GB191515833A - Improvements in or relating to Turbine Pumps or Multi-stage Centrifugal Fans. - Google Patents
Improvements in or relating to Turbine Pumps or Multi-stage Centrifugal Fans.Info
- Publication number
- GB191515833A GB191515833A GB191515833DA GB191515833A GB 191515833 A GB191515833 A GB 191515833A GB 191515833D A GB191515833D A GB 191515833DA GB 191515833 A GB191515833 A GB 191515833A
- Authority
- GB
- United Kingdom
- Prior art keywords
- relating
- sections
- stage centrifugal
- centrifugal fans
- fan
- 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
- F04D17/122—Multi-stage pumps the individual rotor discs being, one for each stage, on a common shaft and axially spaced, e.g. conventional centrifugal multi- stage compressors
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
15,833. Viola, E. O. F. May 9, 1916. Multi - stage fans; casings.-The casing of a multi-stage fan, which is balanced for end thrust by the provision of a number of rotors causing air to pass in reverse directions axially, is built up of a number of sections, each alternate section having a conical flange A', guide vanes A<2> and a plane disk A<3> with a boss surrounding the shaft. The other sections have a reverse conical flange A<4>. Adjacent flanges A<4> and disks A<3> form a rotor chamber, The figure shows a fan having a central inlet I in which is placed a deflector L. In a modified form the inlets may be at each end and the central outlet may be provided with a double impeller.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB191515833T | 1916-05-09 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB191515833A true GB191515833A (en) | 1917-05-09 |
Family
ID=34361866
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB191515833D Expired GB191515833A (en) | 1916-05-09 | 1916-05-09 | Improvements in or relating to Turbine Pumps or Multi-stage Centrifugal Fans. |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB191515833A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109340143A (en) * | 2018-10-30 | 2019-02-15 | 江苏贝莱德风机制造有限公司 | A kind of level Four high pressure blower |
CN109372763A (en) * | 2018-10-30 | 2019-02-22 | 江苏贝莱德风机制造有限公司 | A kind of stable type level Four high pressure blower |
-
1916
- 1916-05-09 GB GB191515833D patent/GB191515833A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109340143A (en) * | 2018-10-30 | 2019-02-15 | 江苏贝莱德风机制造有限公司 | A kind of level Four high pressure blower |
CN109372763A (en) * | 2018-10-30 | 2019-02-22 | 江苏贝莱德风机制造有限公司 | A kind of stable type level Four high pressure blower |
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