/2001WO2000049297B1 Diffuser without pulsation of the impact interface and method for suppressing impact interface pulsation of diffusers
05/23/2001EP1101902A2 Damped torque shaft assembly
05/23/2001EP1101897A2 Methods for disassembling, replacing and assembling parts of a steam cooling system for a gas turbine
05/23/2001DE10009655C1 Air cooling system for the paddles of a high pressure gas turbine has flow chambers at each paddle for the leading and trailing edges and the center profile with a heat exchanger to cool the air flow to the paddle edges