GB604730A - Improvements in or relating to rotors for turbo-machines - Google Patents
Improvements in or relating to rotors for turbo-machinesInfo
- Publication number
- GB604730A GB604730A GB32615/45A GB3261545A GB604730A GB 604730 A GB604730 A GB 604730A GB 32615/45 A GB32615/45 A GB 32615/45A GB 3261545 A GB3261545 A GB 3261545A GB 604730 A GB604730 A GB 604730A
- Authority
- GB
- United Kingdom
- Prior art keywords
- bolt
- shaft
- rotors
- stressed
- boss
- 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
- JHIVVAPYMSGYDF-UHFFFAOYSA-N cyclohexanone Chemical compound O=C1CCCCC1 JHIVVAPYMSGYDF-UHFFFAOYSA-N 0.000 abstract 1
- 210000003739 neck Anatomy 0.000 abstract 1
- 239000011295 pitch Substances 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/04—Blade-carrying members, e.g. rotors for radial-flow machines or engines
- F01D5/043—Blade-carrying members, e.g. rotors for radial-flow machines or engines of the axial inlet- radial outlet, or vice versa, type
-
- 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
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/025—Fixing blade carrying members on shafts
-
- 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
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/04—Blade-carrying members, e.g. rotors for radial-flow machines or engines
- F01D5/043—Blade-carrying members, e.g. rotors for radial-flow machines or engines of the axial inlet- radial outlet, or vice versa, type
- F01D5/045—Blade-carrying members, e.g. rotors for radial-flow machines or engines of the axial inlet- radial outlet, or vice versa, type the wheel comprising two adjacent bladed wheel portions, e.g. with interengaging blades for damping vibrations
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/266—Rotors specially for elastic fluids mounting compressor rotors on shafts
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
604,730. Turbine and like rotors. SULZER FRERES SOC. ANON. Dec. 3, 1945, No. 32615. Convention date, March 3. [Classes 110 (i) and 110 (iii)] A turbine rotor disc 1, Fig. 1, is formed with a boss 2 and the hollow shaft 5, which is centred by a shoulder 6, is secured to it by a bolt 4. The bolt is pre-stressed up to half its yield point stress by means of the nut 8. The hub has a substantial cavity 3 to give the disc radial flexibility. The left side of a helicocentrifugal compressor rotor 34, Fig. 2, is provided with a shaft 21 in a similar way except that the bolt 17 has screw threads 16, 18 of different pitches and the bolt is pre-stressed by turning the bolt in the screwed necks of the shaft and the boss. The right side has a shaft 29 secured by a differentially threaded bolt 27 but there is an intermediate bladed body 24.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH248083 | 1945-03-03 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB604730A true GB604730A (en) | 1948-07-08 |
Family
ID=4522967
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB32615/45A Expired GB604730A (en) | 1945-03-03 | 1945-12-03 | Improvements in or relating to rotors for turbo-machines |
Country Status (5)
Country | Link |
---|---|
CH (1) | CH248083A (en) |
DE (1) | DE968872C (en) |
FR (1) | FR922972A (en) |
GB (1) | GB604730A (en) |
NL (1) | NL65021C (en) |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3677663A (en) * | 1970-10-01 | 1972-07-18 | Avco Corp | Damped turbomachine rotor assembly |
WO1981003047A1 (en) * | 1980-04-17 | 1981-10-29 | Carborundum Co | Ceramic radial turbine wheel |
FR2484035A1 (en) * | 1980-06-06 | 1981-12-11 | Klein Schanzlin & Becker Ag | MEANS FOR COUPLING TREES |
US5087176A (en) * | 1984-12-20 | 1992-02-11 | Allied-Signal Inc. | Method and apparatus to provide thermal isolation of process gas bearings |
WO2001025641A1 (en) * | 1999-10-06 | 2001-04-12 | Ingersoll-Rand Co. | Device and method for detachably connecting an impeller to a pinion shaft in a high speed fluid compressor |
