GB758696A - Improvements in or relating to the guide blade structure of axial flow compressors - Google Patents
Improvements in or relating to the guide blade structure of axial flow compressorsInfo
- Publication number
- GB758696A GB758696A GB2423054A GB2423054A GB758696A GB 758696 A GB758696 A GB 758696A GB 2423054 A GB2423054 A GB 2423054A GB 2423054 A GB2423054 A GB 2423054A GB 758696 A GB758696 A GB 758696A
- Authority
- GB
- United Kingdom
- Prior art keywords
- ring
- casing
- guide blade
- tip
- ridges
- 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
- 230000004048 modification Effects 0.000 abstract 2
- 238000012986 modification Methods 0.000 abstract 2
- 210000004907 gland Anatomy 0.000 abstract 1
- 230000000717 retained effect Effects 0.000 abstract 1
- 125000006850 spacer group Chemical group 0.000 abstract 1
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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
- F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
758,696. Axial-flow compressors; blade fixing. SIEMENS-SCHUCKERTWERKE AKT.- GES. Aug. 19, 1954 [Aug. 19, 1953], No. 24230/54. Classes 110(1) and 110(3) In an axial-flow compressor, the guide blade tips are secured to a non-resilient substantially annular support 6, Fig. 1, and the guide blade roots are secured to a substantially annular support 7 which is resilient and is adapted to locate the blade roots by co-operation with the compressor casing. The root of each guide blade 4 is chamfered at 9 and sweated into the ring 7, while the tip is slid into an axial groove in the ring 6 and retained by inserted wires 8. The ring 7 has a thin web 10 which overlaps the following rotor blades, and a thickened portion 11 which is a snug fit in the cylindrical bore of the casing. The thin web 10 allows the part of the ring 7 which carries the blades 4 to expand radially. Adjacent root support rings 12, 7 and 13 abut one another and are located and held against rotation by pins such as 14, 15 which engage the thickened parts such as 11, 16 and are inserted in the joint of the casing and held by screws. Ridges such as 25 co-operate with annular webs 19, 20, 21 to form labyrinth glands. In a modification, Fig. 2, two labyrinth seals in series are formed by thin cylinders 30, 31 screwed to an extension 28 of a guide blade support ring 27 and cooperating with ridges 33 on a ring 35 and similar ridges on a cylinder 34. In a further modification, two rows of whirlremoving stator blades are provided after the last row of rotor blading, their two tip-supporting rings being secured together, with a spacer ring interposed, by screws. The two root-supporting rings are spaced from the inner wall of the casing, and radial location is provided by the engagement of the second tip-supporting ring with an annular surface in the casing.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DES34865A DE1109310B (en) | 1953-08-19 | 1953-08-19 | Axial compressor with guide vane rims arranged between the rotating blade rims |
Publications (1)
Publication Number | Publication Date |
---|---|
GB758696A true GB758696A (en) | 1956-10-10 |
Family
ID=7481677
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2423054A Expired GB758696A (en) | 1953-08-19 | 1954-08-19 | Improvements in or relating to the guide blade structure of axial flow compressors |
Country Status (3)
Country | Link |
---|---|
CH (1) | CH327434A (en) |
DE (1) | DE1109310B (en) |
GB (1) | GB758696A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3062497A (en) * | 1958-11-24 | 1962-11-06 | Ford Motor Co | Gas turbine engine |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE19507673C2 (en) * | 1995-03-06 | 1997-07-03 | Mtu Muenchen Gmbh | Guide wheel for turbomachinery |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE476399C (en) * | 1929-05-15 | Siemens Schuckertwerke Akt Ges | Device to seal the gap for constant pressure steam turbines | |
AT106893B (en) * | 1923-07-13 | 1927-07-25 | Jan Ing Kieswetter | Device for compensating for different thermal expansions between an outer housing wall and an intermediate wall of the same housing, especially in steam or gas turbines. |
DE518107C (en) * | 1925-04-03 | 1931-02-24 | Jan Kieswetter | Device to compensate for different thermal expansions between an outer housing wall and at least one intermediate wall of the same housing, especially in the case of steam or gas turbines |
DE538088C (en) * | 1927-06-22 | 1931-11-10 | Skoda Kp | Steam or gas turbine |
BE462182A (en) * | 1944-12-22 | 1900-01-01 |
-
1953
- 1953-08-19 DE DES34865A patent/DE1109310B/en active Pending
-
1954
- 1954-08-17 CH CH327434D patent/CH327434A/en unknown
- 1954-08-19 GB GB2423054A patent/GB758696A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3062497A (en) * | 1958-11-24 | 1962-11-06 | Ford Motor Co | Gas turbine engine |
Also Published As
Publication number | Publication date |
---|---|
DE1109310B (en) | 1961-06-22 |
CH327434A (en) | 1958-01-31 |
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