EP1956188A1 - Moteur rotatif hypocycloide a combustion interne - Google Patents
Moteur rotatif hypocycloide a combustion interne Download PDFInfo
- Publication number
- EP1956188A1 EP1956188A1 EP06841702A EP06841702A EP1956188A1 EP 1956188 A1 EP1956188 A1 EP 1956188A1 EP 06841702 A EP06841702 A EP 06841702A EP 06841702 A EP06841702 A EP 06841702A EP 1956188 A1 EP1956188 A1 EP 1956188A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- engine
- rotor
- exhaust
- combustion
- internal
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Withdrawn
Links
- 238000002485 combustion reaction Methods 0.000 title claims abstract description 33
- 239000000446 fuel Substances 0.000 claims description 10
- 239000000203 mixture Substances 0.000 claims description 9
- 239000007789 gas Substances 0.000 claims description 7
- 239000003795 chemical substances by application Substances 0.000 claims description 6
- 239000000376 reactant Substances 0.000 claims description 4
- 239000002826 coolant Substances 0.000 claims description 2
- 238000001816 cooling Methods 0.000 claims description 2
- 239000012530 fluid Substances 0.000 claims description 2
- 238000005192 partition Methods 0.000 claims description 2
- 230000006835 compression Effects 0.000 description 7
- 238000007906 compression Methods 0.000 description 7
- 238000004880 explosion Methods 0.000 description 6
- 230000033001 locomotion Effects 0.000 description 6
- 229910000851 Alloy steel Inorganic materials 0.000 description 2
- 238000002347 injection Methods 0.000 description 2
- 239000007924 injection Substances 0.000 description 2
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 230000001934 delay Effects 0.000 description 1
- 230000009977 dual effect Effects 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000005461 lubrication Methods 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- 230000001131 transforming effect Effects 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
- F01C1/00—Rotary-piston machines or engines
- F01C1/08—Rotary-piston machines or engines of intermeshing engagement type, i.e. with engagement of co- operating members similar to that of toothed gearing
- F01C1/10—Rotary-piston machines or engines of intermeshing engagement type, i.e. with engagement of co- operating members similar to that of toothed gearing of internal-axis type with the outer member having more teeth or tooth-equivalents, e.g. rollers, than the inner member
- F01C1/104—Rotary-piston machines or engines of intermeshing engagement type, i.e. with engagement of co- operating members similar to that of toothed gearing of internal-axis type with the outer member having more teeth or tooth-equivalents, e.g. rollers, than the inner member one member having simultaneously a rotational movement about its own axis and an orbital movement
Definitions
- the invention is comprised in the technical sector dedicated to internal heat combustion engines, more specifically those called explosion or spark ignition engines (SIE).
- SIE explosion or spark ignition engines
- Pistons and connecting rods, as well as reciprocating motions making the balancing of the engine more difficult in order to prevent vibrations, are avoided with the present invention in which the rotor is directly coupled to a crankshaft.
- Patent document DE 103 48 294 A1 describes a rotary engine similar to that of the invention but having different stator and rotor profiles and a different configuration for the distribution and feed system.
- the present invention relates to a hypocycloid rotary heat engine of the type referred to as an explosion or spark ignition engine (SIE).
- SIE explosion or spark ignition engine
- It comprises a curvilinear triangular shaped fixed body or stator with three chambers and planar covers, inside which chambers there is a rotor coupled to a crankshaft, the rotor maintaining permanent contact with the covers and with the profile of the stator in order to achieve tightness between these elements.
- the rotor twice as long as it is wide and with circular ends, is assembled in the crank pin of the crankshaft to which it transmits its circular orbital motion.
- a combustion or explosion chamber there is another small auxiliary chamber in the peripheral part of each of the chambers, referred to as a combustion or explosion chamber, where the sparkplug is included and which also communicates with the rotary valve.
