FR1201123A - Rotor for axial compressor or multistage turbine - Google Patents

Rotor for axial compressor or multistage turbine

Info

Publication number
FR1201123A
FR1201123A FR1201123DA FR1201123A FR 1201123 A FR1201123 A FR 1201123A FR 1201123D A FR1201123D A FR 1201123DA FR 1201123 A FR1201123 A FR 1201123A
Authority
FR
France
Prior art keywords
rotor
axial compressor
multistage turbine
multistage
turbine
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 FR1201123A publication Critical patent/FR1201123A/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
    • 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
    • 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR1201123D 1957-06-14 1958-08-05 Rotor for axial compressor or multistage turbine Expired FR1201123A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB18900/57A GB858763A (en) 1957-06-14 1957-06-14 Rotors for multi-stage axial flow compressors or turbines

Publications (1)

Publication Number Publication Date
FR1201123A true FR1201123A (en) 1959-12-28

Family

ID=10120335

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1201123D Expired FR1201123A (en) 1957-06-14 1958-08-05 Rotor for axial compressor or multistage turbine

Country Status (3)

Country Link
BE (1) BE570301A (en)
FR (1) FR1201123A (en)
GB (1) GB858763A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2834751A1 (en) * 2002-01-17 2003-07-18 Snecma Moteurs ROTOR ARRANGEMENT OF A TURBOMACHINE

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1239820B (en) * 1960-09-20 1967-05-03 Colston Ltd C Low water protection for dishwashers
US3114533A (en) * 1961-04-27 1963-12-17 Gen Electric Rotor construction
DE102007031712A1 (en) * 2007-07-06 2009-01-08 Rolls-Royce Deutschland Ltd & Co Kg Device and method for clamping bladed rotor disks of a jet engine
DE102013213115A1 (en) 2013-07-04 2015-01-22 Siemens Aktiengesellschaft Rotor for a turbine

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2834751A1 (en) * 2002-01-17 2003-07-18 Snecma Moteurs ROTOR ARRANGEMENT OF A TURBOMACHINE
EP1329589A1 (en) * 2002-01-17 2003-07-23 Snecma Moteurs Rotor configuration for a turbomachine
US7008190B2 (en) 2002-01-17 2006-03-07 Snecma Moteurs Turbomachine rotor arrangement

Also Published As

Publication number Publication date
GB858763A (en) 1961-01-18
BE570301A (en) 1958-08-30

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