GB718139A - Improvements in or relating to bladed rotors for fluid-flow machines - Google Patents
Improvements in or relating to bladed rotors for fluid-flow machinesInfo
- Publication number
- GB718139A GB718139A GB846952A GB846952A GB718139A GB 718139 A GB718139 A GB 718139A GB 846952 A GB846952 A GB 846952A GB 846952 A GB846952 A GB 846952A GB 718139 A GB718139 A GB 718139A
- Authority
- GB
- United Kingdom
- Prior art keywords
- rotor
- discs
- blades
- secured
- sheet metal
- 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
- 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
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
- F01D5/3076—Sheet metal discs
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
718,139. Turbine and compressor rotors. POWER JETS (RESEARCH & DEVELOPMENT), Ltd. March 25, 1953 [April 2, 1952], No. 8469/52. Class 110(3) A bladed rotor for axial-flow compressors or turbines comprises at least one sheet metal rotor disc, and a row of blades formed of lengths of bar material of appropriate aerofoil cross-section mounted at the periphery thereof each blade being secured at its root end to a bracket which is itself secured to the rotor disc. Each rotor element in the embodiment shown comprises two discs la, 1b formed with radial slots at the periphery. The blades 3 have two channel-section brackets 4a, 4b secured by rivets or by welding or brazing at the root end, and the sides 4b of the brackets are secured by rivets to the rotor discs, the root portions of the blades entering the radial slots in the rotor discs. The surface of the rotor between adjacent blades in a row is completed by platforms 5 having lugs 5a riveted to the rotor discs. The surface of the rotor between blade rows is formed by sheet metal spacer rings 6. The rotor discs are mounted on tubes 9 carrying tubular distance pieces 10 between the rotor discs. The blade platforms and spacer rings could be omitted and the rotor surface formed by a single sheet metal cylinder enveloping the rotor discs and formed with holes through which the blades project.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB846952A GB718139A (en) | 1952-04-02 | 1952-04-02 | Improvements in or relating to bladed rotors for fluid-flow machines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB846952A GB718139A (en) | 1952-04-02 | 1952-04-02 | Improvements in or relating to bladed rotors for fluid-flow machines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB718139A true GB718139A (en) | 1954-11-10 |
Family
ID=9853056
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB846952A Expired GB718139A (en) | 1952-04-02 | 1952-04-02 | Improvements in or relating to bladed rotors for fluid-flow machines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB718139A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2976011A (en) * | 1955-02-10 | 1961-03-21 | Stalker Corp | Fabricated bladed compressor wheels |
US3056581A (en) * | 1959-10-14 | 1962-10-02 | Gen Motors Corp | Blade attachment |
US3081021A (en) * | 1959-10-14 | 1963-03-12 | Gen Motors Corp | Fabricated wheel and blade attachments |
-
1952
- 1952-04-02 GB GB846952A patent/GB718139A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2976011A (en) * | 1955-02-10 | 1961-03-21 | Stalker Corp | Fabricated bladed compressor wheels |
US3056581A (en) * | 1959-10-14 | 1962-10-02 | Gen Motors Corp | Blade attachment |
US3081021A (en) * | 1959-10-14 | 1963-03-12 | Gen Motors Corp | Fabricated wheel and blade attachments |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US2873944A (en) | Turbine blade cooling | |
GB1284538A (en) | Blade for a fluid flow machine | |
GB1272200A (en) | Axial-flow turbomachine rotors | |
GB715145A (en) | Improvements in or relating to stator constructions for compressors | |
GB751011A (en) | Improvements in or relating to the cooling of turbine blades | |
GB1491556A (en) | Rotor blades for turbomachines | |
GB695221A (en) | Construction of compressor rotors | |
GB1395957A (en) | Fluid flow machines and rotors therefor | |
GB724281A (en) | Improvements in or relating to bladed rotors for axial flow fluid flow machines | |
GB1053420A (en) | ||
GB667194A (en) | Improvements in and relating to turbine rotors | |
GB723405A (en) | Improvements in or relating to blade-carrying turbine rotors and the like | |
GB696815A (en) | Improvements relating to bladed rotors for rotary power conversion machines | |
GB723394A (en) | Improvements in turbine blades | |
GB718139A (en) | Improvements in or relating to bladed rotors for fluid-flow machines | |
GB1148339A (en) | Compressors or turbines for gas turbine engines | |
US3471127A (en) | Turbomachine rotor | |
GB800098A (en) | Improvements in or relating to multi-stage axial-flow compressors | |
GB742476A (en) | Improvements in or relating to bladed stator and rotor constructions for fluid machines such as axial-flow turbines or compressors | |
GB719236A (en) | Improvements in and relating to multi-stage axial flow compressors | |
GB718138A (en) | Improvements in or relating to bladed rotors for axial-flow fluid-flow machines | |
GB848465A (en) | Rotors of multi-stage axial flow compressors or turbines | |
GB811922A (en) | Improvements relating to bladed rotors of axial flow fluid machines | |
US2925248A (en) | Bladed wheels for axial flow machines | |
GB732920A (en) | Improvements relating to blade assemblies of turbo-machines such as compressors and turbines |