- the rotary valves which perform the dual intake/exhaust function, are tubular, penetrating the air and fuel mixture at one of their ends when the intake stroke is carried out and the burned gases exiting at the other end after expansion to carry out the exhaust stroke.
- the operating cycle of the engine has four strokes or phases: intake, compression, explosion-expansion and exhaust.
- the complete cycle is carried out in a single turn of the rotor corresponding to two turns of the crankshaft.
- the fuel to be used can be liquid or gas, in each case varying the fuel injection feed system to obtain suitable explosive mixtures.
- This type of engine can be applied in different fields, such as automotion in general, generating energy and driving industrial and farm equipment.
- the present invention thus has a series of advantages over the state of the art:
- the rotating and at the same time circular orbital motion of the rotor is identical to that of a hypocycloid gear within the stator acting as a crown-wheel; obtaining as a favorable result that the angular and orbital velocities of the rotor are maintained constant for each rate of rotation of the crankshaft.
- Figure 9 shows a section view of an engine of the invention.
- stator In order to make an engine prototype, the stator, its closing covers, the rotor and the valves are to be made of alloy steel, similar to that which is used for cylinders in reciprocating engines, machining fine finishes in the surfaces in contact with the rotor and the valves.
- a cut has been made at each of the ends of the rotor and such ends have been closed with straight segments to ensure the tightness with the stator to absorb the thermal expansions in the rotor; said cuts and segments have not been described in the drawings to simplify and improve the understanding thereof.
- the coupling with the crankshaft has been provided with bearings.
- crankshaft also made of alloy steel suitable for these types of parts, must be constructed in at least two halves in order to be able to assemble the rotor.
- the driving force caused by the engine will be taken from one end of the crankshaft and the other end will move by means of gear-tooth belts and pulleys, the rotary valves, as well as the necessary auxiliary elements for adapting the chosen ignition and fuel injection systems on the market.
- Lubrication can be carried out by means of an oil circulating pump with a crankcase.
- the engine of the invention further comprises a combustion chamber (a, b, c): in communication with each lobe of the internal cavity (A, B, C) through the inner periphery (PI); having:
- the combustion chamber (a, b, c) is located in a vertex of the lobed triangular shape.
- the exhaust means are formed by a rotary circular valve (Va, Vb, Vc) having: a circular intake segment (SA) having an intake arc (AA) for allowing a reactant to enter from an intake manifold into the combustion chamber (a, b, c); and a circular exhaust segment (SE) having an exhaust arc (AE) for allowing an exhaust gas outlet from the combustion chamber (a, b, c) to an exhaust manifold; wherein:
- the engine further comprises:
- Any engine additionally comprises:
- the stator further comprises a plurality of cooling lines (G) for circulating coolant fluid located between an inner wall (IW) rounding the inner periphery (PI) and an outer wall (OW) defining the outer contour of the engine.
