GB108582A - Improvements in and relating to Centrifugal Compressors. - Google Patents
Improvements in and relating to Centrifugal Compressors.Info
- Publication number
- GB108582A GB108582A GB1433516A GB1433516A GB108582A GB 108582 A GB108582 A GB 108582A GB 1433516 A GB1433516 A GB 1433516A GB 1433516 A GB1433516 A GB 1433516A GB 108582 A GB108582 A GB 108582A
- Authority
- GB
- United Kingdom
- Prior art keywords
- sections
- impeller
- casing
- chambers
- stage
- 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
- F04D17/00—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
- F04D17/08—Centrifugal pumps
- F04D17/10—Centrifugal pumps for compressing or evacuating
- F04D17/12—Multi-stage pumps
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
108,582. British Thomson - Houston Co., (General Electric Co.). Oct. 9, 1916. Disk-supported-blade fans; multi-stage centrifugal fans; casings.-The casing of a single-stage fan is composed of an inlet section 14 and a discharge section 15 and for a multi-stage fan intermediate casing-sections are interposed. The casing-sections are castings and are provided with walls 18, 59, 31, 66, which form chambers in which the impellers 12 rotate; at each side of the impeller chambers annular chambers are formed from which the fluid is fed to the whole periphery of the intake of the impeller and surrounding the impeller are two annular chambers, the outer of which 40, 58<a> is connected by radial passages to the suction chamber 45, 63, the inner chambers 46, 64 connecting the discharge of one impeller to the suction chamber of the next or to the discharge outlet 47. Diffuser blades 72 are fixed in grooves in meeting flanges of the adjacent sections. Intermediate sections have a wall 56 which divides one stage from the next. Casing sections of a standard pattern may be adapted for impellers of differing axial width by making the meeting flanges longer or shorter. Openings 71 are provided for removal of matter deposited in the various conduits.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1433516A GB108582A (en) | 1916-10-09 | 1916-10-09 | Improvements in and relating to Centrifugal Compressors. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1433516A GB108582A (en) | 1916-10-09 | 1916-10-09 | Improvements in and relating to Centrifugal Compressors. |
Publications (1)
Publication Number | Publication Date |
---|---|
GB108582A true GB108582A (en) | 1917-08-16 |
Family
ID=32483665
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1433516A Expired GB108582A (en) | 1916-10-09 | 1916-10-09 | Improvements in and relating to Centrifugal Compressors. |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB108582A (en) |
-
1916
- 1916-10-09 GB GB1433516A patent/GB108582A/en not_active Expired
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