GB358406A - Improvements in and relating to elastic fluid turbines - Google Patents
Improvements in and relating to elastic fluid turbinesInfo
- Publication number
- GB358406A GB358406A GB6091/31A GB609131A GB358406A GB 358406 A GB358406 A GB 358406A GB 6091/31 A GB6091/31 A GB 6091/31A GB 609131 A GB609131 A GB 609131A GB 358406 A GB358406 A GB 358406A
- Authority
- GB
- United Kingdom
- Prior art keywords
- relating
- feb
- projections
- blades
- elastic fluid
- 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
- F01D5/12—Blades
- F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
Abstract
358,406. Steam turbines. BRITISH THOMSON-HOUSTON GO., Ltd., Crown House, Aldwych, London.- (Assignees of Delles, W. J. ; 132, Rosa Road, Schenectady, New York, U.S.A.) Feb. 26, 1931, No. 6091.. Convention date, Feb. 28, 1930. [Class 110 (iii).] The blades 2 of a turbine rotor are tied intermediately by a wire 5 having projections 6 engaging notches in the edges of the blades. The parts are secured by fused metal 7. In a modification, Fig. 3, the projections 6 are replaced by pins 10 which are fitted in holes in a tie wire of uniform section.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US358406XA | 1930-02-28 | 1930-02-28 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB358406A true GB358406A (en) | 1931-10-08 |
Family
ID=21885095
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB6091/31A Expired GB358406A (en) | 1930-02-28 | 1931-02-26 | Improvements in and relating to elastic fluid turbines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB358406A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE863345C (en) * | 1940-03-21 | 1953-01-15 | Karl Dr-Ing Roeder | Stiffening of blades with free ends |
US3327995A (en) * | 1965-07-31 | 1967-06-27 | Rolls Royce | Bladed rotor |
GB2222636A (en) * | 1988-08-15 | 1990-03-14 | Gen Electric | Shroud for the low pressure stage of a compressor |
BE1030042B1 (en) * | 2021-12-17 | 2023-07-17 | Safran Aero Boosters | MOBILE WHEEL WITH INTERMEDIATE RING |
BE1030508B1 (en) * | 2022-04-21 | 2023-12-04 | Safran Aero Boosters | INTERMEDIATE RING ROTOR |
-
1931
- 1931-02-26 GB GB6091/31A patent/GB358406A/en not_active Expired
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE863345C (en) * | 1940-03-21 | 1953-01-15 | Karl Dr-Ing Roeder | Stiffening of blades with free ends |
US3327995A (en) * | 1965-07-31 | 1967-06-27 | Rolls Royce | Bladed rotor |
GB2222636A (en) * | 1988-08-15 | 1990-03-14 | Gen Electric | Shroud for the low pressure stage of a compressor |
GB2222636B (en) * | 1988-08-15 | 1993-04-21 | Gen Electric | Shroud for the low pressure stage of a compressor |
BE1030042B1 (en) * | 2021-12-17 | 2023-07-17 | Safran Aero Boosters | MOBILE WHEEL WITH INTERMEDIATE RING |
BE1030508B1 (en) * | 2022-04-21 | 2023-12-04 | Safran Aero Boosters | INTERMEDIATE RING ROTOR |
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