GB373940A - Improvements in and relating to turbines - Google Patents
Improvements in and relating to turbinesInfo
- Publication number
- GB373940A GB373940A GB33099/31A GB3309931A GB373940A GB 373940 A GB373940 A GB 373940A GB 33099/31 A GB33099/31 A GB 33099/31A GB 3309931 A GB3309931 A GB 3309931A GB 373940 A GB373940 A GB 373940A
- Authority
- GB
- United Kingdom
- Prior art keywords
- hole
- inspected
- cover
- turbines
- relating
- 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
- F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
- F01D21/003—Arrangements for testing or measuring
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
Abstract
373,940. Gas turbines. AKT.-GES BROWN, BOVERI, ET CIE, Baden, Switzerland. Nov. 30, 1931, No. 33099. Convention date, May 4. [Class 110 (iii).] In an exhaust gas turbine means are provided to enable the blades to be inspected and the clearances to be measured without dismantling. In the windage protection extension of the nozzle ring 2 surrounding the rotor 1, one or more holes 3 are cut. When a cover 7 is removed the wheel may be inspected through the hole. The cover 7 may carry a plug 9 adapted to close the hole to prevent whistling. An inspection hole 11 may also be provided on the inlet side.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE373940X | 1931-05-04 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB373940A true GB373940A (en) | 1932-06-02 |
Family
ID=6340919
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB33099/31A Expired GB373940A (en) | 1931-05-04 | 1931-11-30 | Improvements in and relating to turbines |
Country Status (2)
Country | Link |
---|---|
FR (1) | FR730375A (en) |
GB (1) | GB373940A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2823890A (en) * | 1952-09-27 | 1958-02-18 | Tech Studien Ag | Housing for gas or steam turbines |
US3186684A (en) * | 1962-04-06 | 1965-06-01 | Hitachi Ltd | Device for measurement of the bottom runner clearance in a reaction type hydraulic turbine |
US3276742A (en) * | 1963-11-05 | 1966-10-04 | Hitachi Ltd | Vertical shaft kaplan water turbines |
US3936217A (en) * | 1975-01-31 | 1976-02-03 | Westinghouse Electric Corporation | Inspection port for turbines |
US8511970B2 (en) | 2009-09-30 | 2013-08-20 | Rolls-Royce Corporation | Plug assembly |
-
1931
- 1931-11-30 GB GB33099/31A patent/GB373940A/en not_active Expired
-
1932
- 1932-01-23 FR FR730375D patent/FR730375A/en not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2823890A (en) * | 1952-09-27 | 1958-02-18 | Tech Studien Ag | Housing for gas or steam turbines |
US3186684A (en) * | 1962-04-06 | 1965-06-01 | Hitachi Ltd | Device for measurement of the bottom runner clearance in a reaction type hydraulic turbine |
US3276742A (en) * | 1963-11-05 | 1966-10-04 | Hitachi Ltd | Vertical shaft kaplan water turbines |
US3936217A (en) * | 1975-01-31 | 1976-02-03 | Westinghouse Electric Corporation | Inspection port for turbines |
US8511970B2 (en) | 2009-09-30 | 2013-08-20 | Rolls-Royce Corporation | Plug assembly |
Also Published As
Publication number | Publication date |
---|---|
FR730375A (en) | 1932-08-11 |
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