GB964327A - A rotary internal combustion engine - Google Patents
A rotary internal combustion engineInfo
- Publication number
- GB964327A GB964327A GB34310/60A GB3431060A GB964327A GB 964327 A GB964327 A GB 964327A GB 34310/60 A GB34310/60 A GB 34310/60A GB 3431060 A GB3431060 A GB 3431060A GB 964327 A GB964327 A GB 964327A
- Authority
- GB
- United Kingdom
- Prior art keywords
- piston
- sleeve
- blade
- rotary
- oct
- 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
- 238000002485 combustion reaction Methods 0.000 title abstract 2
- 239000000567 combustion gas Substances 0.000 abstract 1
- 230000006835 compression Effects 0.000 abstract 1
- 238000007906 compression Methods 0.000 abstract 1
- 239000007789 gas Substances 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
- F01C1/30—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
-
- 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
- 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
- F02B2730/011—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 sliding in the housing
-
- 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)
- Output Control And Ontrol Of Special Type Engine (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
Abstract
964,327. Rotary internal combustion engines. F. J. HOGGUER. Oct. 6, 1960 [Oct. 13, 1959], No. 34310/60. Addition to 929,940. Heading F1F. A rotary I.C. engine comprises a rotary piston 9, Fig. 3, eccentrically arranged on a shaft 6, a portion 10, Fig. 1, of the piston is concentric with the shaft, Fig. 1, which permanently bears against the inner side of the housing 1 and a portion 11 is eccentric thereto. The cylindrical housing has four cylindrical guide means 4 spaced over its periphery in each of which a sleeve 5 is slidable axially. Each sleeve in a transverse direction comprises a bottom 7 extending over three quarters of its periphery and radially inwardly directed wings 7<SP>1</SP> and 7<SP>11</SP> provided with a pin 8 which engage the disc-shaped piston, helical compressor springs 12 ensure permanent contact between them. Laterally of each sleeve or compression chamber 15 is provided, formed by a casing 16 with a spark plug hole provided in the end wall 17. A radially extending blade 25 is located adjacent the piston portion 10, the combustion gases are directed against this causing the piston to rotate. After the gases have given their energy to the blade which is fixed with a pin 28, they leave through the axially bent branch 29 of the blade and the eccentric opening 30 in the side wall 23 of the piston and are discharged through the outlet 31.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
NL244287 | 1959-10-13 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB964327A true GB964327A (en) | 1964-07-22 |
Family
ID=19751975
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB34310/60A Expired GB964327A (en) | 1959-10-13 | 1960-10-06 | A rotary internal combustion engine |
Country Status (4)
Country | Link |
---|---|
BE (1) | BE590130A (en) |
CH (1) | CH393831A (en) |
DE (1) | DE1426009A1 (en) |
GB (1) | GB964327A (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102005038302A1 (en) * | 2005-08-11 | 2007-02-15 | Garri Dr. Alexandrow | Automotive rotary piston engine has rotating cylinder with rising and falling convex surfaces and chamber slide separators |
-
1960
- 1960-04-25 BE BE590130A patent/BE590130A/en unknown
- 1960-04-28 CH CH483360A patent/CH393831A/en unknown
- 1960-04-29 DE DE19601426009 patent/DE1426009A1/en active Pending
- 1960-10-06 GB GB34310/60A patent/GB964327A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
DE1426009A1 (en) | 1968-11-21 |
BE590130A (en) | 1960-10-25 |
CH393831A (en) | 1965-06-15 |
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