FR1098567A - Multistage Turbine Rotor Improvements - Google Patents

Multistage Turbine Rotor Improvements

Info

Publication number
FR1098567A
FR1098567A FR1098567DA FR1098567A FR 1098567 A FR1098567 A FR 1098567A FR 1098567D A FR1098567D A FR 1098567DA FR 1098567 A FR1098567 A FR 1098567A
Authority
FR
France
Prior art keywords
turbine rotor
multistage turbine
multistage
rotor
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.)
Bristol Siddeley Engines Ltd
Original Assignee
De Havilland Engine Co 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 De Havilland Engine Co Ltd filed Critical De Havilland Engine Co Ltd
Application granted granted Critical
Publication of FR1098567A publication Critical patent/FR1098567A/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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Mounting Of Bearings Or Others (AREA)
FR1098567D 1952-07-10 1954-01-15 Multistage Turbine Rotor Improvements Expired FR1098567A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1741752A GB749578A (en) 1952-07-10 1952-07-10 Improvements in or relating to multi-stage turbine rotor assemblies

Publications (1)

Publication Number Publication Date
FR1098567A true FR1098567A (en) 1955-08-08

Family

ID=10094835

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1098567D Expired FR1098567A (en) 1952-07-10 1954-01-15 Multistage Turbine Rotor Improvements

Country Status (3)

Country Link
CH (1) CH315706A (en)
FR (1) FR1098567A (en)
GB (1) GB749578A (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3083947A (en) * 1960-03-03 1963-04-02 United Aircraft Corp Compressor spacer
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

Also Published As

Publication number Publication date
CH315706A (en) 1956-08-31
GB749578A (en) 1956-05-30

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