FR2978989B1 - Cone d'ejection pour turboreacteur d'aeronef - Google Patents

Cone d'ejection pour turboreacteur d'aeronef

Info

Publication number
FR2978989B1
FR2978989B1 FR1157321A FR1157321A FR2978989B1 FR 2978989 B1 FR2978989 B1 FR 2978989B1 FR 1157321 A FR1157321 A FR 1157321A FR 1157321 A FR1157321 A FR 1157321A FR 2978989 B1 FR2978989 B1 FR 2978989B1
Authority
FR
France
Prior art keywords
turbojet engine
aircraft turbojet
ejection cone
ejection
cone
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
FR1157321A
Other languages
English (en)
Other versions
FR2978989A1 (fr
Inventor
Helene Malot
Philippe Bienvenu
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 Nacelles SAS
Original Assignee
Aircelle 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
Priority to FR1157321A priority Critical patent/FR2978989B1/fr
Application filed by Aircelle SA filed Critical Aircelle SA
Priority to BR112014001679A priority patent/BR112014001679A2/pt
Priority to CN201280039233.1A priority patent/CN103717870A/zh
Priority to RU2014108721/06A priority patent/RU2014108721A/ru
Priority to CA2842874A priority patent/CA2842874A1/fr
Priority to EP12744051.9A priority patent/EP2742230A1/fr
Priority to PCT/FR2012/051583 priority patent/WO2013024218A1/fr
Publication of FR2978989A1 publication Critical patent/FR2978989A1/fr
Application granted granted Critical
Publication of FR2978989B1 publication Critical patent/FR2978989B1/fr
Priority to US14/177,494 priority patent/US9051899B2/en
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
    • 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
    • F02K1/04—Mounting of an exhaust cone in the jet pipe
    • 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
    • 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
    • F02K1/80—Couplings or connections
    • 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
    • F05D2230/20—Manufacture essentially without removing material
    • F05D2230/23—Manufacture essentially without removing material by permanently joining parts together
    • F05D2230/232—Manufacture essentially without removing material by permanently joining parts together by welding
    • 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
    • F05D2260/30—Retaining components in desired mutual position
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

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)
  • Exhaust Silencers (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR1157321A 2011-08-12 2011-08-12 Cone d'ejection pour turboreacteur d'aeronef Active FR2978989B1 (fr)

Priority Applications (8)

Application Number Priority Date Filing Date Title
FR1157321A FR2978989B1 (fr) 2011-08-12 2011-08-12 Cone d'ejection pour turboreacteur d'aeronef
CN201280039233.1A CN103717870A (zh) 2011-08-12 2012-07-05 涡轮喷气发动机的排气锥
RU2014108721/06A RU2014108721A (ru) 2011-08-12 2012-07-05 Конус сопла для турбореактивного двигателя летательного аппарата
CA2842874A CA2842874A1 (fr) 2011-08-12 2012-07-05 Cone d'ejection pour turboreacteur d'aeronef
BR112014001679A BR112014001679A2 (pt) 2011-08-12 2012-07-05 cone de escape para motor turbojato de aeronave
EP12744051.9A EP2742230A1 (fr) 2011-08-12 2012-07-05 Cône d'éjection pour turboréacteur d'aéronef
PCT/FR2012/051583 WO2013024218A1 (fr) 2011-08-12 2012-07-05 Cône d'éjection pour turboréacteur d'aéronef
US14/177,494 US9051899B2 (en) 2011-08-12 2014-02-11 Exhaust cone for aircraft turbojet engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1157321A FR2978989B1 (fr) 2011-08-12 2011-08-12 Cone d'ejection pour turboreacteur d'aeronef

Publications (2)

Publication Number Publication Date
FR2978989A1 FR2978989A1 (fr) 2013-02-15
FR2978989B1 true FR2978989B1 (fr) 2013-07-26

Family

ID=46639577

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1157321A Active FR2978989B1 (fr) 2011-08-12 2011-08-12 Cone d'ejection pour turboreacteur d'aeronef

Country Status (8)

Country Link
US (1) US9051899B2 (fr)
EP (1) EP2742230A1 (fr)
CN (1) CN103717870A (fr)
BR (1) BR112014001679A2 (fr)
CA (1) CA2842874A1 (fr)
FR (1) FR2978989B1 (fr)
RU (1) RU2014108721A (fr)
WO (1) WO2013024218A1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107709744A (zh) * 2015-06-11 2018-02-16 赛峰飞机发动机公司 包括排气壳体和下游旋转对称部件的组件

