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US3967914A Expired / Lapsed US ⏱️ 0.0 years remaining

Power generating system

Assignee: JOSEPH GAMELL INDUSTRIES Inc A MN CORP
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Filing: 1975-01-06
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Granted: 1976-07-06
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Expires: 1995-01-06
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Abstract

Abstract A power generating system which includes a turbine and a radiant heat boiler for supplying motive fluid to the turbine. The turbine is provided with a stator having a cylindrical bore and a cylindrical rotor provided with a substantially uniformly rough lateral surface. The inner wall of the turbine stator is provided with a continuous oblique helical groove which serves as a passageway for the motive fluid. The lateral surface of the rotor has a relatively high drag coefficient and the rotor is actuated to a high rotational speed by the motive fluid flowing in the stator passageway and past the rotor lateral surface. The radiant heat boiler comprises a hermetically sealed enclosure having a substantially globular inner surface covered with radiant heat reflecting surfaces, a substantially globular pressure vessel centrally situated within the enclosure and spaced apart from the reflecting surfaces about its entire periphery, a radiant heat source mounted within the space between the reflecting surfaces and the pressure vessel.

Inventors

  • 👤 Joseph A. Gamell

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-28 16:18
CPC Classifications
F; F01; F01D; F01D1/00; F01D1/34; F01D1/36

Claims Analysis

Total Claims: 16
Claim 1
Independent Claim 127 words
A turbine comprising a stator having a cylindrical bore; a cylindrical rotor coaxially journalled in said stator and provided with a substantially uniformly rough lateral surface; and an output shaft secured to the rotor and projecting axially from one end of the rotor; said stator being provided with a motive fluid inlet port near one end of the rotor and with a motive fluid outlet port near the other end of the rotor; and the inner wall of said stator being provided with a continuous oblique helical groove over that portion of the inner wall which is coextensive with the lateral surface of the rotor, one end of said groove communicating with said inlet port and the other end of said groove communicating with said outlet port.
Claim 2
Dependent Claim 127 words
A turbine comprising a stator having a cylindrical bore; a cylindrical rotor coaxially journalled in said stator and provided with a substantially uniformly rough lateral surface; and an output shaft secured to the rotor and projecting axially from one end of the rotor; said stator being provided with a motive fluid inlet port near one end of the rotor and with a motive fluid outlet port near the other end of the rotor; and the inner wall of said stator being provided with a continuous oblique helical groove over that portion of the inner wall which is coextensive with the lateral surface of the rotor, one end of said groove communicating with said inlet port and the other end of said groove communicating with said outlet port.
Claim 3
Dependent Claim 18 words
The turbine of claim 1 wherein each helical convolution is canted about 15° to 35° to the normal.
Claim 4
Dependent Claim 17 words
The turbine of claim 2 in which each helical convolution is canted about 25° to the normal.
Claim 5
Dependent Claim 14 words
The turbine of claim 2 wherein the lateral surface of the rotor is knurled.
Claim 6
Dependent Claim 15 words
The turbine of claim 3 in which the lateral surface of the rotor is knurled.
Claim 7
Dependent Claim 22 words
The turbine of claim 1 wherein the motive fluid inlet port is situated substantially tangential to the lateral surface of the rotor.
Claim 8
Dependent Claim 58 words
The turbine of claim 1 wherein each helical convolution is canted toward the motive fluid inlet port whereby the motive fluid entering the inlet port sweeps across one face of the rotor at a substantial angle away from the inlet and then back across the opposite face of the rotor, at essentially the same angle toward the inlet.
Claim 9
Dependent Claim 21 words
The turbine of claim 7 wherein each helical convolution is canted at an angle of 15° to 35° to the normal.
Claim 10
Dependent Claim 20 words
The turbine of claim 7 wherein each helical convolution is canted at an angle of about 25° to the normal.
Claim 11
Dependent Claim 14 words
The turbine of claim 9 wherein the lateral surface of the rotor is knurled.
Claim 12
Dependent Claim 179 words
In a turbine comprising a stator having a cylindrical bore; a cylindrical rotor coaxially journalled in said stator and provided with a substantially uniformly rough lateral surface; and an output shaft secured to the rotor and projecting axially from one end of the rotor; said stator being provided with a motive fluid inlet port near one end of the rotor and with a motive fluid outlet port near the other end of the rotor; and the inner wall of said stator being provided with a continuous helical groove over that portion of the inner wall which is coextensive with the lateral surface of the rotor, one end of said groove communicating with said inlet port and the other end of said groove communicating with said outlet port, the improvement wherein the helical groove comprises a plurality of sequentially connected convolutions of 360° each, which are characterized in that the line connecting the 180° point in any one convolution to the mid-point between the zero degree point and the 360° point of the same convolution is canted to the normal.
Claim 13
Dependent Claim 179 words
In a turbine comprising a stator having a cylindrical bore; a cylindrical rotor coaxially journalled in said stator and provided with a substantially uniformly rough lateral surface; and an output shaft secured to the rotor and projecting axially from one end of the rotor; said stator being provided with a motive fluid inlet port near one end of the rotor and with a motive fluid outlet port near the other end of the rotor; and the inner wall of said stator being provided with a continuous helical groove over that portion of the inner wall which is coextensive with the lateral surface of the rotor, one end of said groove communicating with said inlet port and the other end of said groove communicating with said outlet port, the improvement wherein the helical groove comprises a plurality of sequentially connected convolutions of 360° each, which are characterized in that the line connecting the 180° point in any one convolution to the mid-point between the zero degree point and the 360° point of the same convolution is canted to the normal.
Claim 14
Dependent Claim 63 words
The turbine of claim 11, in which the said line is canted toward the motive fluid inlet port, whereby the motive fluid entering the inlet port sweeps down across one face of the rotor substantially at the angle of the cant and away from the inlet, and then back across the opposite face of the rotor at substantially the angle of the cant.
Claim 15
Dependent Claim 20 words
The turbine of claim 12, in which the angle of the cant is about 15° to 35° to the normal.
Claim 16
Dependent Claim 18 words
The turbine of claim 13, in which the angle of the cant is about 25° to the normal.

References Cited (Backward Citations)

US68325A Cited
US158579A Cited
US551853A Cited
US778928A Cited
US981311A Cited
US2325530A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1979-07-06 1980-01-05 1980-07-06 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1983-07-06 1984-01-05 1984-07-06 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1987-07-06 1988-01-05 1988-07-06 $7700.00 Window Closed / Lapsed

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