FR1165132A - Improvements to gas turbines - Google Patents

Improvements to gas turbines

Info

Publication number
FR1165132A
FR1165132A FR1165132DA FR1165132A FR 1165132 A FR1165132 A FR 1165132A FR 1165132D A FR1165132D A FR 1165132DA FR 1165132 A FR1165132 A FR 1165132A
Authority
FR
France
Prior art keywords
gas turbines
turbines
gas
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.)
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
Application granted granted Critical
Publication of FR1165132A publication Critical patent/FR1165132A/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
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/18Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F01D5/181Blades having a closed internal cavity containing a cooling medium, e.g. sodium

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR1165132D 1955-11-28 1956-11-23 Improvements to gas turbines Expired FR1165132A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1165132X 1955-11-28

Publications (1)

Publication Number Publication Date
FR1165132A true FR1165132A (en) 1958-10-20

Family

ID=10879031

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1165132D Expired FR1165132A (en) 1955-11-28 1956-11-23 Improvements to gas turbines

Country Status (1)

Country Link
FR (1) FR1165132A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1209806B (en) * 1961-08-30 1966-01-27 Rolls Royce Blade for axial flow machines, especially gas turbines
DE1236279B (en) * 1962-11-21 1967-03-09 Gen Electric Gas turbine blade
DE1300346B (en) * 1964-08-19 1969-07-31 Director Of Nat Aerospace Lab Gas turbine
FR2460387A1 (en) * 1979-06-30 1981-01-23 Rolls Royce TURBINE DAWN

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1209806B (en) * 1961-08-30 1966-01-27 Rolls Royce Blade for axial flow machines, especially gas turbines
DE1236279B (en) * 1962-11-21 1967-03-09 Gen Electric Gas turbine blade
DE1300346B (en) * 1964-08-19 1969-07-31 Director Of Nat Aerospace Lab Gas turbine
FR2460387A1 (en) * 1979-06-30 1981-01-23 Rolls Royce TURBINE DAWN
US4529357A (en) * 1979-06-30 1985-07-16 Rolls-Royce Ltd Turbine blades

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