US6499958B2 (en) | 1999-07-02 | 2002-12-31 | Ingersoll-Rand Company | Device and method for detachably connecting an impeller to a pinion shaft in a high speed fluid compressor |
WO2015009351A3 (en) * | 2013-07-19 | 2015-04-09 | Praxair Technology, Inc. | Coupling for directly driven compressor |
US10018205B2 (en) | 2012-11-28 | 2018-07-10 | Napier Turbochargers Limited | Impeller shaft |
CN109296560A (en) * | 2018-11-30 | 2019-02-01 | 无锡市海星船舶动力有限公司 | The ship compressor rotor shaft of resilient dust boot is installed |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1199545B (en) * | 1959-06-27 | 1965-08-26 | Kuehnle Ag | Hub attachment |
DE1162635B (en) * | 1960-11-09 | 1964-02-06 | Daimler Benz Ag | Gas turbine engine with runner in three bearings |
NO121183B (en) * | 1968-11-25 | 1971-01-25 | Kongsberg Vapenfab As | |
NO120916B (en) * | 1968-11-25 | 1970-12-21 | Kongsberg Vapenfab As | |
US4176519A (en) * | 1973-05-22 | 1979-12-04 | United Turbine Ab & Co., Kommanditbolag | Gas turbine having a ceramic rotor |
DE2845199C2 (en) * | 1978-10-17 | 1982-06-16 | Giovanni F. Moncalieri Torino Savonuzzi | Blade wheel for a gas turbine |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE567576C (en) * | 1931-11-25 | 1933-01-05 | Bbc Brown Boveri & Cie | Gas turbine shaft with internal cooling |
CH196040A (en) * | 1936-11-24 | 1938-02-28 | Alfred Buechi | Gas turbine driven blower. |
NL5016C (en) * | 1937-07-07 | |||
DE707342C (en) * | 1938-06-09 | 1941-06-19 | Rheinmetall Borsig Akt Ges | Turbine runner, especially for gas turbines, which is cooled by the continuous evaporation of a liquid ring |
DE749753C (en) * | 1939-10-31 | 1944-12-08 | Gas turbine driven blower in which the gas turbine runner is connected to the coaxially arranged blower runner by a sleeve |
-
1945
- 1945-03-03 CH CH248083D patent/CH248083A/en unknown
- 1945-09-18 NL NL121197A patent/NL65021C/xx active
- 1945-12-03 GB GB32615/45A patent/GB604730A/en not_active Expired
-
1946
- 1946-02-27 FR FR922972D patent/FR922972A/en not_active Expired
-
1948
- 1948-12-07 DE DEP23823D patent/DE968872C/en not_active Expired
Cited By (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3677663A (en) * | 1970-10-01 | 1972-07-18 | Avco Corp | Damped turbomachine rotor assembly |
WO1981003047A1 (en) * | 1980-04-17 | 1981-10-29 | Carborundum Co | Ceramic radial turbine wheel |
FR2484035A1 (en) * | 1980-06-06 | 1981-12-11 | Klein Schanzlin & Becker Ag | MEANS FOR COUPLING TREES |
US5087176A (en) * | 1984-12-20 | 1992-02-11 | Allied-Signal Inc. | Method and apparatus to provide thermal isolation of process gas bearings |
US6499958B2 (en) | 1999-07-02 | 2002-12-31 | Ingersoll-Rand Company | Device and method for detachably connecting an impeller to a pinion shaft in a high speed fluid compressor |
US6254349B1 (en) | 1999-07-02 | 2001-07-03 | Ingersoll-Rand Company | Device and method for detachably connecting an impeller to a pinion shaft in a high speed fluid compressor |
WO2001025641A1 (en) * | 1999-10-06 | 2001-04-12 | Ingersoll-Rand Co. | Device and method for detachably connecting an impeller to a pinion shaft in a high speed fluid compressor |
US10018205B2 (en) | 2012-11-28 | 2018-07-10 | Napier Turbochargers Limited | Impeller shaft |
WO2015009351A3 (en) * | 2013-07-19 | 2015-04-09 | Praxair Technology, Inc. | Coupling for directly driven compressor |
CN105378316A (en) * | 2013-07-19 | 2016-03-02 | 普莱克斯技术有限公司 | Coupling for directly driven compressor |
US9371835B2 (en) | 2013-07-19 | 2016-06-21 | Praxair Technology, Inc. | Coupling for directly driven compressor |
CN105378316B (en) * | 2013-07-19 | 2019-03-01 | 普莱克斯技术有限公司 | Connector for the compressor directly driven |
CN109296560A (en) * | 2018-11-30 | 2019-02-01 | 无锡市海星船舶动力有限公司 | The ship compressor rotor shaft of resilient dust boot is installed |
Also Published As
Publication number | Publication date |
---|---|
NL65021C (en) | 1949-08-15 |
CH248083A (en) | 1947-04-15 |
FR922972A (en) | 1947-06-24 |
DE968872C (en) | 1958-04-03 |
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