CH315706A - Multi-stage turbine rotor - Google Patents

Multi-stage turbine rotor

Info

Publication number
CH315706A
CH315706A CH315706DA CH315706A CH 315706 A CH315706 A CH 315706A CH 315706D A CH315706D A CH 315706DA CH 315706 A CH315706 A CH 315706A
Authority
CH
Switzerland
Prior art keywords
turbine rotor
stage turbine
stage
rotor
turbine
Prior art date
Application number
Other languages
French (fr)
Inventor
Bernard Halford Frank
Ker Wilson William
Original Assignee
Havilland Engine Company Limit
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 Havilland Engine Company Limit filed Critical Havilland Engine Company Limit
Publication of CH315706A publication Critical patent/CH315706A/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
CH315706D 1952-07-10 1953-12-22 Multi-stage turbine rotor CH315706A (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
CH315706A true CH315706A (en) 1956-08-31

Family

ID=10094835

Family Applications (1)

Application Number Title Priority Date Filing Date
CH315706D CH315706A (en) 1952-07-10 1953-12-22 Multi-stage turbine rotor

Country Status (3)

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

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1261356B (en) * 1960-03-03 1968-02-15 United Aircraft Corp Runner for axial flow machines

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1261356B (en) * 1960-03-03 1968-02-15 United Aircraft Corp Runner for axial flow machines

Also Published As

Publication number Publication date
FR1098567A (en) 1955-08-08
GB749578A (en) 1956-05-30

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