GB632421A - Improvements in rotary internal combustion engines, pumps or motors - Google Patents
Improvements in rotary internal combustion engines, pumps or motorsInfo
- Publication number
- GB632421A GB632421A GB25629/47A GB2562947A GB632421A GB 632421 A GB632421 A GB 632421A GB 25629/47 A GB25629/47 A GB 25629/47A GB 2562947 A GB2562947 A GB 2562947A GB 632421 A GB632421 A GB 632421A
- Authority
- GB
- United Kingdom
- Prior art keywords
- cylinder
- piston
- pistons
- block
- axes
- 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
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
- F02B75/00—Other engines
- F02B75/26—Engines with cylinder axes coaxial with, or parallel or inclined to, main-shaft axis; Engines with cylinder axes arranged substantially tangentially to a circle centred on main-shaft axis
-
- 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
- F01C3/00—Rotary-piston machines or engines with non-parallel axes of movement of co-operating members
- F01C3/06—Rotary-piston machines or engines with non-parallel axes of movement of co-operating members the axes being arranged otherwise than at an angle of 90 degrees
-
- 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
- F02B2075/025—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle two
-
- 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)
- Hydraulic Motors (AREA)
Abstract
632,421. Rotary engines and pumps. McCULLOCH, M. L. Sept: 19, 1947, No. 25629. [Class 110(ii)] The invention relates to engines and pumps having cylinders and pistons moving in circles about axes inclined to one another to cause relative reciprocation between pistons and cylinders. Fig. 1 shows a pump with inlet and outlet ports 17, 18 respectively, a block containing cylinders 15 and revolving on an axis 7, and pistons 12, carried by a disc 8 which revolves on an axis 10. The centres of the spherical pistons 12 lie in a plane 14 which intersects the intersection of axes 7 and 10. The disc 8 is driven through a connection 20 and the shaft in bearings 5, to which the cylinder block is keyed, by means of gears 19. There are clearances between pistons and cylinder bores. Fig. 3 shows an internal-combustion engine in which a cylinder block 20a, 20b, 20c rotates about an axis 41 by means of rollers 42 which engage the flat end walls. Pistons P, carried by supports 24, in a member 33, rotate about an axis 23. During rotation of the two parts on axes 41, 23 the pistons reciprocate in cylinders 28. In Fig. 3, compressed gas above the right-hand piston has just been fired and gas admitted to a space 26 from a port 30. During the down-stroke, compressed gas from 26 passes through ports 31, 34, when they are in alignment, into the hollow sphere 33 and out through an upper port 34 to the space above the descending piston to scavenge the cylinder, burnt gases passing through a port 32 to atmosphere. When the piston rises in the cylinder, the cycle is repeated in the upper part of the cylinder. Each piston is made up of three parts, Fig. 5, a piston support 24, a floating member 35 in the form of a hollow frustrum of a cone and a sealing member 36 fitting over the member 35 and having curved walls which engage the side walls of the cylinder. The member 36 is in two parts joined by a bar 37 which extends through a recess 38 in the support 24. The bar is located by means of a pin 38a engaging in a slot 39. The lower part of the piston is cut away at 40 to fit over a wall 27 at the lower part of the stroke. Where piston rings are used, pivoted counterweights may be provided on each piston to counterbalance centrifugal force. A variable - stroke pump may be formed from a cylinder block rotating in a fixed casing and provided with a number of cylinders having curved axes, the centre of curvature of these axes being the centre of the block. A spherical recess is formed centrally of the block and a parallel-sided passage extends from the centre spherical recess to each cylinder. A valve plate and inlet and delivery ports are formed in the casing at each end of the block making a separate pump associated with each end of the cylinder block. Each pump operates as shown in Fig. 1 and in addition, the delivery may be varied by moving the motor in its mounting and thus varying the inclination of the axes of rotation without varying the speed of the motor. Reversal of flow of fluid may be secured, thus. The two pumps formed on opposite ends of the block may be connected in series or in parallel.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB25629/47A GB632421A (en) | 1947-09-19 | 1947-09-19 | Improvements in rotary internal combustion engines, pumps or motors |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB25629/47A GB632421A (en) | 1947-09-19 | 1947-09-19 | Improvements in rotary internal combustion engines, pumps or motors |
Publications (1)
Publication Number | Publication Date |
---|---|
GB632421A true GB632421A (en) | 1949-11-28 |
Family
ID=10230758
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB25629/47A Expired GB632421A (en) | 1947-09-19 | 1947-09-19 | Improvements in rotary internal combustion engines, pumps or motors |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB632421A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2270440A1 (en) * | 1974-05-06 | 1975-12-05 | Searle Russell | Swash-plate engine with two pistons per cylinder - have sealing surfaces piston ring forming part of sphere |
US5636561A (en) * | 1992-10-30 | 1997-06-10 | Felice Pecorari | Volumetric fluid machine equipped with pistons without connecting rods |
WO2005012692A1 (en) * | 2003-07-25 | 2005-02-10 | VOGLAIRE, Hélène | Multicylinder barrel-type engine |
EP2098702A1 (en) * | 2006-12-29 | 2009-09-09 | Yau Cheung Kwok | Top rotating engine |
-
1947
- 1947-09-19 GB GB25629/47A patent/GB632421A/en not_active Expired
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2270440A1 (en) * | 1974-05-06 | 1975-12-05 | Searle Russell | Swash-plate engine with two pistons per cylinder - have sealing surfaces piston ring forming part of sphere |
US5636561A (en) * | 1992-10-30 | 1997-06-10 | Felice Pecorari | Volumetric fluid machine equipped with pistons without connecting rods |
WO2005012692A1 (en) * | 2003-07-25 | 2005-02-10 | VOGLAIRE, Hélène | Multicylinder barrel-type engine |
EP2098702A1 (en) * | 2006-12-29 | 2009-09-09 | Yau Cheung Kwok | Top rotating engine |
US20100018495A1 (en) * | 2006-12-29 | 2010-01-28 | Yau Cheung Kwok | Gyroscopic Rotary Engine |
EP2098702A4 (en) * | 2006-12-29 | 2011-10-19 | Yau Cheung Kwok | Top rotating engine |
US8297239B2 (en) * | 2006-12-29 | 2012-10-30 | Yau Cheung Kwok | Gyroscopic rotary engine |
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