FR1433712A - Fluid flow regulator - Google Patents

Fluid flow regulator

Info

Publication number
FR1433712A
FR1433712A FR14236A FR14236A FR1433712A FR 1433712 A FR1433712 A FR 1433712A FR 14236 A FR14236 A FR 14236A FR 14236 A FR14236 A FR 14236A FR 1433712 A FR1433712 A FR 1433712A
Authority
FR
France
Prior art keywords
fluid flow
flow regulator
regulator
fluid
flow
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
FR14236A
Other languages
French (fr)
Inventor
Francis Jeffrey Colville
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 GB17164/64A external-priority patent/GB1002116A/en
Application filed by Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to FR14236A priority Critical patent/FR1433712A/en
Application granted granted Critical
Publication of FR1433712A publication Critical patent/FR1433712A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
    • F02K1/1215—Varying effective area of jet pipe or nozzle by means of pivoted flaps of two series of flaps, the upstream series having its flaps hinged at their upstream ends on a fixed structure, and the downstream series having its flaps hinged at their downstream ends on a fixed structure
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
    • F02K1/1207—Varying effective area of jet pipe or nozzle by means of pivoted flaps of one series of flaps hinged at their upstream ends on a fixed structure

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR14236A 1964-04-24 1965-04-22 Fluid flow regulator Expired FR1433712A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR14236A FR1433712A (en) 1964-04-24 1965-04-22 Fluid flow regulator

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB17164/64A GB1002116A (en) 1964-04-24 1964-04-24 Fluid flow control apparatus
FR14236A FR1433712A (en) 1964-04-24 1965-04-22 Fluid flow regulator

Publications (1)

Publication Number Publication Date
FR1433712A true FR1433712A (en) 1966-04-01

Family

ID=26163319

Family Applications (1)

Application Number Title Priority Date Filing Date
FR14236A Expired FR1433712A (en) 1964-04-24 1965-04-22 Fluid flow regulator

Country Status (1)

Country Link
FR (1) FR1433712A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0100697A1 (en) * 1982-06-28 1984-02-15 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Nozzle flap of a carbon and steel composite structure

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0100697A1 (en) * 1982-06-28 1984-02-15 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Nozzle flap of a carbon and steel composite structure

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