BE541578A - - Google Patents

Info

Publication number
BE541578A
BE541578A BE541578DA BE541578A BE 541578 A BE541578 A BE 541578A BE 541578D A BE541578D A BE 541578DA BE 541578 A BE541578 A BE 541578A
Authority
BE
Belgium
Application number
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.)
Publication of BE541578A publication Critical patent/BE541578A/xx
Priority claimed from GB1482553A external-priority patent/GB745073A/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
    • F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3053—Fixing blades to rotors; Blade roots ; Blade spacers by means of pins

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
BE541578D 1953-05-27 BE541578A (xx)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB1482553A GB745073A (en) 1953-05-27 1953-05-27 Improvements in or relating to rotors for axial-flow compressors and like machines
GB391459A GB815507A (en) 1953-05-27 1954-10-01 Improvements in or relating to bladed rotors for axial-flow fluid machines

Publications (1)

Publication Number Publication Date
BE541578A true BE541578A (xx)

Family

ID=32395787

Family Applications (1)

Application Number Title Priority Date Filing Date
BE541578D BE541578A (xx) 1953-05-27

Country Status (4)

Country Link
US (1) US2925997A (xx)
BE (1) BE541578A (xx)
FR (1) FR1136390A (xx)
GB (1) GB815506A (xx)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2906496A (en) * 1957-05-28 1959-09-29 Ransom S Thompson Retaining means for pin used for rotor blade attachment
US3039739A (en) * 1958-11-28 1962-06-19 Gen Motors Corp Pinned blade connecting means
US3042369A (en) * 1959-02-11 1962-07-03 Gen Motors Corp Pinned blade sealing means
US3043562A (en) * 1961-04-10 1962-07-10 Gen Electric Combination sealing and restraining member for long-shank turbo-machine buckets
BE635976A (xx) * 1962-08-10
CH516731A (de) * 1969-12-12 1971-12-15 Bbc Sulzer Turbomaschinen Schaufelkranz für Turbomaschinen
US4119389A (en) * 1977-01-17 1978-10-10 General Motors Corporation Radially removable turbine vanes
FR2419389A1 (fr) * 1978-03-08 1979-10-05 Snecma Perfectionnements aux flasques de rotors de turbomachines
US4344740A (en) * 1979-09-28 1982-08-17 United Technologies Corporation Rotor assembly
FR2637321B1 (fr) * 1988-10-05 1990-11-30 Snecma Rotor de turbomachine muni d'un dispositif de fixation des aubes
US5131814A (en) * 1990-04-03 1992-07-21 General Electric Company Turbine blade inner end attachment structure
US10767558B2 (en) * 2018-03-07 2020-09-08 Rolls-Royce North American Technologies Inc. Adaptive-curvature inertial particle separators

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2537739A (en) * 1946-10-26 1951-01-09 Wright Aeronautical Corp Fan blade mounting
FR960069A (xx) * 1947-04-02 1950-04-12
GB679714A (en) * 1949-04-21 1952-09-24 Rolls Royce Improvements in or relating to axial-flow compressors and turbines
GB667979A (en) * 1949-07-28 1952-03-12 Rolls Royce Improvements in or relating to axial flow compressors and turbines

Also Published As

Publication number Publication date
GB815506A (en) 1959-06-24
US2925997A (en) 1960-02-23
FR1136390A (fr) 1957-05-13

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