Patent US3930744A successfully refreshed from Google Patents.
US3930744A
Expired / Lapsed
US
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Pressure gas engine
Assignee: PATTY PROCESSING Inc AN IL CORP
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Filing: 1973-10-10
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Granted: 1976-01-06
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Expires: 1993-10-10
Abstract
Abstract A pressure gas engine having an inner first member of circular cross section with a periphery containing first energy conversion means for converting gas pressure to power and an outer second member extending around the first member and with a generally circular inner surface facing the outer surface of the first member and having second energy conversion means in the inner surface facing the first member and for converting gas velocity to power. In certain embodiments the inner and outer arrangements of the first and second members will be reversed. At least one of these first and second members is rotatable about an axis of rotation by the force exerted thereon due to the gas acting on its energy conversion means with one of the energy conversion means in either the first member or the second member comprising at least one and preferably a plurality of spaced converging-diverging nozzles each lying on a chord of its member that is less than the diameter and exhausting toward the other energy conversion means with the other energy conversion means comprising a series of impulse turbine buckets facing the nozzles. Each bucket is inclined with respect to its member and is adapted to be aligned with the nozzle exhaust on relative movement of the first and second members with respect to each other.
Inventors
- 👤 James V. Theis, Jr.
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-04 18:35
CPC Classifications
F; F01; F01D; F01D1/00; F01D1/32; F01B; F01B25/00; F01B25/02; F01D1/24; F01D1/28
Claims Analysis
Total Claims: 12
Claim 1
Independent Claim
291 words
A pressure gas engine, comprising: an enclosing casing with spaced outlet openings; an inner first member in said casing of substantially circular cross section having first energy conversion means at its periphery for converting dynamic gas velocity to power; an outer second member in said casing surrounding said first member and having second energy conversion means facing said inner first member also for converting dynamic gas velocity to power; power means including a work output power shaft for mounting one of said first and second members additional means for mounting the other of said first and second members to effect relative rotation therebetween when said power is exerted on one of said first and second members, one of said energy conversion means comprising a straight through gas nozzle having a converging entrance, a throat and a diverging exhaust, said nozzle lying on a chord of its said member that is less than a diameter and exhausting into the other energy conversion means, said other energy conversion means comprising a series of impulse turbine buckets each spaced in its entirety from said member containing said nozzles and facing said nozzles, each bucket having an arcuate surface of constant radius transverse to the direction of said rotation, each said nozzle having its exhaust entering each bucket adjacent one edge for generally arcuate travel around said arcuate surface of the bucket and leaving the bucket at an exhaust edge that is opposite said one edge in an energy transmitting wiping action; means for supplying pressure gas to the converging end of said nozzle; and means for exhausting gas from said exhaust edges of said buckets in substantially unrestricted gas flow substantially directly into said casing for escape through said outlet openings in the casing.
Claim 2
Dependent Claim
291 words
A pressure gas engine, comprising: an enclosing casing with spaced outlet openings; an inner first member in said casing of substantially circular cross section having first energy conversion means at its periphery for converting dynamic gas velocity to power; an outer second member in said casing surrounding said first member and having second energy conversion means facing said inner first member also for converting dynamic gas velocity to power; power means including a work output power shaft for mounting one of said first and second members additional means for mounting the other of said first and second members to effect relative rotation therebetween when said power is exerted on one of said first and second members, one of said energy conversion means comprising a straight through gas nozzle having a converging entrance, a throat and a diverging exhaust, said nozzle lying on a chord of its said member that is less than a diameter and exhausting into the other energy conversion means, said other energy conversion means comprising a series of impulse turbine buckets each spaced in its entirety from said member containing said nozzles and facing said nozzles, each bucket having an arcuate surface of constant radius transverse to the direction of said rotation, each said nozzle having its exhaust entering each bucket adjacent one edge for generally arcuate travel around said arcuate surface of the bucket and leaving the bucket at an exhaust edge that is opposite said one edge in an energy transmitting wiping action; means for supplying pressure gas to the converging end of said nozzle; and means for exhausting gas from said exhaust edges of said buckets in substantially unrestricted gas flow substantially directly into said casing for escape through said outlet openings in the casing.
Claim 3
Dependent Claim
85 words
The engine of claim 1 wherein said inner first member and said outer second member are both rotatable about a common axis with one of said members containing a plurality of said nozzles and the other of said members containing said impulse turbine buckets for receiving gas exhaust from the nozzles, and there is provided a single said work output power shaft and said additional means comprises gearing means connecting both said rotatable first and second members to said single shaft for driving the same.
Claim 4
Dependent Claim
50 words
The engine of claim 1 wherein said impulse turbine buckets are arranged in a plurality of circular side-by-side series with adjacent buckets in adjacent series having a common sharp edge positioned opposite the nozzle exhaust whereby the exhaust is divided by said edge for simultaneous flow into the adjacent buckets.
Claim 5
Dependent Claim
61 words
The engine of claim 1 wherein said buckets are arranged in two side-by-side circular series with the adjacent edges of adjacent buckets being joined at a sharp edge and the opposite exhaust edges of the buckets being extended to overlap the side of the member containing the nozzle as an aid in preventing pumping of the gas by the rotating member.
Claim 6
Dependent Claim
17 words
The engine of claim 1 wherein said arcuate surface of each said bucket extends for about 90°-270°.
Claim 7
Dependent Claim
17 words
The engine of claim 1 wherein said arcuate surface of each said bucket extends for about 180°.
Claim 8
Dependent Claim
38 words
The engine of claim 1 wherein said inner first member is rotatable and has a hollow interior bounded by a peripheral wall in which are located a circular series of said nozzles each communicating with said hollow interior.
Claim 9
Dependent Claim
24 words
The engine of claim 7 wherein each said nozzle discharges generally tangentially and in the same direction relative to the circumference of said wall.
Claim 10
Dependent Claim
48 words
The engine of claim 1 wherein said inner first member and said outer second member are both rotatable about a common axis with one of said members containing said nozzle and the other of said members containing said impulse turbine buckets for receiving gas exhaust from the nozzle.
Claim 11
Dependent Claim
66 words
The engine of claim 9 wherein there are a plurality of said nozzles arranged in circular series around the periphery of said first member rotor and exhausting toward said second member rotor and said buckets are arranged in a pair of circular series with an adjacent pair of buckets in the series being aligned substantially parallel to the axis of rotation and having closely adjacent sides.
Claim 12
Dependent Claim
83 words
The engine of claim 1 wherein said buckets are arranged in a pair of closely adjacent circular series with each pair of laterally adjacent buckets in the two series being joined at a common sharp edge for receiving the exhaust of said nozzle and the opposite edge of each bucket exhausting into a circular series of buckets arranged in the same member containing the nozzle and with the nozzle member buckets being in two sets circularly arranged on opposite sides of said nozzle.
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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) | 1979-01-05 | 1979-07-07 | 1980-01-06 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1983-01-05 | 1983-07-07 | 1984-01-06 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1987-01-05 | 1987-07-07 | 1988-01-06 | $7700.00 | Window Closed / Lapsed |