CH344873A - Rotor of a multistage axial flow turbomachine - Google Patents

Rotor of a multistage axial flow turbomachine

Info

Publication number
CH344873A
CH344873A CH344873DA CH344873A CH 344873 A CH344873 A CH 344873A CH 344873D A CH344873D A CH 344873DA CH 344873 A CH344873 A CH 344873A
Authority
CH
Switzerland
Prior art keywords
rotor
axial flow
multistage axial
flow turbomachine
turbomachine
Prior art date
Application number
Other languages
French (fr)
Inventor
Joseph French Michael
Original Assignee
Napier & Son Ltd
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 Napier & Son Ltd filed Critical Napier & Son Ltd
Publication of CH344873A publication Critical patent/CH344873A/en

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
    • 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
    • F01D5/06—Rotors for more than one axial stage, e.g. of drum or multiple disc type; Details thereof, e.g. shafts, shaft connections
    • F01D5/066—Connecting means for joining rotor-discs or rotor-elements together, e.g. by a central bolt, by clamps
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
CH344873D 1957-05-15 1958-05-14 Rotor of a multistage axial flow turbomachine CH344873A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB344873X 1957-05-15

Publications (1)

Publication Number Publication Date
CH344873A true CH344873A (en) 1960-02-29

Family

ID=10366246

Family Applications (1)

Application Number Title Priority Date Filing Date
CH344873D CH344873A (en) 1957-05-15 1958-05-14 Rotor of a multistage axial flow turbomachine

Country Status (3)

Country Link
CH (1) CH344873A (en)
FR (1) FR1195912A (en)
GB (1) GB836920A (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3070348A (en) * 1960-07-25 1962-12-25 Gen Motors Corp Composite rotor
AT378575B (en) * 1979-10-25 1985-08-26 Elin Union Ag ROTOR FOR A THERMAL TURBO MACHINE
US5031400A (en) * 1988-12-09 1991-07-16 Allied-Signal Inc. High temperature turbine engine structure
JP2001003702A (en) * 1999-06-16 2001-01-09 Mitsubishi Heavy Ind Ltd Gas turbine rotor
US6287079B1 (en) * 1999-12-03 2001-09-11 Siemens Westinghouse Power Corporation Shear pin with locking cam
EP1577493A1 (en) * 2004-03-17 2005-09-21 Siemens Aktiengesellschaft Turbomachine and rotor for a turbomachine

Also Published As

Publication number Publication date
FR1195912A (en) 1959-11-20
GB836920A (en) 1960-06-09

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