Patents for F01D 1 - Non-positive-displacement machines or engines, e.g. steam turbines (3,766)
03/2006
03/01/2006EP1630359A1 Steam turbine with two steam chambers
02/2006
02/28/2006US7004723 Device for controlling variable-pitch vanes in a turbomachine
02/28/2006US7004721 Annular platform for a nozzle of a low-pressure turbine of a turbomachine
02/28/2006US7003961 Trapped vortex combustor
02/23/2006WO2006019927A2 Braking surface cooling assembly and brake performance enhancing methods
02/23/2006DE102005033362A1 Axialdampfturbinenanordnung Axialdampfturbinenanordnung
02/22/2006EP1627185A2 Trapped vortex combustor
02/22/2006EP1337740B1 Gas turbine stator
02/22/2006CN1739229A Turbo-machine and method for operating the same
02/21/2006US7001140 Centrifugal fan diffuser
02/16/2006WO2005121547A3 Pressurized fluid turbine engine
02/16/2006US20060034677 Pressurized fluid turbine engine
02/16/2006US20060032210 Methods and apparatus for assembling a gas turbine engine
02/15/2006EP1626170A1 Turbomachine with counter-rotating fan
02/15/2006EP1626002A1 Gas turbine engine turbine assembly
02/14/2006US6997674 Pressurized fluid turbine engine
02/14/2006US6996971 Rotary heat engine
02/09/2006WO2006014517A2 Molten metal pump
02/09/2006US20060029491 Roto-dynamic fluidic systems
02/09/2006US20060026980 Apparatus, method and software for use with an air conditioning cycle
02/09/2006DE102005025630A1 Drehmomentwandler mit hohem Wirkungsgrad Torque converter with a high efficiency
02/08/2006CN1730916A Carbon dioxide steamer engine
02/07/2006US6995979 Heat-dissipating fan module of electronic apparatus
02/02/2006US20060024162 Method and apparatus for assembling gas turbine engines
02/02/2006US20060024161 Stator for a hydrodynamic torque converter
02/02/2006US20060024160 Centrifugal blower having auxiliary radial inlet
02/02/2006US20060024159 Airfoil shape and sidewall flowpath surfaces for a turbine nozzle
02/02/2006US20060024158 Flow structure for a gas turbine
02/02/2006US20060021353 Gas turbine power plant with supersonic gas compressor
02/02/2006DE102005022027A1 Kraftstoffpumpe mit einseitigem Verdichter Fuel pump with single-sided compressor
01/2006
01/31/2006US6991426 Variable pitch fan
01/31/2006US6991425 Air turbine starter with unitary inlet and stator
01/26/2006WO2006008353A1 Revolving toroidal motor
01/26/2006US20060018751 Fan blade modifications
01/25/2006CN1724851A Method and system for operating rotary machines
01/24/2006US6988870 Casing for a centrifugal pump
01/24/2006US6988868 Propulsion linearizing mechanism
01/24/2006CA2305400C Improved turbine powerplant
01/19/2006US20060013686 Frame for an electrical fan
01/19/2006US20060013685 Vane platform rail configuration for reduced airfoil stress
01/19/2006US20060013684 Fan impeller and fan motor
01/19/2006US20060013683 Spacer arrangement
01/19/2006US20060011425 Braking surface cooling assembly and brake performance enhancing methods
01/19/2006DE202005013520U1 Radial turbine especially for enhanced thermal engine is constructed as stator-less constant-pressure turbine, with active deflection and reaction surfaces provided on rotor
01/19/2006DE10239644B4 Motor, insbesondere zum Antreiben von Fahrzeugen Motor, especially for driving of vehicles
01/12/2006DE102004030273A1 Verbessertes Verfahren und Vorrichtung zur Nutzung der inneren Energie von Fluiden Improved method and apparatus for the utilization of internal energy of fluids
01/11/2006EP1614855A1 Turbomachine and method to operate such a turbomachine
01/11/2006CN1718831A Heat-proof steel and shaft using same for steam turbine,steam turbine and steam turbine generator
01/10/2006US6984108 Compressor stator vane
01/05/2006WO2006001855A2 Gas flow enhancer for combustion engines
01/05/2006WO2006001825A2 Gas turbine cooled shroud assembly with hot gas ingestion suppression
01/05/2006US20060003217 Planar membraneless microchannel fuel cell
01/05/2006US20060002790 Fan assembly and fan frame thereof
01/05/2006CA2571181A1 Gas flow enhancer for combustion engines
