GB997878A - Revolving piston machine with principal and auxiliary revolving pistons - Google Patents
Revolving piston machine with principal and auxiliary revolving pistonsInfo
- Publication number
- GB997878A GB997878A GB3849/62A GB384962A GB997878A GB 997878 A GB997878 A GB 997878A GB 3849/62 A GB3849/62 A GB 3849/62A GB 384962 A GB384962 A GB 384962A GB 997878 A GB997878 A GB 997878A
- Authority
- GB
- United Kingdom
- Prior art keywords
- piston
- pistons
- auxiliary
- point
- principal
- 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
- 238000001816 cooling Methods 0.000 abstract 4
- 239000012530 fluid Substances 0.000 abstract 2
- 239000000203 mixture Substances 0.000 abstract 2
- 238000010276 construction Methods 0.000 abstract 1
- 239000000110 cooling liquid Substances 0.000 abstract 1
- 239000007788 liquid Substances 0.000 abstract 1
- 239000000314 lubricant Substances 0.000 abstract 1
- 230000003014 reinforcing effect Effects 0.000 abstract 1
- 230000001360 synchronised effect Effects 0.000 abstract 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
- F01C1/00—Rotary-piston machines or engines
- F01C1/24—Rotary-piston machines or engines of counter-engagement type, i.e. the movement of co-operating members at the points of engagement being in opposite directions
- F01C1/26—Rotary-piston machines or engines of counter-engagement type, i.e. the movement of co-operating members at the points of engagement being in opposite directions of internal-axis type
-
- 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
- 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
- F02B2730/015—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 hinged to the housing
-
- 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
- F02B2730/017—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 rotating elements fixed to the housing or on the piston
-
- 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
- F02B2730/05—Internal-combustion engines with pistons rotating or oscillating with relation to the housing with pistons intermeshing as gear wheels; with helicoidal 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Compressors, Vaccum Pumps And Other Relevant Systems (AREA)
Abstract
997,878. Rotary piston machines. A. MENCIK VON ZEBINSKY. Feb. 1, 1962 [Feb. 6, 1961; Oct. 20, 1961], No. 3849/62. Heading F1F. A rotary piston machine operable as a pump, compressor, I.C., steam or gas engine, or a hydraulic or pneumatic motor, comprises a principal piston A, Fig. 1, and a co-operating auxiliary piston B mounted for rotation at constant speed in the same direction on spaced apart parallel shafts with the principal piston having a profile comprising the major portion having the same radius as a basic circle 2 and two circular arcs of radius R tangential thereto intersecting at a point 3 or meeting in an arc opposite to the mid point of the basic circle portion and the auxiliary piston having a profile which corresponds with the major portion of an auxiliary circle 6 centred on the basic circle and of radius less than two-thirds that of the basic circle and a circular arc centred on the intersection point 3 having a radius equal to that of the two circular arcs and wherein the perpendicular distance of a line 5, 5 joining the intersection points of the auxiliary circle with its circular arc from the common centre is at least two-tenths of the radius of the auxiliary circle. The construction of the profiles of the principal and auxiliary pistons are shown in Fig. 1. The housing surrounding the principal piston is circular having a radius equal to the distance of the common centre 1 from the intersection point 3. On clockwise rotation of the pistons, fluid is sucked in at E after the passage of the point 3 and is compressed during the following stroke and forced out at D. In Fig. 2, a further auxiliary piston B 1 is fitted, providing an abutment between chambers V 2 , V 1 . During clockwise rotation of the pistons, fuel-air mixture sucked into chamber V 1 through inlet D during the preceding revolution is compressed and pushed out at E by the point 3 and forced into a container F. The fuel-air mixture is then admitted through the inlet G after the passage of the point 3 and ignited. It then expands in the chamber V 2 and is finally exhausted through outlet H. The pistons are interconnected by gearing to provide synchronised movement therebetween and permit the use of contactless seals and the omission of lubricant between the pistons with the consequent non-pollution of the working fluid with oil. Seals inserted in dove-tail grooves at the point 3 and the intersection points on the auxiliary pistons may however be fitted or alternatively labyrinth seals, Fig. 5b, may be included over an arcuate portion of the piston profile located at point 3. The gearing may comprise a gear on each piston and an intermediate gear engaging those gears mounted on a shaft offset from a straight line joining the piston axes with the gear wheels slightly conical and the intermediate wheel axially adjustable to take up backlash and wear. The embodiment shown in Fig. 2, may be adapted to operate as a two-stage compressor. Air sucked in at G being compressed in the chamber V 2 and then exhausted through H into an inter-cooler. It is re-admitted at D and further compressed in the chamber V 1 before passing through the outlet E to its point of use. Several principal pistons, three in Fig. 6, may be mounted on a common shaft 1 separated by intermediate side walls with the points 3 angularly staggered and a corresponding number of co-operating auxiliary pistons mounted on a common shaft 7. The machine may be liquid or air cooled. In Fig. 9, cooling air is admitted at L 1 on either side of the principal piston 2, passing over the bearings 31 and through cooling fins 27 to cool the hub and central web of the piston. It is then directed by fins 26 over side flanges 25 of the piston and thence through fins 29 between the machine housing C 2 and an outer-casing to finally leave at L 2 . In another embodiment, Fig. 10, cooling air entering at L 1 divides into two streams to cool both the shaft 1 and hub 1b and the piston periphery. Parts 33 may be designed as reinforcing ribs and cooling liquid or air may circulate through pockets 32 in the housing. A separate impeller may also be used to circulate the cooling air. Further embodiments are described in Figs. 7 and 8 (not shown) in which the profiles of the principal and auxiliary pistons are somewhat modified.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DEP26526A DE1129962B (en) | 1961-02-06 | 1961-02-06 | Rotary piston machine with main and secondary rotary piston |
DEP0028063 | 1961-10-20 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB997878A true GB997878A (en) | 1965-07-07 |
Family
ID=25990037
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3849/62A Expired GB997878A (en) | 1961-02-06 | 1962-02-01 | Revolving piston machine with principal and auxiliary revolving pistons |
Country Status (5)
Country | Link |
---|---|
AT (1) | AT261315B (en) |
BE (1) | BE613138A (en) |
CH (1) | CH407164A (en) |
GB (1) | GB997878A (en) |
LU (1) | LU41178A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1989001563A1 (en) * | 1987-08-21 | 1989-02-23 | Loeytty Ari Veli Olavi | Rotary machine |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102011001551B4 (en) * | 2011-03-25 | 2017-11-02 | Philipp Diem | Internal combustion engine with a rotatable about its axis rotor |
-
1962
- 1962-01-26 BE BE613138A patent/BE613138A/en unknown
- 1962-01-31 LU LU41178D patent/LU41178A1/xx unknown
- 1962-02-01 GB GB3849/62A patent/GB997878A/en not_active Expired
- 1962-02-02 CH CH125662A patent/CH407164A/en unknown
- 1962-02-05 AT AT92062A patent/AT261315B/en active
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1989001563A1 (en) * | 1987-08-21 | 1989-02-23 | Loeytty Ari Veli Olavi | Rotary machine |
Also Published As
Publication number | Publication date |
---|---|
LU41178A1 (en) | 1962-03-31 |
AT261315B (en) | 1968-04-25 |
BE613138A (en) | 1962-05-16 |
CH407164A (en) | 1966-02-15 |
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