GB672457A - Improvements in or relating to the seating of ceramic rotor blades in steel rotor bodies - Google Patents
Improvements in or relating to the seating of ceramic rotor blades in steel rotor bodiesInfo
- Publication number
- GB672457A GB672457A GB12925/50A GB1292550A GB672457A GB 672457 A GB672457 A GB 672457A GB 12925/50 A GB12925/50 A GB 12925/50A GB 1292550 A GB1292550 A GB 1292550A GB 672457 A GB672457 A GB 672457A
- Authority
- GB
- United Kingdom
- Prior art keywords
- ceramic
- seating
- relating
- steel
- bodies
- 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
- F01D5/3084—Fixing blades to rotors; Blade roots ; Blade spacers the blades being made of ceramics
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Ceramic Engineering (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
672,457. Turbine blades. MASCHINENFABRIK AUGSBURGNURNBERG AKT.- GES. May 23, 1950 [Oct. 5, 1949], No. 12925/50. Drawings to Specification. Class 110(iii) A ceramic turbine blade is mounted in a steel rotor by means of dovetail roots, the inclination of the sides of the dovetail to the direction of the tensile stress on the blade being an angle, the tangent of which is equal to two to three times the ratio of the permissible tensile strength to the compressive strength of the ceramic material.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE672457X | 1949-10-05 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB672457A true GB672457A (en) | 1952-05-21 |
Family
ID=6590735
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB12925/50A Expired GB672457A (en) | 1949-10-05 | 1950-05-23 | Improvements in or relating to the seating of ceramic rotor blades in steel rotor bodies |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB672457A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2828940A (en) * | 1953-12-30 | 1958-04-01 | United Aircraft Corp | Cooled turbine blade |
-
1950
- 1950-05-23 GB GB12925/50A patent/GB672457A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2828940A (en) * | 1953-12-30 | 1958-04-01 | United Aircraft Corp | Cooled turbine blade |
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