US4332520A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Velocity pump reaction turbine
Assignee: United States Department of Energy
•
Filing: 1979-11-29
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Granted: 1982-06-01
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Expires: 1999-11-29
Abstract
Abstract An expanding hydraulic/two-phase velocity pump reaction turbine including a dual concentric rotor configuration with an inter-rotor annular flow channel in which the inner rotor is mechanically driven by the outer rotor. In another embodiment, the inner rotor is immobilized and provided with gas recovery ports on its outer surface by means of which gas in solution may be recovered. This velocity pump reaction turbine configuration is capable of potential energy conversion efficiencies of up to 70%, and is particularly suited for geothermal applications.
Inventors
- 👤 Palmer A. House
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-06 17:50
CPC Classifications
F; F01; F01D; F01D1/00; F01D1/32; F05; F05D; F05D2210/00; F05D2210/10; F05D2210/13
Claims Analysis
Total Claims: 7
Claim 1
Independent Claim
259 words
A velocity pump reaction turbine having the operating characteristic of maximum efficiency at finite speed, for converting thermal energy from a hot liquid at or above its saturation pressure, comprising: a first shaft; an inner velocity pump rotor connected to the first shaft and rotating therewith, the velocity pump rotor having an inlet port at the center, a plurality of first radial passageways extending from the inlet port, and a plurality of first liquid nozzles located on the periphery of the pump rotor at outer ends of the first radial passageways; a second shaft; an outer reaction turbine rotor connected to the second shaft and rotating therewith, and positioned concentrically around the velocity pump rotor, the reaction turbine rotor having a plurality of second radial passageways extending from an inner surface of the reaction turbine rotor, and a plurality of second nozzles located on the periphery of the turbine rotor at outer ends of the second radial passageways; a housing enclosing the pump rotor and concentric turbine rotor, and defining therewith an annular space therebetween; and interconnecting drive means between the first and second shafts to drive the pump rotor from the turbine rotor in the same direction as the turbine rotor and at a speed at which hot liquid at or above its saturation pressure which is flowed into the inlet port of the pump rotor is pumped through the first radial passageways and first liquid nozzles into the annular space with a fluid velocity matching the tangential velocity of the outer turbine rotor at its inner surface.
Claim 2
Dependent Claim
259 words
A velocity pump reaction turbine having the operating characteristic of maximum efficiency at finite speed, for converting thermal energy from a hot liquid at or above its saturation pressure, comprising: a first shaft; an inner velocity pump rotor connected to the first shaft and rotating therewith, the velocity pump rotor having an inlet port at the center, a plurality of first radial passageways extending from the inlet port, and a plurality of first liquid nozzles located on the periphery of the pump rotor at outer ends of the first radial passageways; a second shaft; an outer reaction turbine rotor connected to the second shaft and rotating therewith, and positioned concentrically around the velocity pump rotor, the reaction turbine rotor having a plurality of second radial passageways extending from an inner surface of the reaction turbine rotor, and a plurality of second nozzles located on the periphery of the turbine rotor at outer ends of the second radial passageways; a housing enclosing the pump rotor and concentric turbine rotor, and defining therewith an annular space therebetween; and interconnecting drive means between the first and second shafts to drive the pump rotor from the turbine rotor in the same direction as the turbine rotor and at a speed at which hot liquid at or above its saturation pressure which is flowed into the inlet port of the pump rotor is pumped through the first radial passageways and first liquid nozzles into the annular space with a fluid velocity matching the tangential velocity of the outer turbine rotor at its inner surface.
Claim 3
Dependent Claim
22 words
The turbine of claim 1 wherein the second nozzles each comprise a converging liquid nozzle opening into a diverging two-phase steam nozzle.
Claim 4
Dependent Claim
23 words
The turbine of claim 2 wherein the first and second nozzles are directed substantially tangentially to the pump rotor and turbine rotor, respectively.
Claim 5
Dependent Claim
45 words
The turbine of claims 1, 2 or 3 for use with hot liquid at saturation pressure wherein the pump rotor is driven by the turbine rotor through the interconnecting drive means at an angular velocity of about one-half the angular velocity of the turbine rotor.
Claim 6
Dependent Claim
48 words
The turbine of claims 1, 2 or 3 for use with hot liquid at greater than saturation pressure wherein the pump rotor is driven by the turbine rotor through the interconnecting drive means at an angular velocity of less than one-half the angular velocity of the turbine rotor.
Claim 7
Dependent Claim
26 words
The turbine of claims 1, 2 or 3 adapted to be driven by a hot liquid at or above its saturation pressure from a geothermal source.
References Cited (Backward Citations)
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1985-05-31 | 1985-11-30 | 1986-06-01 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1989-05-31 | 1989-11-30 | 1990-06-01 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1993-05-31 | 1993-11-30 | 1994-06-01 | $7700.00 | Window Closed / Lapsed |