GB704609A - Improvements in or relating to multi-stage axial-flow compressors or turbines - Google Patents

Improvements in or relating to multi-stage axial-flow compressors or turbines

Info

Publication number
GB704609A
GB704609A GB1918050A GB1918050A GB704609A GB 704609 A GB704609 A GB 704609A GB 1918050 A GB1918050 A GB 1918050A GB 1918050 A GB1918050 A GB 1918050A GB 704609 A GB704609 A GB 704609A
Authority
GB
United Kingdom
Prior art keywords
shell
discs
slots
secured
blades
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
GB1918050A
Other languages
English (en)
Inventor
Nelson Hector Kent
Norman Robert Robinson
Cyril Armer
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 PLC filed Critical Rolls Royce PLC
Priority to GB1918050A priority Critical patent/GB704609A/en
Priority to FR1057994D priority patent/FR1057994A/fr
Priority to CH301115D priority patent/CH301115A/de
Publication of GB704609A publication Critical patent/GB704609A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02Blade-carrying members, e.g. rotors
    • F01D5/06Rotors 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)
GB1918050A 1950-08-01 1950-08-01 Improvements in or relating to multi-stage axial-flow compressors or turbines Expired GB704609A (en)

Priority Applications (3)

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
FR1057994D FR1057994A (fr) 1950-08-01 1952-04-08 Perfectionnements aux rotors de turbo-machines
CH301115D CH301115A (de) 1950-08-01 1952-04-09 Rotor für eine axial beaufschlagte Turbomaschine.

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
GB704609A true GB704609A (en) 1954-02-24

Family

ID=10125074

Family Applications (1)

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

Country Status (3)

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

Cited By (2)

* 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
US7147436B2 (en) * 2004-04-15 2006-12-12 United Technologies Corporation Turbine engine rotor retainer

Families Citing this family (3)

* 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
US4310286A (en) * 1979-05-17 1982-01-12 United Technologies Corporation Rotor assembly having a multistage disk

Cited By (2)

* 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
US7147436B2 (en) * 2004-04-15 2006-12-12 United Technologies Corporation Turbine engine rotor retainer

Also Published As

Publication number Publication date
CH301115A (de) 1954-08-31
FR1057994A (fr) 1954-03-12

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