GB893312A - Improvements in or relating to multi-unit arrangements for four-stroke rotary pistonengines - Google Patents

Improvements in or relating to multi-unit arrangements for four-stroke rotary pistonengines

Info

Publication number
GB893312A
GB893312A GB33817/59A GB3381759A GB893312A GB 893312 A GB893312 A GB 893312A GB 33817/59 A GB33817/59 A GB 33817/59A GB 3381759 A GB3381759 A GB 3381759A GB 893312 A GB893312 A GB 893312A
Authority
GB
United Kingdom
Prior art keywords
ports
rotors
units
inlet
shaft
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
GB33817/59A
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.)
Wankel GmbH
Audi AG
Original Assignee
Wankel GmbH
NSU Motorenwerke AG
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 Wankel GmbH, NSU Motorenwerke AG filed Critical Wankel GmbH
Publication of GB893312A publication Critical patent/GB893312A/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
    • F02B53/00Internal-combustion aspects of rotary-piston or oscillating-piston engines
    • F02B2053/005Wankel 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
    • F02B2730/018Internal-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 piston rotating around an axis passing through the gravity centre, this piston or the housing rotating at the same time around an axis parallel to the first axis
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B3/00Engines characterised by air compression and subsequent fuel addition
    • F02B3/06Engines characterised by air compression and subsequent fuel addition with compression ignition
    • 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)
  • Reciprocating Pumps (AREA)
  • Hydraulic Motors (AREA)
  • Applications Or Details Of Rotary Compressors (AREA)

Abstract

893,312. Rotary piston engines. N.S.U. MOTORENWERKE A.G. Oct. 6, 1959 [Oct. 7, 1958], No. 33817/59. Class 110 (2). A two-unit four-stroke rotary piston engine, in which each unit comprises a stationary housing the inner peripheral wall of which is formed as a number of curves meeting in lobes, a rotor having a number, one more than the number of said curves, of apices in continuous sliding contact with the said inner peripheral wall, the rotor rotating on a crank-pin or eccentric of a shaft journalled centrally on the housing, at a speed different from the shaft, and inlet and exhaust ports, controlled by the rotor, in the walls of the housing, is characterized by the two units being so combined that the contours of the two peripheral walls and the two sets of inlet and exhaust ports are in axial alignment, whilst the two sets of crankpins and rotors thereon are displaced by an angle of 180 degrees. Fig. 1 shows diagrammatically two units with a common crank-shaft 4, the housings 1 having two lobes and the rotors 7, 8 each having three apices. The rotors rotate planet-wise about the centres 9, 10 of crank-pins on the shaft 4 which rotates on a fixed axis 3, an internal toothed gear on each rotor meshing with a stationary gear on the end wall of each housing. The gear ratio produces three revolutions of the shaft 4 for each revolution of the rotor. The inlet ports 12, exhaust ports 13 and lobes are in axial alignment, but the rotors are relatively displaced through 180 degrees to produce an ignition every half revolution. Two such units may be coupled with the housing contours and ports in axial alignment and the two crank-shafts displaced relatively by 180 degrees, in which case a dynamic balance results and ignition occurs every half revolution in two cylinders simultaneously; or the two crankshafts are displaced by 90 degrees to produce an ignition every quarter-revolution but it is then necessary to restore dynamic balance by counterweights. Alternatively, the crank-shafts are relatively displaced by 90 degrees, the housing contours and ports of the two units also being displaced by a right-angle, in which case balance is achieved but independent inlet and exhaust manifolds are required for the two units. Fig. 7 shows a two-unit engine with two working chambers 23, 24 separated by a wall 22 having inlet channels and ports for the two units. The rotors 77, 78 rotate on eccentrics 55, 56 which are connected by projecting sleeves 55<SP>1</SP>, 56<SP>1</SP>, a screwed inner sleeve 80 and a bolt 85. A shaft 83 is splined into the eccentric 56, and the sleeve 55<SP>1</SP> is journalled in a bearing 14 carried by the wall 22. The exhaust ports 13 in the aligned contours of the peripheral walls, and the inlet ports, are also axially aligned. Oil ducts convey oil into the apex portions of the rotors to act as a circulating coolant. Internal gears 25 in the rotors mesh with stationary gears 26, and balance weights 87, 88 are provided. The wall member 22 may be made in two parts, one part containing the inlet ports and passages. The two parts have mating curved surfaces which pass approximately diametrically through the axis of rotation, the two parts being bolted together to form a working whole. Coolant passages are provided in the end and central walls. Specifications 791,689 and 892,476 are referred to.
GB33817/59A 1958-10-07 1959-10-06 Improvements in or relating to multi-unit arrangements for four-stroke rotary pistonengines Expired GB893312A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DEN15676A DE1153207B (en) 1958-10-07 1958-10-07 Rotary piston internal combustion engine

Publications (1)

Publication Number Publication Date
GB893312A true GB893312A (en) 1962-04-04

Family

ID=7340072

Family Applications (1)

Application Number Title Priority Date Filing Date
GB33817/59A Expired GB893312A (en) 1958-10-07 1959-10-06 Improvements in or relating to multi-unit arrangements for four-stroke rotary pistonengines

Country Status (4)

Country Link
BE (1) BE577938A (en)
CH (1) CH373593A (en)
DE (1) DE1153207B (en)
GB (1) GB893312A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3620656A (en) * 1968-10-02 1971-11-16 Rolls Royce Rotary piston engines

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1158747B (en) * 1959-11-17 1963-12-05 Curtiss Wrigth Corp Rotary piston machine, in particular internal combustion engine
DE1158751B (en) * 1960-09-16 1963-12-05 Curtiss Wright Corp Bearing training for multiple rotary piston internal combustion engines
DE1296656B (en) * 1961-11-22 1969-06-04 Krupp Gmbh Multiple rotary piston machine
DE19601499A1 (en) * 1996-01-17 1996-06-27 Adolf Dipl Ing Klaus Bearing pressure compensation for rotary piston engine
DE10300747B4 (en) * 2003-01-17 2008-06-19 Rinsum, Cornelis van, Dipl.-Ing. Rotary piston internal combustion engine with two triangular rotary pistons

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10796C (en) * P. KIRCHHOFF in Mittweida, Sachsen Changes to the OLDHAM 'ventilator (addition to P. R. 8689)
AT69273B (en) * 1912-09-10 1915-07-10 Siemens Schuckertwerke Wien Eccentric pump.
FR673265A (en) * 1929-04-13 1930-01-13 Improvements to rotary machines, such as pumps and motors
US2189976A (en) * 1937-01-27 1940-02-13 Lavaud Dimitrl Sensaud De Rotary engine
DE715217C (en) * 1939-06-25 1941-12-17 Fritz Drabert Dr Ing Rotary piston compressor with elliptical housing cross-section
GB583035A (en) * 1943-08-20 1946-12-05 Bernard Maillard A rotary machine generating variable volumes

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3620656A (en) * 1968-10-02 1971-11-16 Rolls Royce Rotary piston engines

Also Published As

Publication number Publication date
BE577938A (en) 1959-08-17
CH373593A (en) 1963-11-30
DE1153207B (en) 1963-08-22

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