GB1065001A - Improvements in or relating to rotary internal combustion engines - Google Patents

Improvements in or relating to rotary internal combustion engines

Info

Publication number
GB1065001A
GB1065001A GB26121/62A GB2612162A GB1065001A GB 1065001 A GB1065001 A GB 1065001A GB 26121/62 A GB26121/62 A GB 26121/62A GB 2612162 A GB2612162 A GB 2612162A GB 1065001 A GB1065001 A GB 1065001A
Authority
GB
United Kingdom
Prior art keywords
shafts
discs
semi
casing
circular
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
GB26121/62A
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.)
ARNOLD BRADBURY TOTAL 9919
Original Assignee
ARNOLD BRADBURY TOTAL 9919
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 ARNOLD BRADBURY TOTAL 9919 filed Critical ARNOLD BRADBURY TOTAL 9919
Priority to GB26121/62A priority Critical patent/GB1065001A/en
Publication of GB1065001A publication Critical patent/GB1065001A/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
    • 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B2730/00Internal-combustion engines with pistons rotating or oscillating with relation to the housing
    • F02B2730/01Internal-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
    • 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)
  • Valve-Gear Or Valve Arrangements (AREA)

Abstract

1,065,001. Rotary I. C. engines. A. BRADLEY. Oct. 7, 1963 [July 6, 1962], No. 26121/62. Heading F1F. In a rotary I. C. engine of the nutating-disc and inclined-shaft type a spherical cavity 12 in a casing 11 contains a set of nutating pistons constituted by a circular disc 13 and semi-circular discs 14, 15 whose straight edges 14a, 15a are pivoted on either side of the disc 13 at rightangles to each other. Rotatable shafts 18, 19 are attached to the semi-circular discs 14, 15, respectively; and carry a chain-wheel 26 and a flywheel 27, respectively. Fuel-air mixture is drawn through an inlet port 21 and compressed between the discs before it is ignited by one or other of two spark-plugs 24, 25, the spent products of combustion being ejected through one or other of two exhaust ports 22, 23. The inlet and exhaust ports are controlled by valves (not shown), which may be operated by cams (not shown) driven by either of the shafts 18, 19, and the spark-plugs may be connected to a magneto, or an equivalent device, coupled to the chainwheel 26. In each of the four working spaces between the discs 13, 14, 15 a complete cycle of induction, compression, expansion and exhaust phases is performed during two successive revolutions of the shafts 18, 19. The engine may be modified so that the ports 22, 23 are replaced by slots or slit-like ports 31, these ports and the inlet port 21 being controlled by the discs 13, 14, 15 so that a complete cycle is performed in each of the working spaces per revolution of the shafts. The shaft 18 serves as a poweroutput-shaft. A rotary I.C. engine, which is generally similar to that shown, has rotatable shafts (40, 43), Figs. 5 and 6 (not shown), in place of the shafts 18, 19, rotary valve-members (42, 44) for controlling exhaust ports (47) being carried by said shafts, respectively. An inlet port (48) for fuel-air mixture is formed by notches in two mutually abutting halves (35, 36) of the casing. The shaft (40) serves as a power-output shaft and also carries a flywheel 41 whereas the shaft (43) also carries a so-called "rotor arm" (45) for controlling the ignition system. Spark-plugs are lodged in screw-threaded holes (72) in the casing. The pistons are constituted by a circular disc (60) and semi-circular discs (62, 63) attached thereto by mutually perpendicular pairs of pivot pins (68), the radially-outermost ends of the pins being in engagement with part-spherical caps (67) fixed to the semi-circular discs and lodged in recesses in the perimeter of the circular disc. The straight edge of each semi-circular disc engages with a V-shaped groove formed in a diametral bar (73) attached to the adjacent face of the circular disc. Sealing strips (69, 71) are provided on the caps (67) and the part-spherical portions (64) of the semi-circular discs respectively. Lubricating passages (58) in the shafts (40, 43) communicate with further passages (58a, 58b) in the pistons to effect lubrication of the peripheral portions of the discs. Passages (54) in the casing are supplied with cooling water through an inlet (55) in one half of the casing, the water being removed from said passages through an outlet (56) in the other half of the casing. A complete cycle is performed in each working space during two successive revolutions of the shafts.
GB26121/62A 1962-07-06 1962-07-06 Improvements in or relating to rotary internal combustion engines Expired GB1065001A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB26121/62A GB1065001A (en) 1962-07-06 1962-07-06 Improvements in or relating to rotary internal combustion engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB26121/62A GB1065001A (en) 1962-07-06 1962-07-06 Improvements in or relating to rotary internal combustion engines

Publications (1)

Publication Number Publication Date
GB1065001A true GB1065001A (en) 1967-04-12

Family

ID=10238721

Family Applications (1)

Application Number Title Priority Date Filing Date
GB26121/62A Expired GB1065001A (en) 1962-07-06 1962-07-06 Improvements in or relating to rotary internal combustion engines

Country Status (1)

Country Link
GB (1) GB1065001A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007039142A1 (en) * 2007-08-18 2009-02-19 Sergej Karakcheyev Hub extrusion machine, particularly swash plate machine, has two sectional areas that are merged at front side in virtual spherical diameter axis, and are attached to circular front surface of swash element in sealing manner

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007039142A1 (en) * 2007-08-18 2009-02-19 Sergej Karakcheyev Hub extrusion machine, particularly swash plate machine, has two sectional areas that are merged at front side in virtual spherical diameter axis, and are attached to circular front surface of swash element in sealing manner

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