GB604730A - Improvements in or relating to rotors for turbo-machines - Google Patents

Improvements in or relating to rotors for turbo-machines

Info

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
Application number
GB32615/45A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Sulzer AG
Original Assignee
Sulzer AG
Sulzer Freres SA
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Sulzer AG, Sulzer Freres SA filed Critical Sulzer AG
Publication of GB604730A publication Critical patent/GB604730A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02Blade-carrying members, e.g. rotors
    • F01D5/04Blade-carrying members, e.g. rotors for radial-flow machines or engines
    • F01D5/043Blade-carrying members, e.g. rotors for radial-flow machines or engines of the axial inlet- radial outlet, or vice versa, type
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02Blade-carrying members, e.g. rotors
    • F01D5/025Fixing blade carrying members on shafts
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02Blade-carrying members, e.g. rotors
    • F01D5/04Blade-carrying members, e.g. rotors for radial-flow machines or engines
    • F01D5/043Blade-carrying members, e.g. rotors for radial-flow machines or engines of the axial inlet- radial outlet, or vice versa, type
    • F01D5/045Blade-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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/266Rotors 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.
GB32615/45A 1945-03-03 1945-12-03 Improvements in or relating to rotors for turbo-machines Expired GB604730A (en)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

Cited By (13)

* Cited by examiner, † Cited by third party
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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