GB1007250A - A rotary internal combustion engine - Google Patents
A rotary internal combustion engineInfo
- Publication number
- GB1007250A GB1007250A GB23697/63A GB2369763A GB1007250A GB 1007250 A GB1007250 A GB 1007250A GB 23697/63 A GB23697/63 A GB 23697/63A GB 2369763 A GB2369763 A GB 2369763A GB 1007250 A GB1007250 A GB 1007250A
- Authority
- GB
- United Kingdom
- Prior art keywords
- chamber
- engine
- rotor
- compression
- valve cylinder
- 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.)
- Expired
Links
- 238000002485 combustion reaction Methods 0.000 title abstract 7
- 230000006835 compression Effects 0.000 abstract 3
- 238000007906 compression Methods 0.000 abstract 3
- 239000000203 mixture Substances 0.000 abstract 3
- 238000005461 lubrication Methods 0.000 abstract 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 abstract 1
- 229910052799 carbon Inorganic materials 0.000 abstract 1
- 239000000446 fuel Substances 0.000 abstract 1
- 239000007789 gas Substances 0.000 abstract 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 abstract 1
Classifications
-
- 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
- F02B53/00—Internal-combustion aspects of rotary-piston or oscillating-piston engines
- F02B53/04—Charge admission or combustion-gas discharge
- F02B53/08—Charging, e.g. by means of rotary-piston pump
-
- 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
- F02B2075/022—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle
- F02B2075/027—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle four
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Applications Or Details Of Rotary Compressors (AREA)
- Rotary Pumps (AREA)
Abstract
1,007,250. Rotary internal combustion engines. R. L. TERRY. May 28, 1964 [June 13, 1963], No. 23697/63. Heading F1F. A rotary I.C. engine comprises first and second stage compressor chambers 3, 4, Figs. 1 and 2, and a combustion chamber 2, Fig. 3, with in each of which is eccentrically and rotatabily mounted a rotor having vanes slidably mounted in radial slots and a distributing valve 5 located between the second stage compressor chamber 4 and the combustion chamber 2 An air/fuel mixture when operating as a four-stroke "Otto" cycle engine or air when operating as a compression-ignition engine is sucked into the chamber 3 through ports 9 and after compression by the rotor is discharged through a port 6 to the chamber 4 where it is further compressed. After the further compression, the charge is discharged through a port 7 into a recess 31 in the valve cylinder 29 formed with longitudinally extending passages 33 which at the mid-length of the valve cylinder communicate with pairs of radial passages 30, so that on rotation of the valve cylinder the passages 30 are sequentially brought into communication with a port 8 opening into the combustion chamber 2. At a point 34 in the chamber 2 is fitted a spark-plug in the case of an "Otto" cycle engine or a fuel-injector in the case of a compression-ignition engine. The expanding gases which are finally exhausted through ports 10 drive the rotor 12 and with it the first stage compressor rotor 13 and through 1:1 ratio gearing 26b, 26a the second stage compressor rotor 27 and the valve cylinder 29. The timing of the closure of the port 8 in relation to the rotation of the rotor 12 may be adjusted by the vertical adjustment of a wedge 36, Fig. 4, which in co-operation with a wedge 38 secured to the engine casing 1 moves a key in a helical key-way 35 to axially move the gear 26a and rotate the shaft 25 to which the valve cylinder 29 is secured. Cam rollers in the bottom of the vane slots in co-operation with a cam groove together with centrifugal force urge the vanes of each of the rotors sealingly against the inner wall of its respective chamber. Lubrication may be provided by the use of a petrol/oil mixture or by forced lubrication. The engine may be water cooled and a thermally insulating gasket provided between the combustion chamber and the two compression chambers. Any build up of carbon in the combustion chamber is removed by the vanes rotating therein. A by-pass channel 40 may be provided in the wall of the chamber 2 so that after the engine has been started the ignition means may be switched off, the newly introduced ignition mixture into the chamber then being ignited by back-ignition from the preceding charge through the channel 40. For cold starting heat could be applied from a suitable source at the location 34.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB23697/63A GB1007250A (en) | 1963-06-13 | 1963-06-13 | A rotary internal combustion engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB23697/63A GB1007250A (en) | 1963-06-13 | 1963-06-13 | A rotary internal combustion engine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB1007250A true GB1007250A (en) | 1965-10-13 |
Family
ID=10199809
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB23697/63A Expired GB1007250A (en) | 1963-06-13 | 1963-06-13 | A rotary internal combustion engine |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB1007250A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5101782A (en) * | 1988-08-29 | 1992-04-07 | Yang Ki W | Rotary piston engine with slide gate |
| CN111779570A (en) * | 2020-07-20 | 2020-10-16 | 李玉春 | Eccentric rotor homogeneous compression ignition engine |
| WO2022165888A1 (en) * | 2021-02-04 | 2022-08-11 | 江苏大学 | Rotary engine |
| CN115045753A (en) * | 2022-07-07 | 2022-09-13 | 范杰 | Vane rotor engine |
| GB2605685A (en) * | 2021-02-04 | 2022-10-12 | Univ Jiangsu | Rotary engine |
-
1963
- 1963-06-13 GB GB23697/63A patent/GB1007250A/en not_active Expired
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5101782A (en) * | 1988-08-29 | 1992-04-07 | Yang Ki W | Rotary piston engine with slide gate |
| CN111779570A (en) * | 2020-07-20 | 2020-10-16 | 李玉春 | Eccentric rotor homogeneous compression ignition engine |
| WO2022165888A1 (en) * | 2021-02-04 | 2022-08-11 | 江苏大学 | Rotary engine |
| GB2605685A (en) * | 2021-02-04 | 2022-10-12 | Univ Jiangsu | Rotary engine |
| GB2605685B (en) * | 2021-02-04 | 2023-03-29 | Univ Jiangsu | Rotary engine |
| US11732640B2 (en) | 2021-02-04 | 2023-08-22 | Jiangsu University | Rotary engine |
| CN115045753A (en) * | 2022-07-07 | 2022-09-13 | 范杰 | Vane rotor engine |
| CN115045753B (en) * | 2022-07-07 | 2024-06-04 | 范杰 | Vane rotor engine |
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