US4854279A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Three chamber continuous combustion engine
Assignee: Individual
•
Filing: 1988-09-27
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Granted: 1989-08-08
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Expires: 2008-09-27
Abstract
Abstract A three chamber continuous combustion engine is a rotary vane, concentric rotor type of internal combustion engine having a burner assembly, three crescent shaped static chambers serving as compressor, expander and oil pump; and six dynamic chambers defined by the three intersecting blades slidably inserted in the rotor slots, carrying combustion media through the continuous combustion cycle consisting of intake, compression, air storage, continuous combustion, expansion, decompression and exhaust.
Inventors
- 👤 Cornelio L. Seno
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-05 21:18
CPC Classifications
F; F01; F01C; F01C11/00; F01C11/002; F01C11/004; F01C1/00; F01C1/30; F01C1/34; F01C1/344; F01C1/3446; F02; F02B; F02B53/00; Y; Y02; Y02T; Y02T10/00; Y02T10/10; Y02T10/12
Claims Analysis
Total Claims: 2
Claim 1
Independent Claim
420 words
A three chamber continuous combustion engine comprising: a. a generally spool-shaped segmented rotor which is rotatably and concentrically mounted inside a sealed housing assembly; and which is made up of: i. six arched segments fastened at both ends to two end plates ii. said two end plates having arched holes for reception of the ends of the arched segments, and rectangular radial notches slidably carrying the transverse edges of the blades perpendicular to the axis of the rotor iii. two shafts in the central axes of the end plates that transmit rotative mechanical energy; b. said housing assembly having: i. a circumferential internal surface which is generally an equilateral triangle whose corners are replaced with circular arcs, and which forms jointly with the rotor three crescent shaped static chambers; ii. three sets of intake and discharge ports corresponding to the three crescent shaped static chambers; iii. two end walls with recesses for journalling the end plates for rotation, and with two center holes with bearings for journalling the shafts for rotation; c. the first crescent shaped static chamber serving as a compressor that takes in air from the atmosphere at constant pressure and temperature, and compresses it at constant entropy; d. an air tank that houses a flame tube, that receives pressurized air from the first crescent shaped static chamber, and that stores air at constant pressure, volume, temperature and entropy; e. said flame tube being a hollow cylinder with several holes for air passage, having a fuel nozzle for the introduction of fuel and a spark plug for starting combustion, and serving as the combustion chamber where fuel and air are mixed properly and continuous combustion takes place at constant pressure and volume; f. the second crescent shaped static chamber serving as an expander that receives the high pressure products of combustion from the flame tube, that generates mechanical power during expansion of dynamic chambers at constant pressure, temperature and entropy, that decompresses the dynamic chambers at constant volume, and that rids the dynamic chambers of exhaust gases at constant pressure and temperature; g. the third crescent shaped static chamber serving as an oil pump that takes in and discharges oil functioning as lubricant, coolant and sealant; and h. three intersecting blades of which one is H shaped and the other two are U shaped, having square edges and axial extensions at their outward corners, as well as being inserted slidably in the rotor slots thereby dividing the engine interior into six dynamic chambers carrying combustion media or oil.
Claim 2
Dependent Claim
420 words
A three chamber continuous combustion engine comprising: a. a generally spool-shaped segmented rotor which is rotatably and concentrically mounted inside a sealed housing assembly; and which is made up of: i. six arched segments fastened at both ends to two end plates ii. said two end plates having arched holes for reception of the ends of the arched segments, and rectangular radial notches slidably carrying the transverse edges of the blades perpendicular to the axis of the rotor iii. two shafts in the central axes of the end plates that transmit rotative mechanical energy; b. said housing assembly having: i. a circumferential internal surface which is generally an equilateral triangle whose corners are replaced with circular arcs, and which forms jointly with the rotor three crescent shaped static chambers; ii. three sets of intake and discharge ports corresponding to the three crescent shaped static chambers; iii. two end walls with recesses for journalling the end plates for rotation, and with two center holes with bearings for journalling the shafts for rotation; c. the first crescent shaped static chamber serving as a compressor that takes in air from the atmosphere at constant pressure and temperature, and compresses it at constant entropy; d. an air tank that houses a flame tube, that receives pressurized air from the first crescent shaped static chamber, and that stores air at constant pressure, volume, temperature and entropy; e. said flame tube being a hollow cylinder with several holes for air passage, having a fuel nozzle for the introduction of fuel and a spark plug for starting combustion, and serving as the combustion chamber where fuel and air are mixed properly and continuous combustion takes place at constant pressure and volume; f. the second crescent shaped static chamber serving as an expander that receives the high pressure products of combustion from the flame tube, that generates mechanical power during expansion of dynamic chambers at constant pressure, temperature and entropy, that decompresses the dynamic chambers at constant volume, and that rids the dynamic chambers of exhaust gases at constant pressure and temperature; g. the third crescent shaped static chamber serving as an oil pump that takes in and discharges oil functioning as lubricant, coolant and sealant; and h. three intersecting blades of which one is H shaped and the other two are U shaped, having square edges and axial extensions at their outward corners, as well as being inserted slidably in the rotor slots thereby dividing the engine interior into six dynamic chambers carrying combustion media or oil.
References Cited (Backward Citations)
US1977780A
Cited
US2062576A
Cited
US2452471A
Cited
US3057157A
Cited
DE2125516A1
Cited
GB1427038A
Cited
DE3145814A1
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1992-08-07 | 1993-02-06 | 1993-08-08 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1996-08-07 | 1997-02-06 | 1997-08-08 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2000-08-07 | 2001-02-06 | 2001-08-08 | $7700.00 | Window Closed / Lapsed |