GB251659A - Improvements in blades for centrifugal compressors - Google Patents
Improvements in blades for centrifugal compressorsInfo
- Publication number
- GB251659A GB251659A GB11456/26A GB1145626A GB251659A GB 251659 A GB251659 A GB 251659A GB 11456/26 A GB11456/26 A GB 11456/26A GB 1145626 A GB1145626 A GB 1145626A GB 251659 A GB251659 A GB 251659A
- Authority
- GB
- United Kingdom
- Prior art keywords
- blades
- centrifugal compressors
- secured
- blade
- ribs
- 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
- 239000002184 metal Substances 0.000 abstract 2
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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
251,659. Akt.-Ges. Brown, Boveri, et Cie. May 2, 1925, [Convention date]. Impeller blades.-Blades 1 for the rotor wheels of centrifugal compressors have transverse and longitudinal ribs 5, 6 and are secured to the rotor discs by rivets 3. The ribs are provided only on the side of the blade facing the centre of the wheel, and they are covered with a sheet 17 of metal bent round the inner edge of the blade and secured by a rivet 19. The blades are composed of light metal and may be made in sections which can be arranged to form passages of any desired shape.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE251659X | 1925-05-02 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB251659A true GB251659A (en) | 1926-06-10 |
Family
ID=5944042
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB11456/26A Expired GB251659A (en) | 1925-05-02 | 1926-04-30 | Improvements in blades for centrifugal compressors |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB251659A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2254892A (en) * | 1991-04-16 | 1992-10-21 | Gen Electric | Hollow airfoil. |
US5253824A (en) * | 1991-04-16 | 1993-10-19 | General Electric Company | Hollow core airfoil |
-
1926
- 1926-04-30 GB GB11456/26A patent/GB251659A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2254892A (en) * | 1991-04-16 | 1992-10-21 | Gen Electric | Hollow airfoil. |
US5253824A (en) * | 1991-04-16 | 1993-10-19 | General Electric Company | Hollow core airfoil |
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