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3026786B1 (fr) * 2014-10-07 2019-07-26 Safran Aircraft Engines Flasque de fermeture d'un carter d'echappement
US10337453B2 (en) * 2015-04-21 2019-07-02 Rohr, Inc. Attachment feature for a core panel
CN105298684B (zh) * 2015-09-18 2017-11-03 中国航空工业集团公司沈阳发动机设计研究所 一种航空发动机用尾椎连接结构
FR3043138B1 (fr) * 2015-11-04 2019-09-13 Safran Aircraft Engines Tube de degazage et cone d'ejection pour une turbomachine, ainsi que leur outillage de montage
US10907508B2 (en) * 2015-11-12 2021-02-02 Rohr, Inc. Turbine engine and exhaust system connection
FR3082238A1 (fr) * 2018-06-11 2019-12-13 Airbus Operations Tuyere primaire d'un conduit d'ejection primaire d'une turbomachine
FR3084917B1 (fr) * 2018-08-09 2021-04-16 Safran Ceram Ensemble pour une tuyere d'ejection de turbomachine
FR3084916B1 (fr) * 2018-08-10 2020-07-17 Safran Ceramics Cone d'ejection a fixation flexible
CN109372653A (zh) * 2018-12-13 2019-02-22 中国航发沈阳发动机研究所 一种涡扇发动机降噪排气组件
FR3098552B1 (fr) * 2019-07-08 2022-07-15 Airbus Operations Sas Turbomachine comportant une structure et une structure interne d’un conduit d’ejection primaire fixee a ladite structure
FR3100575B1 (fr) * 2019-09-05 2022-04-08 Safran Ceram Cone d’ejection a fixation flexible aerodynamique
FR3100845B1 (fr) * 2019-09-13 2022-07-08 Safran Nacelles Organe de tuyère extérieur pour turbomachine
FR3115832B1 (fr) * 2020-11-05 2023-04-21 Safran Nacelles Ensemble pour une turbomachine
FR3115830B1 (fr) * 2020-11-05 2022-09-30 Safran Nacelles Ensemble pour une turbomachine
US11867077B2 (en) 2021-06-07 2024-01-09 Rohr, Inc. Acoustic structure with floating interior skin
US11976597B2 (en) 2021-09-13 2024-05-07 Rohr, Inc. Low-frequency acoustic center body

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1543312A (en) * 1976-07-21 1979-04-04 Rolls Royce Honeycomb linings
FR2623249A1 (fr) * 1987-11-12 1989-05-19 Snecma Ensemble constitue de deux pieces en materiaux ayant des coefficients de dilatation differents, reliees entre elles et methode d'assemblage
GB9120658D0 (en) * 1991-09-27 1991-11-06 Short Brothers Plc Ducted fan turbine engine
US5251435A (en) * 1991-10-30 1993-10-12 General Electric Company Reverser inner cowl with integral bifurcation walls and core cowl
GB9613615D0 (en) * 1996-06-28 1996-08-28 Short Brothers Plc Method of manufacturing a noise attenuation panel
FR2869874B1 (fr) * 2004-05-04 2006-06-23 Snecma Moteurs Sa Moteur d'avion avec des moyens de suspension a la structure d'un avion
US7870722B2 (en) * 2006-12-06 2011-01-18 The Boeing Company Systems and methods for passively directing aircraft engine nozzle flows
FR2920146B1 (fr) * 2007-08-20 2009-10-30 Aircelle Sa Nacelle a section de sortie adaptable
FR2935753B1 (fr) * 2008-09-08 2011-07-01 Snecma Propulsion Solide Liaisons souples a butee pour fixation de piece en cmc
DE102008051241B4 (de) * 2008-10-10 2011-06-16 Airbus Operations Gmbh Schalldämpfer für ein Hilfstriebwerk eines Flugzeugs
FR2949820B1 (fr) * 2009-09-04 2011-10-14 Aircelle Sa Ensemble structurant pour une tuyere d'ejection.
US8579584B2 (en) * 2010-10-06 2013-11-12 Dewain Ray Brown Turbofan jet engine
US9279386B2 (en) * 2012-03-09 2016-03-08 Hamilton Sundstrand Corporation Jet noise reduction using eduction effect
FR2988777B1 (fr) * 2012-03-29 2014-04-25 Snecma Propulsion Solide Integration de pieces d'arriere-corps de moteur aeronautique
US8985942B2 (en) * 2012-07-02 2015-03-24 United Technologies Corporation Turbine exhaust case duct

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107709744A (zh) * 2015-06-11 2018-02-16 赛峰飞机发动机公司 包括排气壳体和下游旋转对称部件的组件
CN107709744B (zh) * 2015-06-11 2019-09-20 赛峰飞机发动机公司 包括排气壳体和下游旋转对称部件的组件

Also Published As

Publication number Publication date
CN103717870A (zh) 2014-04-09
US20140158458A1 (en) 2014-06-12
US9051899B2 (en) 2015-06-09
BR112014001679A2 (pt) 2017-03-07
FR2978989A1 (fr) 2013-02-15
EP2742230A1 (fr) 2014-06-18
CA2842874A1 (fr) 2013-02-21
WO2013024218A1 (fr) 2013-02-21
RU2014108721A (ru) 2015-09-20

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