CH301115A - Rotor für eine axial beaufschlagte Turbomaschine. - Google Patents

Rotor für eine axial beaufschlagte Turbomaschine.

Info

Publication number
CH301115A
CH301115A CH301115DA CH301115A CH 301115 A CH301115 A CH 301115A CH 301115D A CH301115D A CH 301115DA CH 301115 A CH301115 A CH 301115A
Authority
CH
Switzerland
Prior art keywords
rotor
axially loaded
turbomachine
loaded turbomachine
axially
Prior art date
Application number
Other languages
English (en)
Inventor
Limited Rolls-Royce
Original Assignee
Rolls Royce
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 Rolls Royce filed Critical Rolls Royce
Publication of CH301115A publication Critical patent/CH301115A/de

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

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)
CH301115D 1950-08-01 1952-04-09 Rotor für eine axial beaufschlagte Turbomaschine. CH301115A (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1918050A GB704609A (en) 1950-08-01 1950-08-01 Improvements in or relating to multi-stage axial-flow compressors or turbines

Publications (1)

Publication Number Publication Date
CH301115A true CH301115A (de) 1954-08-31

Family

ID=10125074

Family Applications (1)

Application Number Title Priority Date Filing Date
CH301115D CH301115A (de) 1950-08-01 1952-04-09 Rotor für eine axial beaufschlagte Turbomaschine.

Country Status (3)

Country Link
CH (1) CH301115A (de)
FR (1) FR1057994A (de)
GB (1) GB704609A (de)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1095453B (de) * 1955-07-18 1960-12-22 Rolls Royce Mehrstufige Axialstroemungsmaschine
DE1140306B (de) * 1958-07-17 1962-11-29 Daimler Benz Ag Trommellaeufer fuer Axialstroemungsmaschinen, insbesondere Verdichter

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3173655A (en) * 1961-09-08 1965-03-16 Stalker Corp Bladed rotor
US4310286A (en) * 1979-05-17 1982-01-12 United Technologies Corporation Rotor assembly having a multistage disk
US7147436B2 (en) * 2004-04-15 2006-12-12 United Technologies Corporation Turbine engine rotor retainer

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1095453B (de) * 1955-07-18 1960-12-22 Rolls Royce Mehrstufige Axialstroemungsmaschine
DE1140306B (de) * 1958-07-17 1962-11-29 Daimler Benz Ag Trommellaeufer fuer Axialstroemungsmaschinen, insbesondere Verdichter

Also Published As

Publication number Publication date
GB704609A (en) 1954-02-24
FR1057994A (fr) 1954-03-12

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