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 pistonenginesInfo
- 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
Links
- 230000002093 peripheral effect Effects 0.000 abstract 4
- 239000002826 coolant Substances 0.000 abstract 2
- 230000013011 mating Effects 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
-
- 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
- F02B2053/005—Wankel 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
- 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
-
- 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
- F02B2730/018—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 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
-
- 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
- F02B3/00—Engines characterised by air compression and subsequent fuel addition
- F02B3/06—Engines characterised by air compression and subsequent fuel addition with compression ignition
-
- 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)
- 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.
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)
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)
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)
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 |
-
1958
- 1958-10-07 DE DEN15676A patent/DE1153207B/en active Pending
-
1959
- 1959-04-16 CH CH7212459A patent/CH373593A/en unknown
- 1959-04-21 BE BE577938A patent/BE577938A/en unknown
- 1959-10-06 GB GB33817/59A patent/GB893312A/en not_active Expired
Cited By (1)
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 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US3062435A (en) | Multi-unit rotary engine | |
GB973134A (en) | Improvements in and relating to internal combustion engines | |
US5123394A (en) | Rotary reciprocating internal combustion engine | |
US2076334A (en) | Diesel engine | |
GB1231701A (en) | ||
US1831263A (en) | Internal combustion engine | |
GB893312A (en) | Improvements in or relating to multi-unit arrangements for four-stroke rotary pistonengines | |
GB1402593A (en) | Reciprocating piston machine | |
US3477415A (en) | Rotary piston engine | |
US3268156A (en) | Engine or power driven machine with the rotary piston | |
US3955541A (en) | Rotary internal combustion engine with uniformly rotating pistons cooperating with reaction elements having a varying speed of rotation | |
RU2472017C2 (en) | Rotary engine | |
GB1218579A (en) | Rotary-piston machines | |
US1033701A (en) | Rotary explosion-engine. | |
US2413590A (en) | Arcuate piston | |
US4021160A (en) | Orbital motor | |
GB355136A (en) | Improvements in and relating to reciprocating engines | |
GB1245323A (en) | Improvements in rotary machines such as internal combustion engines and compressors | |
FR2311183A1 (en) | Multi cylinder rotary internal combustion engine - has cylinder block rotating in opposite direction to single throw crankshaft | |
US1299777A (en) | Explosive-engine. | |
GB1259801A (en) | A nutating piston fluid machine | |
US3751193A (en) | Rotary engine with intermeshed disks incorporating adjustable gear structure | |
GB499553A (en) | Rotary internal combustion engine | |
FR2243608A5 (en) | I.C. engine with radial rotating pistons - crankshaft/rotor speed ratio is equal to number of cylinders | |
US3648671A (en) | Modified internal combustion engine |