FR3010052B1 - Bras de servitude d’une nacelle de turboreacteur a double flux, comportant deux parties - Google Patents

Bras de servitude d’une nacelle de turboreacteur a double flux, comportant deux parties

Info

Publication number
FR3010052B1
FR3010052B1 FR1358281A FR1358281A FR3010052B1 FR 3010052 B1 FR3010052 B1 FR 3010052B1 FR 1358281 A FR1358281 A FR 1358281A FR 1358281 A FR1358281 A FR 1358281A FR 3010052 B1 FR3010052 B1 FR 3010052B1
Authority
FR
France
Prior art keywords
turboboreacteur
servotude
nacelle
arm
parts
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
FR1358281A
Other languages
English (en)
Other versions
FR3010052A1 (fr
Inventor
Loic Chapelain
Jean-Francois Locufier
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
Application filed by Aircelle SA filed Critical Aircelle SA
Priority to FR1358281A priority Critical patent/FR3010052B1/fr
Priority to PCT/FR2014/052143 priority patent/WO2015028756A1/fr
Publication of FR3010052A1 publication Critical patent/FR3010052A1/fr
Application granted granted Critical
Publication of FR3010052B1 publication Critical patent/FR3010052B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00—Power-plant nacelles, fairings, or cowlings
    • B64D29/06—Attaching of nacelles, fairings or cowlings
    • 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
    • F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
    • F01D25/162—Bearing supports
    • 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
    • F01D9/00—Stators
    • F01D9/06—Fluid supply conduits to nozzles or the like
    • F01D9/065—Fluid supply or removal conduits traversing the working fluid flow, e.g. for lubrication-, cooling-, or sealing fluids
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B64D2045/009—Fire detection or protection; Erosion protection, e.g. from airborne particles

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR1358281A 2013-08-29 2013-08-29 Bras de servitude d’une nacelle de turboreacteur a double flux, comportant deux parties Active FR3010052B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1358281A FR3010052B1 (fr) 2013-08-29 2013-08-29 Bras de servitude d’une nacelle de turboreacteur a double flux, comportant deux parties
PCT/FR2014/052143 WO2015028756A1 (fr) 2013-08-29 2014-08-29 Bras de servitude d'une nacelle de turboréacteur à double flux, comportant deux parties

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1358281A FR3010052B1 (fr) 2013-08-29 2013-08-29 Bras de servitude d’une nacelle de turboreacteur a double flux, comportant deux parties

Publications (2)

Publication Number Publication Date
FR3010052A1 FR3010052A1 (fr) 2015-03-06
FR3010052B1 true FR3010052B1 (fr) 2015-09-25

Family

ID=49753326

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1358281A Active FR3010052B1 (fr) 2013-08-29 2013-08-29 Bras de servitude d’une nacelle de turboreacteur a double flux, comportant deux parties

Country Status (2)

Country Link
FR (1) FR3010052B1 (fr)
WO (1) WO2015028756A1 (fr)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102016215030A1 (de) 2016-08-11 2018-02-15 Rolls-Royce Deutschland Ltd & Co Kg Turbofan-Triebwerk mit einer im Sekundärstromkanal liegenden und ein separates Abschlusselement aufweisenden Verkleidung
FR3076860B1 (fr) 2018-01-12 2020-11-13 Safran Aircraft Engines Bras de passage de servitudes pour turbomachine
GB201820505D0 (en) * 2018-12-17 2019-01-30 Rolls Royce Connector system
FR3096743B1 (fr) 2019-05-28 2021-05-07 Safran Aircraft Engines Paroi coupe-feu et procédé d’ouverture de celle-ci

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5887822A (en) * 1997-03-28 1999-03-30 The Boeing Company Segmented engine flow control device
WO2008045093A1 (fr) * 2006-10-12 2008-04-17 United Technologies Corporation Bifurcation de moteur à turbine à gaz dans une tuyère à zone variable de soufflante
GB2497934B (en) * 2011-12-22 2014-06-04 Rolls Royce Plc Aeroengine arrangement

Also Published As

Publication number Publication date
WO2015028756A1 (fr) 2015-03-05
FR3010052A1 (fr) 2015-03-06

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Effective date: 20180125

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