GB1155876A - Axial Flow Compressors, Blowers And Pumps - Google Patents
Axial Flow Compressors, Blowers And PumpsInfo
- Publication number
- GB1155876A GB1155876A GB4648466A GB4648466A GB1155876A GB 1155876 A GB1155876 A GB 1155876A GB 4648466 A GB4648466 A GB 4648466A GB 4648466 A GB4648466 A GB 4648466A GB 1155876 A GB1155876 A GB 1155876A
- Authority
- GB
- United Kingdom
- Prior art keywords
- rotor
- hub
- section
- impulse
- rotor hub
- 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
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/321—Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
- F04D29/324—Blades
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
1,155,876. Axial-flow compressors, blowers and pumps. JOY MFG. CO, Oct.18, 1966, No.46484/66. Heading F1C. In an encased axial-flow compressor, blower or pump, having a rotor comprising a hub and a number of blades extending radially outwardly from the hub, each blade has a radially inner portion forming an impulse section and a radially outer portion at least the radially outer expanse of which forms a reaction section. The minimum radial length of the impulse section and, preferably, of the reaction section is 10% of the total blade length or of the rotor hub radius, whichever is the smaller. The radial length of the impulse section is not normally greater than <SP>1</SP>/ 3 of the rotor hub radius. The trailing end of the impulse section extends in the direction of rotation at an angle of at least 15 degrees with a plane through the rotational axis. The rotor hub may diverge in the direction of flow. The rotor blades may be of adjustable pitch and be non- uniformly spaced around the rotor hub. Stator blades may be arranged upstream and/or downstream of the rotor. Contra-rotating rotors may be used.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB4648466A GB1155876A (en) | 1966-10-18 | 1966-10-18 | Axial Flow Compressors, Blowers And Pumps |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB4648466A GB1155876A (en) | 1966-10-18 | 1966-10-18 | Axial Flow Compressors, Blowers And Pumps |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1155876A true GB1155876A (en) | 1969-06-25 |
Family
ID=10441453
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB4648466A Expired GB1155876A (en) | 1966-10-18 | 1966-10-18 | Axial Flow Compressors, Blowers And Pumps |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB1155876A (en) |
-
1966
- 1966-10-18 GB GB4648466A patent/GB1155876A/en not_active Expired
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