GB406051A - Improvements in and relating to compressors for air and gases - Google Patents
Improvements in and relating to compressors for air and gasesInfo
- Publication number
- GB406051A GB406051A GB2347432A GB2347432A GB406051A GB 406051 A GB406051 A GB 406051A GB 2347432 A GB2347432 A GB 2347432A GB 2347432 A GB2347432 A GB 2347432A GB 406051 A GB406051 A GB 406051A
- Authority
- GB
- United Kingdom
- Prior art keywords
- air
- compressors
- gases
- relating
- oil
- 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
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C29/00—Component parts, details or accessories of pumps or pumping installations, not provided for in groups F04C18/00 - F04C28/00
- F04C29/0007—Injection of a fluid in the working chamber for sealing, cooling and lubricating
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physical Or Chemical Processes And Apparatus (AREA)
Abstract
406,051. Cooling rotary compressors. OGILVIE, H., 38, St. Augustine's Road, Camden Square, London. Aug. 22, 1932, No. 23474. [Class 110 (ii).] Oil is admitted as a jet or jets through orifices 8 in the inlet of a rotary compressor or at points of low compression in the barrel, to cool the air. The oil is supplied from a pipe 9.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2347432A GB406051A (en) | 1932-08-22 | 1932-08-22 | Improvements in and relating to compressors for air and gases |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2347432A GB406051A (en) | 1932-08-22 | 1932-08-22 | Improvements in and relating to compressors for air and gases |
Publications (1)
Publication Number | Publication Date |
---|---|
GB406051A true GB406051A (en) | 1934-02-22 |
Family
ID=10196201
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2347432A Expired GB406051A (en) | 1932-08-22 | 1932-08-22 | Improvements in and relating to compressors for air and gases |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB406051A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3765392A (en) * | 1971-03-04 | 1973-10-16 | Audi Ag | Rotary piston combustion engine |
DE3209035A1 (en) * | 1981-03-13 | 1982-09-30 | Sullair Technology AB, 11653 Stockholm | METHOD AND DEVICE FOR INTERCOOLING IN AN OIL INJECTED MULTI-STAGE SCREW COMPRESSOR |
-
1932
- 1932-08-22 GB GB2347432A patent/GB406051A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3765392A (en) * | 1971-03-04 | 1973-10-16 | Audi Ag | Rotary piston combustion engine |
DE3209035A1 (en) * | 1981-03-13 | 1982-09-30 | Sullair Technology AB, 11653 Stockholm | METHOD AND DEVICE FOR INTERCOOLING IN AN OIL INJECTED MULTI-STAGE SCREW COMPRESSOR |
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