FR1257577A - Convergent-Divergent Exhaust Nozzle with Flow Stabilizer - Google Patents

Convergent-Divergent Exhaust Nozzle with Flow Stabilizer

Info

Publication number
FR1257577A
FR1257577A FR828334A FR828334A FR1257577A FR 1257577 A FR1257577 A FR 1257577A FR 828334 A FR828334 A FR 828334A FR 828334 A FR828334 A FR 828334A FR 1257577 A FR1257577 A FR 1257577A
Authority
FR
France
Prior art keywords
convergent
exhaust nozzle
flow stabilizer
divergent exhaust
divergent
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
FR828334A
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.)
General Electric Co
Original Assignee
General Electric Co
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 CH569760A external-priority patent/CH384944A/en
Application filed by General Electric Co filed Critical General Electric Co
Priority to FR828334A priority Critical patent/FR1257577A/en
Application granted granted Critical
Publication of FR1257577A publication Critical patent/FR1257577A/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
    • 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
FR828334A 1960-05-18 1960-05-27 Convergent-Divergent Exhaust Nozzle with Flow Stabilizer Expired FR1257577A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR828334A FR1257577A (en) 1960-05-18 1960-05-27 Convergent-Divergent Exhaust Nozzle with Flow Stabilizer

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CH569760A CH384944A (en) 1960-05-18 1960-05-18 Convergent-divergent exhaust nozzle
FR828334A FR1257577A (en) 1960-05-18 1960-05-27 Convergent-Divergent Exhaust Nozzle with Flow Stabilizer

Publications (1)

Publication Number Publication Date
FR1257577A true FR1257577A (en) 1961-03-31

Family

ID=25698220

Family Applications (1)

Application Number Title Priority Date Filing Date
FR828334A Expired FR1257577A (en) 1960-05-18 1960-05-27 Convergent-Divergent Exhaust Nozzle with Flow Stabilizer

Country Status (1)

Country Link
FR (1) FR1257577A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3371743A (en) * 1965-04-29 1968-03-05 American Radiator & Standard Jet exhaust silencing nozzle with suction applied at exit wall
FR2602275A1 (en) * 1986-08-04 1988-02-05 Onera (Off Nat Aerospatiale) IMPROVEMENTS IN PULSES OF PROPELLERS FOR REDUCING LATERAL EFFORTS
US6094907A (en) * 1996-06-05 2000-08-01 The Boeing Company Jet engine and method for reducing jet engine noise by reducing nacelle boundary layer thickness

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3371743A (en) * 1965-04-29 1968-03-05 American Radiator & Standard Jet exhaust silencing nozzle with suction applied at exit wall
FR2602275A1 (en) * 1986-08-04 1988-02-05 Onera (Off Nat Aerospatiale) IMPROVEMENTS IN PULSES OF PROPELLERS FOR REDUCING LATERAL EFFORTS
US6094907A (en) * 1996-06-05 2000-08-01 The Boeing Company Jet engine and method for reducing jet engine noise by reducing nacelle boundary layer thickness

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