GB180299A - Improvements in rotors for centrifugal compressors - Google Patents
Improvements in rotors for centrifugal compressorsInfo
- Publication number
- GB180299A GB180299A GB5412/22A GB541222A GB180299A GB 180299 A GB180299 A GB 180299A GB 5412/22 A GB5412/22 A GB 5412/22A GB 541222 A GB541222 A GB 541222A GB 180299 A GB180299 A GB 180299A
- Authority
- GB
- United Kingdom
- Prior art keywords
- ring
- blades
- blade
- rotors
- rings
- 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
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/28—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
- F04D29/30—Vanes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/28—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
- F04D29/284—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for compressors
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
180,299. Akt.-Ges. Brown, Boveri, et Cie. May 14, 1922, [Convention date]. Disc - supported - blade fans; impeller blades. - The rotor of a centrifugal compressor has a plurality of rings of blades b, c, d, arranged concentrically with an annular gap e, f between adjacent rings, of such width as to allow the streams of fluid from each ring to reunite, if eddy wedges are formed in any blade ring, before entering the next blade-ring. The blades of one ring may be in staggered relation to those of the adjacent ring.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH180299X | 1921-05-14 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB180299A true GB180299A (en) | 1922-10-26 |
Family
ID=4429887
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB5412/22A Expired GB180299A (en) | 1921-05-14 | 1922-02-23 | Improvements in rotors for centrifugal compressors |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB180299A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2781963A (en) * | 1950-06-16 | 1957-02-19 | Guy S Faber | Blower |
US3197124A (en) * | 1962-04-03 | 1965-07-27 | Sallou Jean | Centrifugal pump impellers |
US3221662A (en) * | 1963-02-14 | 1965-12-07 | American Radiator & Standard | Method and apparatus for controlling flow in centrifugal machines |
US3505819A (en) * | 1967-02-27 | 1970-04-14 | Rolls Royce | Gas turbine power plant |
US3627447A (en) * | 1969-03-17 | 1971-12-14 | United Aircraft Canada | Radial turbines |
EP3591235A4 (en) * | 2017-02-28 | 2020-02-26 | Mitsubishi Heavy Industries Compressor Corporation | Impeller and rotary machine |
-
1922
- 1922-02-23 GB GB5412/22A patent/GB180299A/en not_active Expired
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2781963A (en) * | 1950-06-16 | 1957-02-19 | Guy S Faber | Blower |
US3197124A (en) * | 1962-04-03 | 1965-07-27 | Sallou Jean | Centrifugal pump impellers |
US3221662A (en) * | 1963-02-14 | 1965-12-07 | American Radiator & Standard | Method and apparatus for controlling flow in centrifugal machines |
US3505819A (en) * | 1967-02-27 | 1970-04-14 | Rolls Royce | Gas turbine power plant |
US3627447A (en) * | 1969-03-17 | 1971-12-14 | United Aircraft Canada | Radial turbines |
EP3591235A4 (en) * | 2017-02-28 | 2020-02-26 | Mitsubishi Heavy Industries Compressor Corporation | Impeller and rotary machine |
US11053952B2 (en) | 2017-02-28 | 2021-07-06 | Mitsubishi Heavy Industries Compressor Corporation | Impeller and rotary machine |
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