GB229627A - Improvements relating to turbine casings having transverse partitions and the like therein - Google Patents
Improvements relating to turbine casings having transverse partitions and the like thereinInfo
- Publication number
- GB229627A GB229627A GB24300/24A GB2430024A GB229627A GB 229627 A GB229627 A GB 229627A GB 24300/24 A GB24300/24 A GB 24300/24A GB 2430024 A GB2430024 A GB 2430024A GB 229627 A GB229627 A GB 229627A
- Authority
- GB
- United Kingdom
- Prior art keywords
- diaphragm
- casing
- bearing surfaces
- ring
- offset bearing
- 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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
- F01D25/246—Fastening of diaphragms or stator-rings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2230/00—Manufacture
- F05D2230/60—Assembly methods
- F05D2230/64—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins
- F05D2230/642—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins using maintaining alignment while permitting differential dilatation
Abstract
229,627. Kieswetter, J. Feb. 19, 1924, [Convention date]. Addition to 219,023. Casings.-In means for connecting a partition 'or diaphragm to a turbine casing so as to permit differential heat expansion of the parts, as described in the parent Specification, a flexible ring 30, arranged between the diaphragm 2 and the casing 1, has circumferentially offset bearing surfaces 31, 32 on its outer and inner walls. Alternatively, these projections 31, 32 may be formed on the casing and the diaphragm; or pins may be inserted in recesses in these parts. Specification 216,737 is referred to. The Specification as open to inspection under Sect. 91 (3) (a) comprises also a modification, Figs. 5, 8 and 9 (Cancelled), wherein the ring 50 has, in addition to offset bearing surfaces 51, 52 which permit radial yielding, offset bearing surfaces 53, 54 at the sides which permit axial yielding of the ring. These surfaces 51 - - 54 may alternatively be formed on the casing and the diaphragm. This subject-matter does not appear in the Specification as accepted.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CS229627X | 1924-02-19 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB229627A true GB229627A (en) | 1926-01-14 |
Family
ID=5451222
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB24300/24A Expired GB229627A (en) | 1924-02-19 | 1924-10-14 | Improvements relating to turbine casings having transverse partitions and the like therein |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB229627A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2470126A (en) * | 1942-12-05 | 1949-05-17 | Allis Chalmers Mfg Co | Turbine construction |
DE2532538A1 (en) * | 1975-07-04 | 1977-01-27 | Bbc Brown Boveri & Cie | COMBINED SEAL AND GUIDE ARRANGEMENT |
EP0486082A1 (en) * | 1990-11-16 | 1992-05-20 | General Motors Corporation | Bearing support for a gas turbine |
EP1041250A3 (en) * | 1999-04-01 | 2002-07-31 | Alstom | Heat shield for a gas turbine |
US20130330187A1 (en) * | 2012-06-11 | 2013-12-12 | General Electric Company | Method and apparatus for mitigating out of roundness effects at a turbine |
-
1924
- 1924-10-14 GB GB24300/24A patent/GB229627A/en not_active Expired
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2470126A (en) * | 1942-12-05 | 1949-05-17 | Allis Chalmers Mfg Co | Turbine construction |
DE2532538A1 (en) * | 1975-07-04 | 1977-01-27 | Bbc Brown Boveri & Cie | COMBINED SEAL AND GUIDE ARRANGEMENT |
US4078812A (en) * | 1975-07-04 | 1978-03-14 | Bbc Brown Boveri & Company Limited | Combined seal and guide arrangement for two coaxially arranged machine parts |
EP0486082A1 (en) * | 1990-11-16 | 1992-05-20 | General Motors Corporation | Bearing support for a gas turbine |
EP1041250A3 (en) * | 1999-04-01 | 2002-07-31 | Alstom | Heat shield for a gas turbine |
US20130330187A1 (en) * | 2012-06-11 | 2013-12-12 | General Electric Company | Method and apparatus for mitigating out of roundness effects at a turbine |
EP2674580A1 (en) * | 2012-06-11 | 2013-12-18 | General Electric Company | Method and apparatus for mitigating out of roundness effects at a turbine |
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