GB812273A - Improvements in and relating to turbines, compressors, blowers and fans - Google Patents
Improvements in and relating to turbines, compressors, blowers and fansInfo
- Publication number
- GB812273A GB812273A GB13555/55A GB1355555A GB812273A GB 812273 A GB812273 A GB 812273A GB 13555/55 A GB13555/55 A GB 13555/55A GB 1355555 A GB1355555 A GB 1355555A GB 812273 A GB812273 A GB 812273A
- Authority
- GB
- United Kingdom
- Prior art keywords
- blowers
- compressors
- turbines
- fans
- relating
- 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
- F04D21/00—Pump involving supersonic speed of pumped fluids
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/141—Shape, i.e. outer, aerodynamic form
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/141—Shape, i.e. outer, aerodynamic form
- F01D5/145—Means for influencing boundary layers or secondary circulations
-
- 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
-
- 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
- F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
- F04D29/68—Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers
- F04D29/681—Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers especially adapted for elastic fluid pumps
- F04D29/682—Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers especially adapted for elastic fluid pumps by fluid extraction
Abstract
812,273. Boundary layer control. HAUSAMMANN, W. May 10, 1955 [May 10, 1954], No. 13555/55. Class 4. [Also in Group XXVI] A turbine or compressor comprising at least one duct formed between the hub surface and partition walls 152 of the rotor and an outer surface, and a sill 155 on the hub or outer surface which faces upstream in the case of a compressor and downstream in the case of a turbine and is arranged at an angle to the plane of the rotor, has the boundary layer removed from the sill by a suction pump 171 through the slot 156 and ducts 159, 161.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH812273X | 1954-05-10 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB812273A true GB812273A (en) | 1959-04-22 |
Family
ID=4538608
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB13555/55A Expired GB812273A (en) | 1954-05-10 | 1955-05-10 | Improvements in and relating to turbines, compressors, blowers and fans |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB812273A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP3418494A1 (en) * | 2017-06-23 | 2018-12-26 | Rolls-Royce plc | Secondary flow control |
-
1955
- 1955-05-10 GB GB13555/55A patent/GB812273A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP3418494A1 (en) * | 2017-06-23 | 2018-12-26 | Rolls-Royce plc | Secondary flow control |
US10760427B2 (en) | 2017-06-23 | 2020-09-01 | Rolls-Royce Plc | Secondary flow control |
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