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7478629 |
Axial flow supercharger and fluid compression machine
A compression and vacuum-producing machine includes a housing, at least one rotating disk having a plurality of blades rotationally supported within the housing, and at least one stationary disk...
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6638014 |
Valve arrangement for a power plant
The invention relates to a valve arrangement ( 1 ), in particular for a power plant. A housing ( 2 ) contains a shut-off valve ( 3 ) for shutting off a fluid flow, a control valve ( 4 ) for...
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6398491 |
Multistage turbocompressor
A multistage turbocompressor is equipped with a tapping point between two compressor stages. The guide-blade cascade of the stage arranged directly upstream or downstream of the tapping point is...
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6092984 |
System life for continuously operating engines
A method is provided for extending the system life of variable geometry components, including variable geometry rings, in an engine system by minimizing relative motion incurred from engine...
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5911679 |
Variable pitch rotor assembly for a gas turbine engine inlet
A cospander for extending the high efficiency range of a turbine engine is described. A cospander, in one aspect, is a turbomachinery device including at least one stage wherein stator vane and...
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5553995 |
Method of driving a turbine in rotation by means of a jet device
A turbine device and a method of driving the turbine device are disclosed. The turbine device includes an admission channel, a turbine, and an injection channel. The turbine device may also include...
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5269648 |
Arrangement for controlling the flow cross section of a turbomachine
An arrangement for controlled admission to a nozzle assembly of axial flow extraction steam turbines consists essentially of a control valve located upstream of the nozzle assembly and having two...
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5184459 |
Variable vane valve in a gas turbine
In a gas turbine bypass engine having an inlet for gas flow to a core duct and an outer duct for bypassing a portion of the inlet air flow around such core duct, an improvement is provided in which...
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4874287 |
Variable-geometry turbocompressor
A variable-geometry turbocompressor is provided which includes a tandem variable stator downstream of a rotor stage. The tandem stator includes an inlet stator cascade and an outlet stator cascade...
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4836746 |
Axial flow engine guide vane adjusting device
The shafts of guide vanes of an axial-flow engine, in particular, a combustion turbine, are supported angle-adjustably in an annular guide vane carrier and are spring-loaded and vibration-damped in...
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4590889 |
Arrangement for influencing a cooling air flow
An arrangement for influencing a cooling air flow passing through a cooling air system of an internal-combustion engine of a vehicle includes a heat exchanger and a blower arranged in an air...
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4486144 |
Rotating wind-guiding shell for the fan
A rotating wind-guiding shell for an electrical fan effectively changes the direction and magnitude of the blowing wind from the fan. The pressure and the direction of the wind from the fan can be...
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4400135 |
Vane actuation system
An improved vane actuation system for a gas turbine engine having adjustable stator vanes in stages between which the engine casing exhibits relative axial and radial thermal growth, the improved...
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4321476 |
Bi-directional wind power generator
A structure designed to be placed in an existing pass in a mountain range comprises a framework having a plurality of individual passageways through which moving air may travel. Each passageway...
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4245467 |
Isolated reverse turbine system for gas turbine engines
A reversing system for gas turbine engines having, in addition to a conventional gas generator and power turbine, a reversing turbine coupled to the exhaust end of the power turbine output shaft, a...
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4079665 |
Wall mounted ventilator
A ventilator adapted for wall mounting use in ventilating buildings such as agricultural buildings and the like used for housing livestock, and having inlet and exhaust duct means, located one...
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3795458 |
MULTISTAGE COMPRESSOR
The axial-flow low pressure section and radial-flow or diagonal-flow high pressure section are separated by a recooler in which the working fluid is first deflected outwardly from the rotor, spread...
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3790298 |
FLEXIBLE CONTOUR TURBINE NOZZLE FOR TIGHT CLOSURE
In a two shaft, axial flow, reversing gas turbine, hot turbine gases from the blades of the compressor turbine are selectively directed through a variable nozzle ring to rotate the turbine wheel of...
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3772886 |
APPARATUS FOR WATER JET PROPULSION
Apparatus for water jet propulsion in which a screw propeller is integrally formed with a surrounding duct, which surrounding duct rotates with the screw propeller to eliminate blade-tip vortex. A...
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3356289 |
Supersonic compressors of the centrifugal or axial flow and centrifugal types
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3297307 |
Multi-stage circulators
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3289597 |
Centrifugal pump
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3209537 |
Motive fluid control for a re-expansion gas turbine engine
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3050946 |
Method and apparatus for operation of ship installed gas turbine plants
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2831627 |
Axial flow compressor apparatus
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3552873 |
Title is not available
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