FR3096086B1 - Capotage acoustique pour une turbomachine ou un ensemble propulsif d’aeronef - Google Patents

Capotage acoustique pour une turbomachine ou un ensemble propulsif d’aeronef Download PDF

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Publication number
FR3096086B1
FR3096086B1 FR1905160A FR1905160A FR3096086B1 FR 3096086 B1 FR3096086 B1 FR 3096086B1 FR 1905160 A FR1905160 A FR 1905160A FR 1905160 A FR1905160 A FR 1905160A FR 3096086 B1 FR3096086 B1 FR 3096086B1
Authority
FR
France
Prior art keywords
turbomachine
propulsion assembly
aircraft propulsion
cowling
acoustic hood
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.)
Active
Application number
FR1905160A
Other languages
English (en)
Other versions
FR3096086A1 (fr
Inventor
Benoît Marty
Frédéric Amblard
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 SA
Original Assignee
Safran 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 Safran SA filed Critical Safran SA
Priority to FR1905160A priority Critical patent/FR3096086B1/fr
Priority to PCT/FR2020/050772 priority patent/WO2020229763A1/fr
Publication of FR3096086A1 publication Critical patent/FR3096086A1/fr
Application granted granted Critical
Publication of FR3096086B1 publication Critical patent/FR3096086B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F02K1/78—Other construction of jet pipes
    • F02K1/82—Jet pipe walls, e.g. liners
    • F02K1/827—Sound absorbing structures or liners
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/24—Heat or noise insulation
    • 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
    • F02K1/44—Nozzles having means, e.g. a shield, reducing sound radiation in a specified direction
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/30—Manufacture with deposition of material
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/50—Building or constructing in particular ways
    • F05D2230/51—Building or constructing in particular ways in a modular way, e.g. using several identical or complementary parts or features
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/20—Three-dimensional
    • F05D2250/23—Three-dimensional prismatic
    • F05D2250/232—Three-dimensional prismatic conical
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/20—Three-dimensional
    • F05D2250/28—Three-dimensional patterned
    • F05D2250/283—Three-dimensional patterned honeycomb
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/96—Preventing, counteracting or reducing vibration or noise
    • F05D2260/963—Preventing, counteracting or reducing vibration or noise by Helmholtz resonators

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Soundproofing, Sound Blocking, And Sound Damping (AREA)

Abstract

Capotage acoustique (20) pour une turbomachine ou un ensemble propuslif d’aéronef, ce capotage ayant une forme annulaire autour d’un axe et comportant deux peaux annulaires, respectivement radialement interne et externe, s’étendant l’une autour de l’autre et reliées entre elles par des cloisons définissant des alvéoles, l’une des peaux comportant des perforations débouchant dans les alvéoles, caractérisé en ce qu’il est formé de plus de six morceaux (20a-20n) fabriqués indépendamment les uns des autres et assemblés pour former le capotage, chacun de ces morceaux comportant une portion de peau interne, une portion peau externe et des cloisons s’étendant entre les portions de peaux interne et externe. Figure pour l'abrégé : Figure 2a
FR1905160A 2019-05-16 2019-05-16 Capotage acoustique pour une turbomachine ou un ensemble propulsif d’aeronef Active FR3096086B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1905160A FR3096086B1 (fr) 2019-05-16 2019-05-16 Capotage acoustique pour une turbomachine ou un ensemble propulsif d’aeronef
PCT/FR2020/050772 WO2020229763A1 (fr) 2019-05-16 2020-05-11 Capotage acoustique pour une turbomachine ou un ensemble propulsif d'aeronef

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1905160 2019-05-16
FR1905160A FR3096086B1 (fr) 2019-05-16 2019-05-16 Capotage acoustique pour une turbomachine ou un ensemble propulsif d’aeronef

Publications (2)

Publication Number Publication Date
FR3096086A1 FR3096086A1 (fr) 2020-11-20
FR3096086B1 true FR3096086B1 (fr) 2022-01-21

Family

ID=67660327

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1905160A Active FR3096086B1 (fr) 2019-05-16 2019-05-16 Capotage acoustique pour une turbomachine ou un ensemble propulsif d’aeronef

Country Status (2)

Country Link
FR (1) FR3096086B1 (fr)
WO (1) WO2020229763A1 (fr)

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5594216A (en) * 1994-11-29 1997-01-14 Lockheed Missiles & Space Co., Inc. Jet engine sound-insulation structure
ES2224807B1 (es) * 2002-08-14 2007-05-01 Sener, Ingenieria Y Sistemas, S.A. Conducto de reduccion de ruido para componentes estaticos de motores aeronauticos.
EP3180185B1 (fr) * 2014-08-12 2020-10-14 HRL Laboratories, LLC Panneau sandwich acoustique à structure à rigidité progressive
FR3028020B1 (fr) 2014-10-29 2016-11-11 Snecma Panneau d'echange thermique et de reduction de bruit ameliore pour une turbomachine
FR3039148B1 (fr) * 2015-07-24 2020-07-17 Safran Nacelles Procede de fabrication d’un panneau d’attenuation acoustique en materiau composite a matrice ceramique et panneau d’attenuation acoustique obtenu par ledit procede

Also Published As

Publication number Publication date
WO2020229763A1 (fr) 2020-11-19
FR3096086A1 (fr) 2020-11-20

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