Matches 1 - 20 out of 20


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US20100172749 WALL OF TURBO MACHINE AND TURBO MACHINE  
The invention relates to wall of a turbo machine having a cascade of blades. The wall includes: a first platform facing a first passage between blades in the cascade of blades; and a second...
US20130089415 GAS TURBINE WITH OPTIMIZED AIRFOIL ELEMENT ANGLES  
A turbine airfoil assembly for installation in a gas turbine engine. The airfoil assembly includes an endwall and an airfoil extending radially outwardly from the endwall. The airfoil includes...
US20050226719 Built-up guide flow fan device  
A built-up guide flow fan device includes a first guide flow fan and a second guide flow fan. The first guide flow fan provides cooling blades and a guide flow part and the guide flow part is...
US20050244268 Self-regulating turbine  
An energy cascade which is preferably fed by solar energy is made from standard solar absorbers including Seebeck elements on the upper end thereof, a self-regulating turbine including a generator...
US20140271158 COMPRESSOR STATOR  
Compressor stators (22) for gas turbine engines (10) are disclosed. An exemplary compressor stator (22) comprises a circumferential array of stator vanes (28) and a shroud (24, 26) for supporting...
US20100158678 AIRFOIL SHAPE FOR A TURBINE NOZZLE  
An article of manufacture having a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in a table. Wherein X and Y are distances in inches which,...
US20130051997 FAN MODULES AND SERVER EQUIPMENT  
A fan module and server equipment are provided that can achieve a balance between increased airflow and noise reduction when an axial flow fan is mounted in the server equipment. The fan module...
US20090169371 STATOR CASCADE OF TURBO TYPE FLUID MACHINE  
In the invention, stator blades are arranged in such a manner that respective intervals between the adjacent stator blades (SV) become unequal at least partly. If the stator blades are arranged as...
US20100111684 TURBINE AIRFOIL CLOCKING  
An assembly of airfoils in a turbine engine, the assembly comprising: at least three successive axially stacked rows of airfoils in one of a compressor and a turbine: a first airfoil row, a second...
US20090123276 STEAM TURBINE  
A steam turbine is provided having a rotor which rotates around a machine axis, and a stator which concentrically encompasses the rotor with clearance, between which an annular passage is formed...
US20100122538 METHODS, APPARATUS AND SYSTEMS CONCERNING THE CIRCUMFERENTIAL CLOCKING OF TURBINE AIRFOILS IN RELATION TO COMBUSTOR CANS AND THE FLOW OF COOLING AIR THROUGH THE TURBINE HOT GAS FLOWPATH  
A method of operating a turbine engine, wherein the turbine engine includes a compressor, a combustor, a turbine, a plurality of successive axially stacked stages that include a row of...
US20100126141 GAS TURBINE ENGINE BOOSTER HAVING ROTATABLE RADIALLY INWARDLY EXTENDING BLADES AND NON-ROTATABLE VANES  
A gas turbine engine booster includes one or more rotatable booster stages having booster blades extending radially inwardly from a rotatable drum and one or more non-rotatable vane stages having...
US20110318174 Compressor Rectifier Architecture  
The present invention relates to a turbomachine rectifier comprising a plurality of stator vanes (5) connecting an inner collar (4) to an outer collar (3), each of said vanes (5) comprising a...
US20150050135 STATOR BLADE DIAPHRAGM RING, STEAM TURBINE AND METHOD  
A stator blade diaphragm ring includes a plurality of stator blades each having a root and a radial pin receiver. The diaphragm ring further includes a first ring having a plurality of slots,...
US20150226124 GAS TURBINE  
In a gas turbine of the invention, a first blade ring portion to which first vanes are attached and a second blade ring portion to which second vanes are attached are integrally formed to form an...
US20140356149 FAN  
A fan includes an impeller and a frame. The frame is used for accommodating the impeller. The frame includes a plurality of static blade groups. Each of the static blade groups has a plurality of...
US20170102009 Metal-to-Metal Sealing for Diffusers Of An Electrical Submersible Well Pump  
A well pump assembly includes a centrifugal pump having a housing with a cylindrical internal side wall. Upper and lower diffusers are located in the housing. A metal-to-metal seal seals an upper...
US20160377091 Axial Turbomachine Compressor Casing  
The present application relates to an axial turbomachine low-pressure compressor stator. The stator includes an outer annular casing made of organic matrix composite materials. The stator also has...
US20160146013 TURBINE ARRANGEMENT  
The invention relates to a turbine for generating work by a stagewise expansion of a gas, such as steam wherein a downstream stage guide average height is less than an adjacent upstream stage...
US20160097281 GAS TURBINE ENGINE AIRFOIL MISTUNING  
A circumferential airfoil array that provides a total airfoil count for the stage and that includes first and second sets of airfoils with different vibrational frequencies. First and second...

Matches 1 - 20 out of 20