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FR1367231A - Improvements to gas turbo-engines - Google Patents

Improvements to gas turbo-engines

Info

Publication number
FR1367231A
FR1367231A FR945185A FR945185A FR1367231A FR 1367231 A FR1367231 A FR 1367231A FR 945185 A FR945185 A FR 945185A FR 945185 A FR945185 A FR 945185A FR 1367231 A FR1367231 A FR 1367231A
Authority
FR
France
Prior art keywords
engines
gas turbo
turbo
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
FR945185A
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
Priority claimed from GB3235262A external-priority patent/GB951298A/en
Application filed by Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to FR945185A priority Critical patent/FR1367231A/en
Application granted granted Critical
Publication of FR1367231A publication Critical patent/FR1367231A/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
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • F01D17/162—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for axial flow, i.e. the vanes turning around axes which are essentially perpendicular to the rotor centre line

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR945185A 1962-08-22 1963-08-20 Improvements to gas turbo-engines Expired FR1367231A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR945185A FR1367231A (en) 1962-08-22 1963-08-20 Improvements to gas turbo-engines

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB3235262A GB951298A (en) 1962-08-22 1962-08-22 Improvements relating to gas turbine engines
FR945185A FR1367231A (en) 1962-08-22 1963-08-20 Improvements to gas turbo-engines

Publications (1)

Publication Number Publication Date
FR1367231A true FR1367231A (en) 1964-07-17

Family

ID=26202968

Family Applications (1)

Application Number Title Priority Date Filing Date
FR945185A Expired FR1367231A (en) 1962-08-22 1963-08-20 Improvements to gas turbo-engines

Country Status (1)

Country Link
FR (1) FR1367231A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2419390A1 (en) * 1978-03-09 1979-10-05 Mtu Muenchen Gmbh ORIENTABLE VANE DISTRIBUTOR FOR AXIAL TURBINE OF GAS TURBINE ENGINE

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2419390A1 (en) * 1978-03-09 1979-10-05 Mtu Muenchen Gmbh ORIENTABLE VANE DISTRIBUTOR FOR AXIAL TURBINE OF GAS TURBINE ENGINE

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