FR3136516B1 - Ensemble pour turbomachine - Google Patents

Ensemble pour turbomachine Download PDF

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Publication number
FR3136516B1
FR3136516B1 FR2205720A FR2205720A FR3136516B1 FR 3136516 B1 FR3136516 B1 FR 3136516B1 FR 2205720 A FR2205720 A FR 2205720A FR 2205720 A FR2205720 A FR 2205720A FR 3136516 B1 FR3136516 B1 FR 3136516B1
Authority
FR
France
Prior art keywords
ejection cone
exhaust casing
longitudinal axis
annular portion
circumferentially
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
FR2205720A
Other languages
English (en)
Other versions
FR3136516A1 (fr
Inventor
Bertrand Léon Marie Desjoyeaux
Philippe Avenel
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
Safran Nacelles 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 Safran Nacelles SAS filed Critical Safran Nacelles SAS
Priority to FR2205720A priority Critical patent/FR3136516B1/fr
Priority to PCT/FR2023/050806 priority patent/WO2023242496A1/fr
Priority to US18/869,147 priority patent/US20250341192A1/en
Priority to EP23736415.3A priority patent/EP4540514A1/fr
Publication of FR3136516A1 publication Critical patent/FR3136516A1/fr
Application granted granted Critical
Publication of FR3136516B1 publication Critical patent/FR3136516B1/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
    • F02K1/04—Mounting of an exhaust cone in the jet pipe
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/243—Flange connections; Bolting arrangements
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/30—Exhaust heads, chambers, or the like
    • 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
    • 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
    • F02K1/805—Sealing devices therefor, e.g. for movable parts of jet pipes or nozzle flaps
    • 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
    • F05D2230/60—Assembly methods
    • F05D2230/64—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins
    • F05D2230/642—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins using maintaining alignment while permitting differential dilatation
    • 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
    • F05D2240/00—Components
    • F05D2240/40—Use of a multiplicity of similar components
    • 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
    • F05D2240/00—Components
    • F05D2240/55—Seals

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Gasket Seals (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

Ensemble pour turbomachine d’axe longitudinal (X) comprenant un cône d’éjection (40) comprenant une paroi annulaire (44) ; un carter d’échappement agencé en amont du cône d’éjection (40) ; une bride de liaison (46) disposée longitudinalement entre le carter d’échappement et le cône d’éjection (40), la bride de liaison (46) comprenant une partie annulaire (47) qui est fixée au carter d’échappement et des pattes de liaison (50) s’étendant longitudinalement vers l’aval depuis la partie annulaire, les pattes de liaison (50) étant distribuées circonférentiellement autour de l’axe longitudinal (X), chaque patte de liaison (50) étant reliée à la paroi annulaire (44) du cône d’éjection (40) ; une pluralité d’organes d’étanchéité (60), chaque organe d’étanchéité (60) obturant de manière étanche un espace délimité circonférentiellement entre une première patte de liaison (50) et une deuxième patte de liaison (50) circonférentiellement consécutives. Figure de l’abrégé : Figure 4
FR2205720A 2022-06-14 2022-06-14 Ensemble pour turbomachine Active FR3136516B1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR2205720A FR3136516B1 (fr) 2022-06-14 2022-06-14 Ensemble pour turbomachine
PCT/FR2023/050806 WO2023242496A1 (fr) 2022-06-14 2023-06-07 Ensemble pour turbomachine
US18/869,147 US20250341192A1 (en) 2022-06-14 2023-06-07 Assembly for a turbine engine
EP23736415.3A EP4540514A1 (fr) 2022-06-14 2023-06-07 Ensemble pour turbomachine

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR2205720A FR3136516B1 (fr) 2022-06-14 2022-06-14 Ensemble pour turbomachine
FR2205720 2022-06-14

Publications (2)

Publication Number Publication Date
FR3136516A1 FR3136516A1 (fr) 2023-12-15
FR3136516B1 true FR3136516B1 (fr) 2024-08-02

Family

ID=83438692

Family Applications (1)

Application Number Title Priority Date Filing Date
FR2205720A Active FR3136516B1 (fr) 2022-06-14 2022-06-14 Ensemble pour turbomachine

Country Status (4)

Country Link
US (1) US20250341192A1 (fr)
EP (1) EP4540514A1 (fr)
FR (1) FR3136516B1 (fr)
WO (1) WO2023242496A1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3165041A1 (fr) 2024-07-24 2026-01-30 Safran Nacelles Ensemble pour turbomachine

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2855559B1 (fr) * 2003-05-27 2005-07-15 Snecma Moteurs Systeme d'etancheite du flux secondaire a l'entree d'une tuyere d'une turbomachine avec chambre de post-combustion
FR2914707B1 (fr) * 2007-04-05 2009-10-30 Snecma Propulsion Solide Sa Procede d'assemblage avec recouvrement de deux pieces ayant des coefficients de dilatation differents et assemblage ainsi obtenu
US8721278B2 (en) * 2010-08-02 2014-05-13 Siemens Energy, Inc. Exhaust manifold flange connection
US9784215B2 (en) * 2014-11-07 2017-10-10 Rohr, Inc. Exhaust nozzle center body attachment
FR3100575B1 (fr) * 2019-09-05 2022-04-08 Safran Ceram Cone d’ejection a fixation flexible aerodynamique
FR3114847B1 (fr) * 2020-10-07 2022-09-16 Safran Ceram Ensemble d’étanchéité pour un cône d’éjection de turbine
FR3115835B1 (fr) * 2020-10-30 2022-11-04 Safran Ceram Ensemble de turbine de turbomachine
FR3115832B1 (fr) * 2020-11-05 2023-04-21 Safran Nacelles Ensemble pour une turbomachine

Also Published As

Publication number Publication date
EP4540514A1 (fr) 2025-04-23
US20250341192A1 (en) 2025-11-06
FR3136516A1 (fr) 2023-12-15
WO2023242496A1 (fr) 2023-12-21

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