EP0093822A1 - Moteur à piston rotatif à combustion continue - Google Patents
Moteur à piston rotatif à combustion continue Download PDFInfo
- Publication number
- EP0093822A1 EP0093822A1 EP82830106A EP82830106A EP0093822A1 EP 0093822 A1 EP0093822 A1 EP 0093822A1 EP 82830106 A EP82830106 A EP 82830106A EP 82830106 A EP82830106 A EP 82830106A EP 0093822 A1 EP0093822 A1 EP 0093822A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- continuous combustion
- cylinder
- drive shaft
- engine
- combustion chamber
- 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- Withdrawn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
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01B—MACHINES OR ENGINES, IN GENERAL OR OF POSITIVE-DISPLACEMENT TYPE, e.g. STEAM ENGINES
- F01B3/00—Reciprocating-piston machines or engines with cylinder axes coaxial with, or parallel or inclined to, main shaft axis
- F01B3/0032—Reciprocating-piston machines or engines with cylinder axes coaxial with, or parallel or inclined to, main shaft axis having rotary cylinder block
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B57/00—Internal-combustion aspects of rotary engines in which the combusted gases displace one or more reciprocating pistons
- F02B57/08—Engines with star-shaped cylinder arrangements
- F02B57/10—Engines with star-shaped cylinder arrangements with combustion space in centre of star
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B75/00—Other engines
- F02B75/02—Engines characterised by their cycles, e.g. six-stroke
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B57/00—Internal-combustion aspects of rotary engines in which the combusted gases displace one or more reciprocating pistons
Definitions
- the engine according to the invention is a new development.
- the following description relates to the functional principle and the elements contributing to the movement with the aim of explaining them in the present patent application without going into certain details relating to construction.
- the engine consists of a cylinder block rotating around the drive shaft, together with the variable-volume chambers formed by the general means (piston, connecting rod - crankshaft), the whole of which is enclosed in an appropriately sized housing and the cylinder head.
- the cylinder head (17) is shown, in which two openings, one to the outlet (2o) and the other to the inlet (21) are provided, which are connected to the respective lines (16) and (3); there is also the holder for the spark plug or the on Spray valve (18) which is in communication with the combustion chamber (19).
- Figure 2 shows the rotating structure, which consists of the following main parts for functional purposes: the drive shaft (1) which is fixedly connected to the rotatable cylinder block (4), in which a certain number of cylinders is provided, in the embodiment six cylinders
- the chambers of variable volume (14) for the rotary movement are formed within these cylinders and are transferred to the pistons via the bevel gear transmission by means of the connecting rod crankshaft power transmission system.
- a movable connection is created between the rotatable cylinder block (4) and the cylinder head (17), which ensures the perfect sealing of the gases contained in the cylinders during their work cycle movement (with suitable lubrication).
- the bevel gears designed for a reduction ratio of 2: 1 consist of a ring gear (7) attached to the housing and freely rotating on the drive shaft, on which six pinions (8) roll and thus rotate around the drive shaft, by generating the alternating movement of the pistons (12) by rotating their own axis by means of connecting rods and crankshafts (10-11).
- a feature of this engine is that it performs continuous combustion in a single combustion chamber, which is clocked in conjunction with the Is brought chambers of variable volume, which are determined by the rotational movement of the cylinder block (4).
- the engine according to the invention has the characteristic function of the four-stroke internal combustion engines, which carry out the heat stroke in the four characteristic phases of intake - compression - combustion or explode and work - discharge at two revolutions of the crankshaft; whereas in normal engines these phases take place cyclically in the same cylinder and independently of each other through the system of intake or injection for each cylinder, in our case the heat cycle takes place through one revolution of the drive shaft and the different chambers of the rotatable cylinder block become consecutive and cyclical in accordance brought with the single combustion chamber of the cylinder head (19).
- the combustion is triggered and maintained by the injection valve arranged in the combustion chamber (19).
- the engine can be designed in a conventional manner as an explosion engine or as an internal combustion engine with compression, in that the space (19) is designed accordingly, and in the first case the candle required for igniting the combustion and in the second case the complicated injection structure for the fuel has to be inserted.