01/05/2006CA2551016A1 Gas turbine cooled shroud assembly with hot gas ingestion suppression
12/2005
12/29/2005WO2005124109A1 Combined cycle boundary layer turbine
12/29/2005US20050287001 Shroud and vane segments having edge notches
12/29/2005US20050286995 Method and system for determining gas turbine tip clearance
12/29/2005DE102004028950A1 Conversion of thermal energy e.g. piston engine exhaust gases into kinetic energy includes accelerating a gas at temperature and pressure values exceeding those of the ambient air through a jet and mixing with colder ambient air
12/28/2005EP1540140A4 Apparatus, method and software for use with an air conditioning cycle
12/22/2005WO2005121548A2 Pressurized fluid bladeless turbine engine with opposing fluid intake assemblies
12/22/2005WO2005121547A2 Pressurized fluid turbine engine
12/22/2005US20050281663 Double impingement vane platform cooling
12/22/2005DE102004026602A1 Verfahren und Vorrichtung zur Nutzung der inneren Energie von Fluiden A method and apparatus for the utilization of internal energy of fluids
12/21/2005EP1607583A1 Method and system for operating rotary machines
12/18/2005CA2509863A1 Double impingement vane platform cooling
12/15/2005WO2005119056A1 Method and device for using internal energy of fluids by means of a flow process and a turbomachine
12/15/2005WO2005119011A1 Radiator cooling fan replacement to increase engine efficiency
12/15/2005US20050276693 Fan enabling increased air volume
12/15/2005US20050276692 Lightened interblade platform for a turbojet blade support disc
12/15/2005US20050276681 Combined cycle boundary layer turbine
12/15/2005DE10250547A1 Compressed air engine used in automobile construction comprises rotating propelling nozzles arranged on one end which are structured in such a way that repelling forces produced in the nozzles are converted into a rotary movement
12/14/2005CN1231682C Blower device
12/14/2005CA2470137A1 The gas jet engine generator
12/13/2005US6974305 Roto-dynamic fluidic systems
12/13/2005US6973792 Method of and apparatus for a multi-stage boundary layer engine and process cell
12/08/2005WO2005116443A1 Hydroelectric turbine with collapsile shroud
12/08/2005US20050271508 Flexible turbine blade
12/08/2005US20050271499 Methods and systems for operating rotary machines
12/08/2005US20050268603 High efficiency torque converter
12/08/2005DE10236273B4 Turax-Motor mit dreifachem Wirkungsprinzip Turax motor with triple action principle
12/08/2005DE102004058928A1 Drive motor for concentrated turbine, has free flight dual piston and drive block for hydrodynamically transferring basis energy to turbine with external teeth, and axle directly connected with motor and mutually containing air bag
12/06/2005US6971848 Multistage pump and method of making same
12/01/2005US20050265820 Means to regulate water velocity through a hydro electric turbine
11/2005
11/30/2005EP1599657A1 Device for effecting heat transfer to rotating equipment, in particular gas turbines
11/29/2005US6968691 Recirculating medium turbine
11/24/2005US20050260074 Centrifugal compressor and manufacturing method for impeller
11/24/2005US20050260073 Heat-dissipating device
11/24/2005US20050260072 Heat-dissipating device
11/24/2005US20050260071 Heat-dissipating device
11/24/2005US20050260065 Blower
11/24/2005US20050260063 Retractable drum fan
11/22/2005US6966751 Turbine vibrator
11/17/2005WO2005108759A1 Shockwave-induced boundary layer bleed for transonic gas turbine
11/17/2005US20050254944 Fastened vane assembly
11/17/2005DE102004020042A1 Compact rotary IC engine has a cylindrical rotor with shaped combustion chambers between inlet and outlet plates rotating inside a stator
11/17/2005DE102004007145A1 Strömungsleitelement und eine damit ausgestattete strömungstechnische Anlage Flow guide and a fluidic system equipped therewith
11/17/2005CA2565867A1 Shockwave-induced boundary layer bleed for transonic gas turbine
11/10/2005WO2005106205A1 Bladeless fluid machine
11/10/2005US20050249617 Fuel pump having single sided impeller
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