Fluidic controlled diffusers for turbopumps
AssigneeThe United States of America as represented by the Secretary of the Navy
InventorsSydney Davis, John M. Durkin
Life of this patent
Estimating the term…
Abstract
An arrangement for controlling the apparent curvature of diffuser vanes of turbine fan to reduce stalling of the vanes and increase efficiency of the fan output over a wider range of flow demand. Sensors responsive to pressure on opposite sides of the vanes selectively control the discharge of pressurized fluid from the diffuser vanes to effect their apparent curvature changes. The arrangement has particular use in a ride control system for surface effect ships.
Claims4
In a centrifugal fan including a rotor for supplying air under pressure at varying flow rate demands, the improvement comprising:
- a cascade of curved hollow diffuser vanes fixedly disposed radially about the rotor for converting velocity head to static pressure in fan output air;
- said fixed hollow diffuser vanes having openings communicating from their hollow interiors to their surfaces adjacent trailing edges thereof;
- an independent source of pressurized fluid in communication with the hollow vanes for discharging fluid from said openings so as to effect an apparent curvature change of the diffuser vanes to fan air flowing thereover;
- and
- means sensing static pressure on opposite sides of the vanes and in response thereto instanteously controlling the amount of pressurized fluid discharging from the diffuser vanes to present an apparent curvature for most efficiently handling that flow rate.
In a centrifugal fan including a rotor and a cascade of curved diffuser vanes fixedly disposed about the rotor for converting velocity head to static pressure of fan air being delivered to a pressurized cushion beneath a surface effect ship at varying rates of flow for supporting the ship and maintaining it in proper ride control, an improvement comprising:
- an independent source of pressurized fluid;
- and
- means responsive to impending flow rate demands by sensing pressure variations on opposite sides of the vanes and associated with the pressurized fluid for selectively discharging pressurized fluid from surfaces of the diffuser vanes in a manner and at a rate to instantaneously create an apparent curvature change on the diffuser vanes to air supplied by the fan for most efficiently handling that flow rate.
A ride control system for a surface effect ship comprising in combination:
- a centrifugal fan for supplying air to a pressurized cushion in a plenum chamber beneath the surface effect ship at varying rates of flow for supporting the ship on cushion and for maintaining it in proper ride control;
- said fan having a rotor;
- a cascade of curved diffuser vanes disposed peripherally of the rotor for receiving air discharged from the rotor and converting its velocity head to static pressure;
- said diffuser vanes being hollow and having passage means communicating with the exterior surfaces thereof;
- a source of pressurized fluid in communication with the vanes interiors;
- and
- means responsive to flow requirements for maintaining the cushion in proper ride control;
- said responsive means sensing pressure variations on opposite sides of the diffuser vanes and selectively admitting pressurized fluid from the source to interiors of said diffuser vanes for discharge from the passages at a rate for effecting an apparent curvature change on the vanes which curvature most efficiently handles the fan output necessary to meet the air flow requirements.
The method of improving efficiency of a centrifugal fan having a rotor which discharges air through a cascade of fixed curved diffuser vanes for converting velocity head to static pressure in air supplied downstream over a wide range of varying rates to meet flow demands comprising the steps of:
- sensing pressure variations on opposite sides of the diffuser vanes;
- and
- responding to the sensed pressure by selectively permitting the ejection of pressurized fluid of an independent source from the surface of diffuser vanes at a rate for effecting an apparent curvature on the diffuser vane surfaces sufficient to most efficiently handle the flow rate to meet the demand.
Dependencies are inferred from the claim text.