- the engine can operate with continuous combustion as described above, but also according to conventional systems with single explosion or injection into each individual cylinder.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Output Control And Ontrol Of Special Type Engine (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP82830106A EP0093822A1 (fr) | 1982-04-22 | 1982-04-22 | Moteur à piston rotatif à combustion continue |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP82830106A EP0093822A1 (fr) | 1982-04-22 | 1982-04-22 | Moteur à piston rotatif à combustion continue |
Publications (1)
Publication Number | Publication Date |
---|---|
EP0093822A1 true EP0093822A1 (fr) | 1983-11-16 |
Family
ID=8190118
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP82830106A Withdrawn EP0093822A1 (fr) | 1982-04-22 | 1982-04-22 | Moteur à piston rotatif à combustion continue |
Country Status (1)
Country | Link |
---|---|
EP (1) | EP0093822A1 (fr) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6662775B2 (en) | 1999-03-23 | 2003-12-16 | Thomas Engine Company, Llc | Integral air compressor for boost air in barrel engine |
US6698394B2 (en) | 1999-03-23 | 2004-03-02 | Thomas Engine Company | Homogenous charge compression ignition and barrel engines |
US6834636B2 (en) | 1999-03-23 | 2004-12-28 | Thomas Engine Company | Single-ended barrel engine with double-ended, double roller pistons |
CN101413435B (zh) * | 2006-01-12 | 2012-01-25 | 李武权 | 单缸体圆环形缸体内燃机 |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB191309525A (en) * | 1913-04-23 | 1914-02-12 | Joseph Southall | Improvements in Revolving Cylinder Reciprocating Engines. |
FR498685A (fr) * | 1919-04-26 | 1920-01-20 | Albin Marty | Moteur à explosions rotatif |
DE698243C (de) * | 1938-08-25 | 1940-11-05 | Hermann Haacke | Brennkraftmaschine mit parallel zu einer Achse angeordneten und um diese kreisenden Zylindern |
US2245570A (en) * | 1938-05-20 | 1941-06-17 | Manly Corp | Fluid pressure device |
DE2028888A1 (de) * | 1970-06-12 | 1971-12-16 | Lutz, Prof. Dr.-Ing. Otto, 3300 Braunschweig | Hydrostatische Pumpe oder hydrostatischer Motor |
-
1982
- 1982-04-22 EP EP82830106A patent/EP0093822A1/fr not_active Withdrawn
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB191309525A (en) * | 1913-04-23 | 1914-02-12 | Joseph Southall | Improvements in Revolving Cylinder Reciprocating Engines. |
FR498685A (fr) * | 1919-04-26 | 1920-01-20 | Albin Marty | Moteur à explosions rotatif |
US2245570A (en) * | 1938-05-20 | 1941-06-17 | Manly Corp | Fluid pressure device |
DE698243C (de) * | 1938-08-25 | 1940-11-05 | Hermann Haacke | Brennkraftmaschine mit parallel zu einer Achse angeordneten und um diese kreisenden Zylindern |
DE2028888A1 (de) * | 1970-06-12 | 1971-12-16 | Lutz, Prof. Dr.-Ing. Otto, 3300 Braunschweig | Hydrostatische Pumpe oder hydrostatischer Motor |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6662775B2 (en) | 1999-03-23 | 2003-12-16 | Thomas Engine Company, Llc | Integral air compressor for boost air in barrel engine |
US6698394B2 (en) | 1999-03-23 | 2004-03-02 | Thomas Engine Company | Homogenous charge compression ignition and barrel engines |
US6834636B2 (en) | 1999-03-23 | 2004-12-28 | Thomas Engine Company | Single-ended barrel engine with double-ended, double roller pistons |
CN101413435B (zh) * | 2006-01-12 | 2012-01-25 | 李武权 | 单缸体圆环形缸体内燃机 |
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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 |
|
AK | Designated contracting states |
Designated state(s): BE DE FR GB IT SE |
|
RBV | Designated contracting states (corrected) |
Designated state(s): BE DE FR GB IT SE |
|
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: 19840717 |