GB346020A - Improvements in or relating to rotary engines, motors, compressors, power transmitters and the like, of the direct pressure type - Google Patents
Improvements in or relating to rotary engines, motors, compressors, power transmitters and the like, of the direct pressure typeInfo
- Publication number
- GB346020A GB346020A GB3674529A GB3674529A GB346020A GB 346020 A GB346020 A GB 346020A GB 3674529 A GB3674529 A GB 3674529A GB 3674529 A GB3674529 A GB 3674529A GB 346020 A GB346020 A GB 346020A
- Authority
- GB
- United Kingdom
- Prior art keywords
- piston
- oil
- working space
- casing
- compressors
- 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
- 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
- F01C1/30—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
- F01C1/34—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members
- F01C1/356—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the outer member
- F01C1/3562—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the outer member the inner and outer member being in contact along one line or continuous surface substantially parallel to the axis of rotation
- F01C1/3564—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the outer member the inner and outer member being in contact along one line or continuous surface substantially parallel to the axis of rotation the surfaces of the inner and outer member, forming the working space, being surfaces of revolution
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Applications Or Details Of Rotary Compressors (AREA)
Abstract
346,020. Force-feed lubricators. PHILLIPS, H. C., 45, Conduit Street, Gloucester. Nov. 30, 1929, Nos. 36745/29 and 29105/30. [Class 12 (iii).] A rotary engine, pump, compresser, or the like, which is adaptable for the transmission of power between a reciprocating piston and a rotary shaft, comprises an eccentric piston 3 which rotates within a casing but without contracting peripherally therewith and is engaged by a plurality of cylindrical rollers 6 which are located in recesses 5 in the casing and urged into contact with the piston so that a fluid chamber 7 varying in volume is provided. A rotary engine is shown in Fig. 1 in which the working fluid is admitted to and exhausted from the working space 7, bounded by the periphery of the eccentric piston 3 and the oppositely situated roller abutments 6, through timed valves 9, 10 actuated from the shaft 4 of the piston 3. Pipes 14 admit the pressure fluid to the abutment recesses 5 to act on the rollers 6. The lower space 8 may be utilized to draw in oil through an opening 16 and discharge it through a pipe fitted with a non-return valve. Fig. 13 shows a force feed lubrication arrangement in which oil from the upper working space 7 enters a duct 16 which is later cut off by the piston 3 and the oil is thereupon compressed by the differential plunger 40, the large area of which is exposed to the pressure in the working space 7. Specification 345,667, [Group XXVI], is referred to.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3674529A GB346020A (en) | 1929-11-30 | 1929-11-30 | Improvements in or relating to rotary engines, motors, compressors, power transmitters and the like, of the direct pressure type |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3674529A GB346020A (en) | 1929-11-30 | 1929-11-30 | Improvements in or relating to rotary engines, motors, compressors, power transmitters and the like, of the direct pressure type |
Publications (1)
Publication Number | Publication Date |
---|---|
GB346020A true GB346020A (en) | 1931-03-30 |
Family
ID=10390861
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3674529A Expired GB346020A (en) | 1929-11-30 | 1929-11-30 | Improvements in or relating to rotary engines, motors, compressors, power transmitters and the like, of the direct pressure type |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB346020A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2475391A (en) * | 1945-05-03 | 1949-07-05 | James P Johnson | Rotary movable abutment pump |
US2580561A (en) * | 1945-09-10 | 1952-01-01 | Link Belt Co | Hydraulic pulsator transmission system for converting rotary motion into reciprocatory motion |
US2658486A (en) * | 1947-04-23 | 1953-11-10 | Waide Hal De | Engine for transmitting forces developed therein |
US2665056A (en) * | 1951-06-20 | 1954-01-05 | Bendix Aviat Corp | Means for resiliently mounting vanes or frangible pump elements |
US3175469A (en) * | 1962-12-14 | 1965-03-30 | William R Kee | Hydraulic cam motor vane switching system |
US3194122A (en) * | 1962-12-14 | 1965-07-13 | William R Kee | Hydraulic cam motor vane switching system |
-
1929
- 1929-11-30 GB GB3674529A patent/GB346020A/en not_active Expired
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2475391A (en) * | 1945-05-03 | 1949-07-05 | James P Johnson | Rotary movable abutment pump |
US2580561A (en) * | 1945-09-10 | 1952-01-01 | Link Belt Co | Hydraulic pulsator transmission system for converting rotary motion into reciprocatory motion |
US2658486A (en) * | 1947-04-23 | 1953-11-10 | Waide Hal De | Engine for transmitting forces developed therein |
US2665056A (en) * | 1951-06-20 | 1954-01-05 | Bendix Aviat Corp | Means for resiliently mounting vanes or frangible pump elements |
US3175469A (en) * | 1962-12-14 | 1965-03-30 | William R Kee | Hydraulic cam motor vane switching system |
US3194122A (en) * | 1962-12-14 | 1965-07-13 | William R Kee | Hydraulic cam motor vane switching system |
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