- G cooling lines
- the engine also comprises:
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
- Rotary Pumps (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ES200503041A ES2292326B1 (es) | 2005-11-23 | 2005-11-23 | Motor rotativo hipocicloide de combustion interna. |
PCT/ES2006/000649 WO2007063152A1 (fr) | 2005-11-23 | 2006-11-23 | Moteur rotatif hypocycloide a combustion interne |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1956188A1 true EP1956188A1 (fr) | 2008-08-13 |
EP1956188A4 EP1956188A4 (fr) | 2012-07-18 |
Family
ID=38091899
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP06841702A Withdrawn EP1956188A4 (fr) | 2005-11-23 | 2006-11-23 | Moteur rotatif hypocycloide a combustion interne |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP1956188A4 (fr) |
ES (1) | ES2292326B1 (fr) |
WO (1) | WO2007063152A1 (fr) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104654362B (zh) * | 2015-02-13 | 2016-08-24 | 中国人民解放军国防科学技术大学 | 大尺度超燃冲压发动机和三维花瓣形截面燃烧室 |
US20230053217A1 (en) * | 2020-04-22 | 2023-02-16 | Beihang University | Oblong-shaped rotor engine having high sealing performance |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
BE635946A (fr) * | ||||
GB190925247A (en) * | 1909-11-02 | 1910-10-27 | Harry Gray | Improvements in Rotary Engines, Pumps and Compressors. |
FR1415922A (fr) * | 1964-10-20 | 1965-10-29 | Moteur à combustion | |
US3288121A (en) * | 1962-08-30 | 1966-11-29 | Ceriani | Rotary piston engine |
JPS53105710A (en) * | 1977-02-26 | 1978-09-14 | Ebara Corp | Rotary piston machine |
WO1995012053A1 (fr) * | 1993-10-29 | 1995-05-04 | Pieter Adolf De Geus | Machine a piston rotatif |
DE10348294A1 (de) * | 2003-10-17 | 2005-05-19 | Gerhard Ehlig | Umlaufmotor |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3246835A (en) * | 1966-04-19 | Rotary fluid delivering machine | ||
US2853980A (en) * | 1955-08-29 | 1958-09-30 | Merritt A Zimmerman | Internal combustion engine |
FR1278136A (fr) * | 1960-10-27 | 1961-12-08 | Machine volumétrique à capacités engrenantes | |
DE4209607A1 (de) * | 1992-03-25 | 1992-08-13 | Rolf Eckert | Rotationskolbenmaschine als brennkraftmaschine, expansionsmaschine oder verdichter |
-
2005
- 2005-11-23 ES ES200503041A patent/ES2292326B1/es not_active Expired - Fee Related
-
2006
- 2006-11-23 EP EP06841702A patent/EP1956188A4/fr not_active Withdrawn
- 2006-11-23 WO PCT/ES2006/000649 patent/WO2007063152A1/fr active Application Filing
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
BE635946A (fr) * | ||||
GB190925247A (en) * | 1909-11-02 | 1910-10-27 | Harry Gray | Improvements in Rotary Engines, Pumps and Compressors. |
US3288121A (en) * | 1962-08-30 | 1966-11-29 | Ceriani | Rotary piston engine |
FR1415922A (fr) * | 1964-10-20 | 1965-10-29 | Moteur à combustion | |
JPS53105710A (en) * | 1977-02-26 | 1978-09-14 | Ebara Corp | Rotary piston machine |
WO1995012053A1 (fr) * | 1993-10-29 | 1995-05-04 | Pieter Adolf De Geus | Machine a piston rotatif |
DE10348294A1 (de) * | 2003-10-17 | 2005-05-19 | Gerhard Ehlig | Umlaufmotor |
Non-Patent Citations (1)
Title |
---|
See also references of WO2007063152A1 * |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104654362B (zh) * | 2015-02-13 | 2016-08-24 | 中国人民解放军国防科学技术大学 | 大尺度超燃冲压发动机和三维花瓣形截面燃烧室 |
US20230053217A1 (en) * | 2020-04-22 | 2023-02-16 | Beihang University | Oblong-shaped rotor engine having high sealing performance |
US11668232B2 (en) * | 2020-04-22 | 2023-06-06 | Beihang University | Oblong-shaped rotor engine having high sealing performance |
Also Published As
Publication number | Publication date |
---|---|
ES2292326A1 (es) | 2008-03-01 |
ES2292326B1 (es) | 2009-04-01 |
EP1956188A4 (fr) | 2012-07-18 |
WO2007063152A1 (fr) | 2007-06-07 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
17P | Request for examination filed |
Effective date: 20080605 |
|
AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC NL PL PT RO SE SI SK TR |
|
A4 | Supplementary search report drawn up and despatched |
Effective date: 20120619 |
|
RIC1 | Information provided on ipc code assigned before grant |
Ipc: F01C 1/10 20060101AFI20120613BHEP |
|
DAX | Request for extension of the european patent (deleted) | ||
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN |
|
18D | Application deemed to be withdrawn |
Effective date: 20130117 |