FR1113517A - Improvements to rotor assemblies of gas turbines - Google Patents

Improvements to rotor assemblies of gas turbines

Info

Publication number
FR1113517A
FR1113517A FR1113517DA FR1113517A FR 1113517 A FR1113517 A FR 1113517A FR 1113517D A FR1113517D A FR 1113517DA FR 1113517 A FR1113517 A FR 1113517A
Authority
FR
France
Prior art keywords
gas turbines
rotor assemblies
assemblies
rotor
turbines
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 Aeroplane Co Ltd
Original Assignee
Bristol Aeroplane 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 Bristol Aeroplane Co Ltd filed Critical Bristol Aeroplane Co Ltd
Application granted granted Critical
Publication of FR1113517A publication Critical patent/FR1113517A/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
    • F01D5/08—Heating, heat-insulating or cooling means
    • F01D5/081—Cooling fluid being directed on the side of the rotor disc or at the roots of the blades

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR1113517D 1953-11-20 1954-11-17 Improvements to rotor assemblies of gas turbines Expired FR1113517A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1113517X 1953-11-20

Publications (1)

Publication Number Publication Date
FR1113517A true FR1113517A (en) 1956-03-30

Family

ID=10875012

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1113517D Expired FR1113517A (en) 1953-11-20 1954-11-17 Improvements to rotor assemblies of gas turbines

Country Status (1)

Country Link
FR (1) FR1113517A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3070351A (en) * 1959-02-06 1962-12-25 Gen Motors Corp Blade retention
FR2130011A1 (en) * 1971-03-26 1972-11-03 Aviat Supply R Unis
FR2732405A1 (en) * 1982-03-23 1996-10-04 Snecma Cooling circuit for rotors of gas turbine

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3070351A (en) * 1959-02-06 1962-12-25 Gen Motors Corp Blade retention
FR2130011A1 (en) * 1971-03-26 1972-11-03 Aviat Supply R Unis
FR2732405A1 (en) * 1982-03-23 1996-10-04 Snecma Cooling circuit for rotors of gas turbine

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