GB200474A - Improved means of fastening the blades in gas turbines and steam turbines - Google Patents
Improved means of fastening the blades in gas turbines and steam turbinesInfo
- Publication number
- GB200474A GB200474A GB33467/22A GB3346722A GB200474A GB 200474 A GB200474 A GB 200474A GB 33467/22 A GB33467/22 A GB 33467/22A GB 3346722 A GB3346722 A GB 3346722A GB 200474 A GB200474 A GB 200474A
- Authority
- GB
- United Kingdom
- Prior art keywords
- blades
- turbines
- fastening
- improved means
- spacing members
- 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
- F01D5/3023—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses
- F01D5/3046—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses the rotor having ribs around the circumference
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
200,474. Akt.-Ges. Brown, Boveri, et Cie. July 6, 1922, [Convention date]. Blades are fixed by spacing members which clasp the sides of discs as shown at a. The blades are formed with a T-shaped foot which is clamped between two adjacent spacing members, and bears directly on the periphery of the disc. The spacing members may be wider than the blades and the parts a may be formed with suitable projections engaging grooves in the disc as at b.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH200474X | 1922-07-06 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB200474A true GB200474A (en) | 1924-01-17 |
Family
ID=4442330
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB33467/22A Expired GB200474A (en) | 1922-07-06 | 1922-12-07 | Improved means of fastening the blades in gas turbines and steam turbines |
Country Status (5)
Country | Link |
---|---|
CH (1) | CH101877A (en) |
DE (1) | DE383251C (en) |
FR (1) | FR557923A (en) |
GB (1) | GB200474A (en) |
NL (1) | NL11668C (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1016982B (en) * | 1953-07-06 | 1957-10-03 | Power Jets Res & Dev Ltd | Runner with cooling device for flow machines operated with gaseous equipment, in particular gas turbines |
-
0
- NL NL11668D patent/NL11668C/xx active
-
1922
- 1922-07-06 CH CH101877D patent/CH101877A/en unknown
- 1922-07-25 DE DEA38167D patent/DE383251C/en not_active Expired
- 1922-10-28 FR FR557923D patent/FR557923A/en not_active Expired
- 1922-12-07 GB GB33467/22A patent/GB200474A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1016982B (en) * | 1953-07-06 | 1957-10-03 | Power Jets Res & Dev Ltd | Runner with cooling device for flow machines operated with gaseous equipment, in particular gas turbines |
Also Published As
Publication number | Publication date |
---|---|
CH101877A (en) | 1923-10-16 |
FR557923A (en) | 1923-08-18 |
NL11668C (en) | |
DE383251C (en) | 1923-10-11 |
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