FR937533A - Axial compressor rotor - Google Patents

Axial compressor rotor

Info

Publication number
FR937533A
FR937533A FR937533DA FR937533A FR 937533 A FR937533 A FR 937533A FR 937533D A FR937533D A FR 937533DA FR 937533 A FR937533 A FR 937533A
Authority
FR
France
Prior art keywords
compressor rotor
axial compressor
axial
rotor
compressor
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.)
Compagnie Electro Mecanique SA
Original Assignee
Compagnie Electro Mecanique 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 Compagnie Electro Mecanique SA filed Critical Compagnie Electro Mecanique SA
Application granted granted Critical
Publication of FR937533A publication Critical patent/FR937533A/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
    • 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)
FR937533D 1946-11-26 1946-11-26 Axial compressor rotor Expired FR937533A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR937533T 1946-11-26

Publications (1)

Publication Number Publication Date
FR937533A true FR937533A (en) 1948-08-19

Family

ID=9458035

Family Applications (1)

Application Number Title Priority Date Filing Date
FR937533D Expired FR937533A (en) 1946-11-26 1946-11-26 Axial compressor rotor

Country Status (1)

Country Link
FR (1) FR937533A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2672279A (en) * 1950-08-03 1954-03-16 United Aircraft Corp End bell construction
EP0529379A1 (en) * 1991-08-29 1993-03-03 KSB Aktiengesellschaft Rotor assembly for turbomachines
EP1672172A1 (en) * 2004-12-17 2006-06-21 United Technologies Corporation Turbine engine rotor stack
ITMI20100684A1 (en) * 2010-04-21 2011-10-22 Nuovo Pignone Spa STACKED ROTOR WITH TIE AND BOLTED FLANGE AND METHOD

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2672279A (en) * 1950-08-03 1954-03-16 United Aircraft Corp End bell construction
EP0529379A1 (en) * 1991-08-29 1993-03-03 KSB Aktiengesellschaft Rotor assembly for turbomachines
EP1672172A1 (en) * 2004-12-17 2006-06-21 United Technologies Corporation Turbine engine rotor stack
US7309210B2 (en) 2004-12-17 2007-12-18 United Technologies Corporation Turbine engine rotor stack
ITMI20100684A1 (en) * 2010-04-21 2011-10-22 Nuovo Pignone Spa STACKED ROTOR WITH TIE AND BOLTED FLANGE AND METHOD
US8967960B2 (en) 2010-04-21 2015-03-03 Nuovo Pignone, S.P.A. Stack rotor with tie rod and bolted flange and method
EP2381109A3 (en) * 2010-04-21 2017-11-22 Nuovo Pignone S.p.A. Rotor stack for centrifugal compressor

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