FR1343676A - Device for adjusting the passage section of a nozzle - Google Patents

Device for adjusting the passage section of a nozzle

Info

Publication number
FR1343676A
FR1343676A FR911650A FR911650A FR1343676A FR 1343676 A FR1343676 A FR 1343676A FR 911650 A FR911650 A FR 911650A FR 911650 A FR911650 A FR 911650A FR 1343676 A FR1343676 A FR 1343676A
Authority
FR
France
Prior art keywords
nozzle
adjusting
passage section
passage
section
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
FR911650A
Other languages
French (fr)
Inventor
Paul Lambotte
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.)
Bronzavia SA
Original Assignee
Bronzavia SA
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 Bronzavia SA filed Critical Bronzavia SA
Priority to FR911650A priority Critical patent/FR1343676A/en
Application granted granted Critical
Publication of FR1343676A publication Critical patent/FR1343676A/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
    • F02K1/15—Control or regulation
    • 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
    • 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
    • F02K1/15—Control or regulation
    • F02K1/18—Control or regulation automatic

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR911650A 1962-10-09 1962-10-09 Device for adjusting the passage section of a nozzle Expired FR1343676A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR911650A FR1343676A (en) 1962-10-09 1962-10-09 Device for adjusting the passage section of a nozzle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR911650A FR1343676A (en) 1962-10-09 1962-10-09 Device for adjusting the passage section of a nozzle

Publications (1)

Publication Number Publication Date
FR1343676A true FR1343676A (en) 1963-11-22

Family

ID=8788302

Family Applications (1)

Application Number Title Priority Date Filing Date
FR911650A Expired FR1343676A (en) 1962-10-09 1962-10-09 Device for adjusting the passage section of a nozzle

Country Status (1)

Country Link
FR (1) FR1343676A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2976624A1 (en) * 2011-06-15 2012-12-21 Snecma Dual-flow turbomotor i.e. dual-flow turbojet, for aircraft, has controllable system connected to pneumatic feeding source so as to occupy inflated state, in which outlet section is maximum by movement of downstream structural part

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2976624A1 (en) * 2011-06-15 2012-12-21 Snecma Dual-flow turbomotor i.e. dual-flow turbojet, for aircraft, has controllable system connected to pneumatic feeding source so as to occupy inflated state, in which outlet section is maximum by movement of downstream structural part

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