GB640669A - Improvements in and relating to high speed rotors for centrifugal compressors and the like - Google Patents
Improvements in and relating to high speed rotors for centrifugal compressors and the likeInfo
- Publication number
- GB640669A GB640669A GB30709/47A GB3070947A GB640669A GB 640669 A GB640669 A GB 640669A GB 30709/47 A GB30709/47 A GB 30709/47A GB 3070947 A GB3070947 A GB 3070947A GB 640669 A GB640669 A GB 640669A
- Authority
- GB
- United Kingdom
- Prior art keywords
- centrifugal compressors
- relating
- high speed
- impeller
- reinforced
- 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
- F04D29/18—Rotors
- F04D29/22—Rotors specially for centrifugal pumps
- F04D29/2205—Conventional flow pattern
- F04D29/2222—Construction and assembly
-
- 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
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/04—Blade-carrying members, e.g. rotors for radial-flow machines or engines
- F01D5/043—Blade-carrying members, e.g. rotors for radial-flow machines or engines of the axial inlet- radial outlet, or vice versa, type
- F01D5/048—Form or construction
-
- 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
- F04D29/284—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for compressors
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
640,669. Centrifugal compressors. BRITISH THOMSON-HOUSTON CO., Ltd. Nov. 19, 1947, No. 30709. Convention date, March 8, 1943. [Class 110(i)] An impeller is reinforced by a ring 10 which is S-shaped in cross-section having axially extending ends 8, 9 which engage the shroud 4 at radially spaced surfaces 11, 12. These surfaces are tapered inwardly. The crosssection of the ring is such that there is no tendency to twist under the action of centrifugal force. The hub 1 is reinforced by rings 13, 14. The rings 10, 13, 14 are of high strength steel and are shrunk on to the impeller, which may be of aluminium alloy.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US640669XA | 1943-03-08 | 1943-03-08 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB640669A true GB640669A (en) | 1950-07-26 |
Family
ID=22053354
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB30709/47A Expired GB640669A (en) | 1943-03-08 | 1947-11-19 | Improvements in and relating to high speed rotors for centrifugal compressors and the like |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB640669A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2479349A1 (en) * | 1980-03-26 | 1981-10-02 | Klein Schanzlin & Becker Ag | WHEEL FOR CIRCULATING CENTRIFUGAL PUMPS OF THE PRIMARY CIRCUIT OF NUCLEAR POWER PLANTS |
GB2282189A (en) * | 1993-05-25 | 1995-03-29 | Swea Tong Chiang | Fan rotor assembly |
EP4148281A1 (en) * | 2021-09-10 | 2023-03-15 | Hamilton Sundstrand Corporation | Stress relieving compressor shroud compression rings |
EP4148282A1 (en) * | 2021-09-10 | 2023-03-15 | Hamilton Sundstrand Corporation | Dynamic sealing labyrinth seals |
-
1947
- 1947-11-19 GB GB30709/47A patent/GB640669A/en not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2479349A1 (en) * | 1980-03-26 | 1981-10-02 | Klein Schanzlin & Becker Ag | WHEEL FOR CIRCULATING CENTRIFUGAL PUMPS OF THE PRIMARY CIRCUIT OF NUCLEAR POWER PLANTS |
GB2282189A (en) * | 1993-05-25 | 1995-03-29 | Swea Tong Chiang | Fan rotor assembly |
GB2282189B (en) * | 1993-05-25 | 1997-06-04 | Swea Tong Chiang | Fan blade assembly |
EP4148281A1 (en) * | 2021-09-10 | 2023-03-15 | Hamilton Sundstrand Corporation | Stress relieving compressor shroud compression rings |
EP4148282A1 (en) * | 2021-09-10 | 2023-03-15 | Hamilton Sundstrand Corporation | Dynamic sealing labyrinth seals |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB1395930A (en) | Diffuser | |
GB1523668A (en) | Turbomachinery stator assembly | |
GB621545A (en) | Improvements relating to axial compressors and turbines | |
GB1490806A (en) | Impeller for a high-speed turbo machine | |
GB1533805A (en) | Turbine wheel with structural discontinuity | |
GB954369A (en) | Drum-type fan rotor with forwardly curved blades | |
GB640669A (en) | Improvements in and relating to high speed rotors for centrifugal compressors and the like | |
GB1084968A (en) | Turbine wheel | |
US2394124A (en) | Bladed body | |
GB1161298A (en) | Turbomachine Rotors | |
GB941328A (en) | Turbo-converters | |
GB623149A (en) | Improvements in and relating to fan-wheels | |
GB1012978A (en) | Improvements in and relating to hydrodynamic torque converters | |
GB987016A (en) | Improvements in turbine rotors | |
GB586838A (en) | Elastic fluid turbines | |
GB473714A (en) | Improvements in or relating to turbines | |
GB579425A (en) | Improvements in blade drums for axial-flow compressors and turbines | |
GB972999A (en) | Hydraulic coupling | |
GB624777A (en) | Improvements in or relating to stator casings for compressors and like machines | |
GB572202A (en) | Improvements in or relating to vehicle brakes | |
GB871098A (en) | Improvements in axial-flow bladed rotor wheels | |
GB647143A (en) | Improvements in or relating to turbine blades | |
GB590433A (en) | Improvements in and relating to the manufacture of turbine rotors | |
GB913812A (en) | Self-centralising mounting for rotor wheels on rotating shafts | |
GB568770A (en) | Improvements in or relating to the fixing of the blades in turbines and compressors |