GB526374A - Rotary internal combustion engine - Google Patents

Rotary internal combustion engine

Info

Publication number
GB526374A
GB526374A GB8196/39A GB819639A GB526374A GB 526374 A GB526374 A GB 526374A GB 8196/39 A GB8196/39 A GB 8196/39A GB 819639 A GB819639 A GB 819639A GB 526374 A GB526374 A GB 526374A
Authority
GB
United Kingdom
Prior art keywords
rotor
ducts
chambers
engine
vanes
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
GB8196/39A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of GB526374A publication Critical patent/GB526374A/en
Expired legal-status Critical Current

Links

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
    • 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
    • F02B2730/00—Internal combustion engines with pistons rotating or oscillating with relation to the housing
    • F02B2730/01—Internal combustion engines with pistons rotating or oscillating with relation to the housing with one or more pistons in the form of a disk or rotor rotating with relation to the housing; with annular working chamber
    • F02B2730/012—Internal combustion engines with pistons rotating or oscillating with relation to the housing with one or more pistons in the form of a disk or rotor rotating with relation to the housing; with annular working chamber with vanes sliding in the piston
    • F02B2730/013—Vanes fixed in the centre of the housing; Excentric rotors
    • 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

Abstract

526,374. Rotary engines. TIPS, M. March 14, 1939, No. 8196. Convention date, March 18, 1938. [Class 110 (ii)] An internal combustion engine comprises a rotor 12 eccentrically positioned in a stator 10, having vanes 22 pivoted on a fixed shaft 21 which is concentric with the inner bore of the casing. The vanes slide between members 25 and co-operate with a rotary abutment 49 driven by bevel gearing, placed between inlet and exhaust ports 48, 47. The rotor is mounted in bearings 15, 16, in the casing end walls 17, 18. Members 25 are mortised cylinders provided with packing pieces 36 at the sides and edges. Packing pieces 37 in the tip of each vane are balanced centrifugally (Fig. 4) by means of a weight 39 through rocking bars 41 pivoted in fixed partitions' 38. A spring 43 presses the weight 39 inwards. An adjusting screw 45 is provided. Further packings 46, 66, 67 are provided. Combustion chambers 52 extend transversely through the rotor between each pair of vanes and terminate in ducts 53. Ducts 54 in the rotor allow compressed air, or fuel gas, to pass into a combustion chamber 52 when in augment. Packing 55 is provided, to be forced against the stator wall. When operating as a diesel engine, oil is injected through the ducts 53. Sparking plugs 57 may be used. Cooling oil is forced by a pump 59 through a pipe 61 into chambers 58 which surround the combustion chambers, and returns to the pump via ducts 65. Grooves 68 in the walls 19, 20, allow compressed air, or fuel gas, to fill chambers 52. The capacity of a compression chamber is adjusted by means of a cylinder 70 with a piston 71 on a threaded spindle which may be rotated by a handwheel. Passages 73 connect the cylinder with the interior of the engine. Where the engine is fitted to an aircraft, bullets may be fired through the hollow shaft 21.
GB8196/39A 1938-03-18 1939-03-14 Rotary internal combustion engine Expired GB526374A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
BE526374X 1938-03-18

Publications (1)

Publication Number Publication Date
GB526374A true GB526374A (en) 1940-09-17

Family

ID=3871557

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8196/39A Expired GB526374A (en) 1938-03-18 1939-03-14 Rotary internal combustion engine

Country Status (1)

Country Link
GB (1) GB526374A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3637332A (en) * 1970-07-28 1972-01-25 United Aircraft Corp Variable compression means for a rotary engine
CN105888826A (en) * 2016-05-09 2016-08-24 张立 Novel simple internal combustion engine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3637332A (en) * 1970-07-28 1972-01-25 United Aircraft Corp Variable compression means for a rotary engine
CN105888826A (en) * 2016-05-09 2016-08-24 张立 Novel simple internal combustion engine

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