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GB1007250A - A rotary internal combustion engine - Google Patents

A rotary internal combustion engine

Info

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
Application number
GB23697/63A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
RICHARD LESLIE TERRY
Original Assignee
RICHARD LESLIE TERRY
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by RICHARD LESLIE TERRY filed Critical RICHARD LESLIE TERRY
Priority to GB23697/63A priority Critical patent/GB1007250A/en
Publication of GB1007250A publication Critical patent/GB1007250A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B53/00Internal-combustion aspects of rotary-piston or oscillating-piston engines
    • F02B53/04Charge admission or combustion-gas discharge
    • F02B53/08Charging, e.g. by means of rotary-piston pump
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/02Engines characterised by their cycles, e.g. six-stroke
    • F02B2075/022Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle
    • F02B2075/027Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle four
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving 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.
GB23697/63A 1963-06-13 1963-06-13 A rotary internal combustion engine Expired GB1007250A (en)

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)

* Cited by examiner, † Cited by third party
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

Cited By (8)

* Cited by examiner, † Cited by third party
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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