US5408824A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Rotary heat engine
Assignee: InnerPoint Energy Corp
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Filing: 1993-12-15
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Granted: 1995-04-25
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Expires: 2013-12-15
Abstract
Abstract A jet-propelled rotary engine comprises a housing, a rotor journalled to the housing for rotation of the rotor about an axis, and at least one jet assembly secured to the rotor and adapted for combustion of a pressurized oxygen-fuel mixture. The jet assembly includes a hollow body having a closed leading end and an open trailing end downstream of the leading end. The hollow body defines a chamber having a combustion region where the pressurized oxygen-fuel mixture reacts during combustion to form combustion reaction products, a throat region downstream of the combustion region, a converging region extending from the combustion region to the throat region, and a diverging region extending from the throat region to the trailing end. The combustion reaction products form at least a part of thrust matter passing through the hollow body and discharged therefrom. The converging and diverging regions are configured for increasing the kinetic energy of and expanding the thrust matter. The trailing end defines a discharge port for high speed discharge of a jet stream of the thrust matter from the discharge port generally along a line tangent to the rotor periphery for turning the rotor. The converging region being of a shape such that a curve defined by the locus of centroids of transverse cross-sectional areas of the converging region slope radially outwardly relative to said tangent line.
Inventors
- 👤 Andrew Schlote
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-31 20:53
CPC Classifications
F; F23; F23R; F23R3/00; F23R3/42; F23R3/56; F01; F01D; F01D1/00; F01D1/32; F02; F02C; F02C3/00; F02C3/14; F02C3/16; F02C3/165; Y; Y02; Y02T; Y02T50/00; Y02T50/60
Claims Analysis
Total Claims: 11
Claim 1
Independent Claim
236 words
A jet-propelled rotary engine comprising: a housing; a rotor journalled to said housing for rotation of the rotor about an axis, said rotor having a rotor periphery; and at least one jet assembly secured to the rotor periphery and adapted for combustion of a pressurized oxygen-fuel mixture, said jet assembly including a hollow body having a closed leading end and an open trailing end downstream of the leading end, said hollow body defining a chamber having a combustion region in which the pressurized oxygen-fuel mixture reacts during combustion to form combustion reaction products, a throat region downstream of the combustion region, a converging region extending from the combustion region to the throat region, and a diverging region extending from the throat region to the trailing end, said combustion reaction products forming at least a part of thrust matter passing through the hollow body and discharged therefrom, said converging and diverging regions configured for increasing the kinetic energy of and expanding the thrust matter, said trailing end defining a discharge port for high speed discharge of a jet stream of the thrust matter from the discharge port generally along a line tangent to the rotor periphery for turning the rotor, said converging region being of a shape such that a curve defined by the locus of centroids of cross-sectional areas of the converging region transverse to said tangent line slopes radially outwardly relative to said tangent line.
Claim 2
Dependent Claim
236 words
A jet-propelled rotary engine comprising: a housing; a rotor journalled to said housing for rotation of the rotor about an axis, said rotor having a rotor periphery; and at least one jet assembly secured to the rotor periphery and adapted for combustion of a pressurized oxygen-fuel mixture, said jet assembly including a hollow body having a closed leading end and an open trailing end downstream of the leading end, said hollow body defining a chamber having a combustion region in which the pressurized oxygen-fuel mixture reacts during combustion to form combustion reaction products, a throat region downstream of the combustion region, a converging region extending from the combustion region to the throat region, and a diverging region extending from the throat region to the trailing end, said combustion reaction products forming at least a part of thrust matter passing through the hollow body and discharged therefrom, said converging and diverging regions configured for increasing the kinetic energy of and expanding the thrust matter, said trailing end defining a discharge port for high speed discharge of a jet stream of the thrust matter from the discharge port generally along a line tangent to the rotor periphery for turning the rotor, said converging region being of a shape such that a curve defined by the locus of centroids of cross-sectional areas of the converging region transverse to said tangent line slopes radially outwardly relative to said tangent line.
Claim 3
Dependent Claim
57 words
A jet-propelled rotary engine as set forth in claim 1 wherein said rotor comprises at least one conduit extending generally radially outwardly from a central portion of said rotor to said jet assembly for delivering an oxygen-fuel mixture to said jet assembly, said conduit having a discharge end in communication with the combustion region of the chamber.
Claim 4
Dependent Claim
83 words
A jet-propelled rotary engine as set forth in claim 2 further comprising a delivery nozzle at the discharge end of said conduit, said nozzle having a nozzle restriction for preventing ignition of the oxygen-fuel mixture within the conduit and nozzle, said nozzle extending into the combustion region where it is heated by the combustion reaction products and heats the fuel of the oxygen-fuel mixture in the conduits thereby to hydroxylate the fuel before it is discharged into the combustion regions of the chambers.
Claim 5
Dependent Claim
23 words
A jet-propelled rotary engine as set forth in claim 2 further comprising a compressor communicating with said conduit for compressing the oxygen-fuel mixture.
Claim 6
Dependent Claim
37 words
A jet-propelled rotary engine as set forth in claim 1 wherein said rotor comprises at least one fluid passage communicating with the chamber of said jet assembly for delivering water into the chamber of said jet assembly.
Claim 7
Dependent Claim
23 words
A jet-propelled rotary engine as set forth in claim 1 wherein said housing comprises a rotor housing enclosing the rotor and jet assembly.
Claim 8
Dependent Claim
24 words
A jet-propelled rotary engine as set forth in claim 6 further comprising means for evacuating the rotor housing for reducing drag on the rotor.
Claim 9
Dependent Claim
146 words
A jet-propelled rotary engine as set forth in claim 7 wherein said rotor further comprises first and second axially spaced parallel planar surfaces, and wherein said rotor housing further comprises a first plate axially spaced from and opposing the first planar surface of said rotor and a second plate axially spaced from and opposing the second planar surface of said rotor, said first planar surface and said first plate defining a first clearance gap and said second planar surface and said second plate defining a second clearance gap, said clearance gaps being sufficiently wide to prevent the rotor from contacting the first and second plates during rotation of the rotor relative to the housing and sufficiently narrow to reduce counterflow drafts between the planar surfaces and plates during rotation of the rotor relative to the housing, said planar surfaces and said plates constituting said evacuating means.
Claim 10
Dependent Claim
31 words
A jet-propelled rotary engine as set forth in claim 8 wherein said evacuating means further comprises means for removing at least some of the thrust matter discharged from said jet assemblies.
Claim 11
Dependent Claim
44 words
A jet-propelled rotary engine as set forth in claim 9 wherein said rotor housing further comprises a circumferential duct disposed radially outwardly of said jet assembly, said duct comprising a plurality of openings for passage of the thrust matter discharged from said jet assembly.
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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) | 1998-04-24 | 1998-10-24 | 1999-04-25 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 2002-04-24 | 2002-10-24 | 2003-04-25 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2006-04-24 | 2006-10-24 | 2007-04-25 | $7700.00 | Window Closed / Lapsed |