FR1422203A - Perfectionnement à la régulation de section des tuyères à effet de silencieux - Google Patents

Perfectionnement à la régulation de section des tuyères à effet de silencieux

Info

Publication number
FR1422203A
FR1422203A FR993637A FR993637A FR1422203A FR 1422203 A FR1422203 A FR 1422203A FR 993637 A FR993637 A FR 993637A FR 993637 A FR993637 A FR 993637A FR 1422203 A FR1422203 A FR 1422203A
Authority
FR
France
Prior art keywords
improvement
section regulation
silencer effect
nozzles
effect nozzles
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
FR993637A
Other languages
English (en)
Inventor
Rene Gerard Hoch
Louis Francois Jumelle
Jean-Marie Minos
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.)
Safran Aircraft Engines SAS
Original Assignee
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
SNECMA SAS
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 Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SAS filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Priority to FR993637A priority Critical patent/FR1422203A/fr
Priority to US498259A priority patent/US3351155A/en
Priority to GB46265/65A priority patent/GB1116639A/en
Application granted granted Critical
Publication of FR1422203A publication Critical patent/FR1422203A/fr
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
    • F02K1/1207—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
    • F02K1/46—Nozzles having means for adding air to the jet or for augmenting the mixing region between the jet and the ambient air, e.g. for silencing

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Exhaust Silencers (AREA)
  • Sampling And Sample Adjustment (AREA)
FR993637A 1964-11-03 1964-11-03 Perfectionnement à la régulation de section des tuyères à effet de silencieux Expired FR1422203A (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR993637A FR1422203A (fr) 1964-11-03 1964-11-03 Perfectionnement à la régulation de section des tuyères à effet de silencieux
US498259A US3351155A (en) 1964-11-03 1965-10-20 Adjustable jet silencer nozzle with controlled flaps and follower flaps
GB46265/65A GB1116639A (en) 1964-11-03 1965-11-02 Improvements in or relating to variable area turbojet nozzles

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR993637A FR1422203A (fr) 1964-11-03 1964-11-03 Perfectionnement à la régulation de section des tuyères à effet de silencieux

Publications (1)

Publication Number Publication Date
FR1422203A true FR1422203A (fr) 1965-12-24

Family

ID=8841664

Family Applications (1)

Application Number Title Priority Date Filing Date
FR993637A Expired FR1422203A (fr) 1964-11-03 1964-11-03 Perfectionnement à la régulation de section des tuyères à effet de silencieux

Country Status (3)

Country Link
US (1) US3351155A (fr)
FR (1) FR1422203A (fr)
GB (1) GB1116639A (fr)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4422524A (en) * 1982-03-22 1983-12-27 Lockheed Corporation Variable shape, fluid flow nozzle for sound suppression
US6487848B2 (en) 1998-11-06 2002-12-03 United Technologies Corporation Gas turbine engine jet noise suppressor
US6612106B2 (en) 2000-05-05 2003-09-02 The Boeing Company Segmented mixing device having chevrons for exhaust noise reduction in jet engines
GB2372779A (en) * 2001-03-03 2002-09-04 Rolls Royce Plc Gas turbine engine nozzle with noise reducing tabs
GB0105349D0 (en) * 2001-03-03 2001-04-18 Rolls Royce Plc Gas turbine engine exhaust nozzle
US6718752B2 (en) * 2002-05-29 2004-04-13 The Boeing Company Deployable segmented exhaust nozzle for a jet engine
US7340883B2 (en) 2004-11-12 2008-03-11 The Boeing Company Morphing structure
EP2074312B1 (fr) * 2006-10-12 2017-12-13 United Technologies Corporation Tuyère à section variable pour nacelle de soufflante de moteur à turbine à gaz équipée d' un système d'actionnement coulissant
FR2928183A1 (fr) * 2008-02-29 2009-09-04 Aircelle Sa Dispositif de reduction de bruit pour moteur d'aeronef, du type a chevrons mobiles
FR2934875B1 (fr) * 2008-08-06 2010-08-13 Aircelle Sa Nacelle de turboreacteur a chevrons mobiles.
GB201115860D0 (en) 2011-09-14 2011-10-26 Rolls Royce Plc A variable geometry structure
GB201609071D0 (en) 2016-05-24 2016-07-06 Rolls Royce Plc Aircraft gas turbine engine nacelle
US11004703B1 (en) * 2019-10-25 2021-05-11 Xia Tai Xin Semiconductor (Qing Dao) Ltd. Gas flow guiding device for semiconductor processing apparatus and method of using the same

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2886946A (en) * 1955-04-14 1959-05-19 Canadair Ltd Thrust reversing device for turbojet engines
GB868868A (en) * 1959-01-15 1961-05-25 Rolls Royce Improvements in or relating to jet propulsion nozzle arrangements
US3057150A (en) * 1961-03-27 1962-10-09 United Aircraft Corp Two dimensional floating blow-in-door and flap ejector
FR1376576A (fr) * 1963-08-02 1964-10-31 Snecma Silencieux pour réacteurs

Also Published As

Publication number Publication date
US3351155A (en) 1967-11-07
GB1116639A (en) 1968-06-12

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