FR1195912A - Rotors for compressors or turbines of the multistage axial type - Google Patents

Rotors for compressors or turbines of the multistage axial type

Info

Publication number
FR1195912A
FR1195912A FR1195912DA FR1195912A FR 1195912 A FR1195912 A FR 1195912A FR 1195912D A FR1195912D A FR 1195912DA FR 1195912 A FR1195912 A FR 1195912A
Authority
FR
France
Prior art keywords
compressors
rotors
turbines
axial type
multistage axial
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
Other languages
French (fr)
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.)
Napier Turbochargers Ltd
Original Assignee
D Napier and 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 D Napier and Son Ltd filed Critical D Napier and Son Ltd
Application granted granted Critical
Publication of FR1195912A publication Critical patent/FR1195912A/en
Expired legal-status Critical Current

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)
FR1195912D 1957-05-15 1958-05-14 Rotors for compressors or turbines of the multistage axial type Expired FR1195912A (en)

Applications Claiming Priority (1)

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

Publications (1)

Publication Number Publication Date
FR1195912A true FR1195912A (en) 1959-11-20

Family

ID=10366246

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1195912D Expired FR1195912A (en) 1957-05-15 1958-05-14 Rotors for compressors or turbines of the multistage axial type

Country Status (3)

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

Cited By (2)

* 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
WO1990006421A1 (en) * 1988-12-09 1990-06-14 Allied-Signal Inc. High temperature turbine engine structure

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AT378575B (en) * 1979-10-25 1985-08-26 Elin Union Ag ROTOR FOR A THERMAL TURBO MACHINE
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

Cited By (2)

* 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
WO1990006421A1 (en) * 1988-12-09 1990-06-14 Allied-Signal Inc. High temperature turbine engine structure

Also Published As

Publication number Publication date
CH344873A (en) 1960-02-29
GB836920A (en) 1960-06-09

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