FR2953810B1 - Nacelle de turboreacteur - Google Patents

Nacelle de turboreacteur

Info

Publication number
FR2953810B1
FR2953810B1 FR0959061A FR0959061A FR2953810B1 FR 2953810 B1 FR2953810 B1 FR 2953810B1 FR 0959061 A FR0959061 A FR 0959061A FR 0959061 A FR0959061 A FR 0959061A FR 2953810 B1 FR2953810 B1 FR 2953810B1
Authority
FR
France
Prior art keywords
turboreactor
nacelle
turboreactor nacelle
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
FR0959061A
Other languages
English (en)
Other versions
FR2953810A1 (fr
Inventor
Jacky Raphael Michel Derenes
Lambert Delphine Edith Dijoud
Christophe Claude Philippe Nouhaud
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
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 SNECMA SAS filed Critical SNECMA SAS
Priority to FR0959061A priority Critical patent/FR2953810B1/fr
Priority to US12/967,849 priority patent/US8585352B2/en
Publication of FR2953810A1 publication Critical patent/FR2953810A1/fr
Application granted granted Critical
Publication of FR2953810B1 publication Critical patent/FR2953810B1/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
    • B64D29/08—Inspection panels for power plants

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR0959061A 2009-12-16 2009-12-16 Nacelle de turboreacteur Active FR2953810B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR0959061A FR2953810B1 (fr) 2009-12-16 2009-12-16 Nacelle de turboreacteur
US12/967,849 US8585352B2 (en) 2009-12-16 2010-12-14 Turbojet nacelle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0959061A FR2953810B1 (fr) 2009-12-16 2009-12-16 Nacelle de turboreacteur

Publications (2)

Publication Number Publication Date
FR2953810A1 FR2953810A1 (fr) 2011-06-17
FR2953810B1 true FR2953810B1 (fr) 2012-01-13

Family

ID=42342452

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0959061A Active FR2953810B1 (fr) 2009-12-16 2009-12-16 Nacelle de turboreacteur

Country Status (2)

Country Link
US (1) US8585352B2 (fr)
FR (1) FR2953810B1 (fr)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9759095B2 (en) 2013-03-07 2017-09-12 Rolls-Royce Corporation Gas turbine engine access panel
FR3010049B1 (fr) 2013-09-04 2017-03-31 Snecma Structure de liaison moteur-nacelle a secteurs de virole pivotants
GB201704841D0 (en) * 2017-03-27 2017-05-10 Rolls Royce Plc Gas Turbine Engine
FR3064601B1 (fr) * 2017-03-30 2021-01-01 Safran Nacelles Nacelle pour turboreacteur reliee au fuselage d'un aeronef, et ensemble propulsif
US11142326B2 (en) * 2018-07-27 2021-10-12 The Boeing Company Mechanism for indicating position of a latch mechanism for an aircraft nacelle
EP4141315A1 (fr) * 2021-08-23 2023-03-01 GRZ Technologies SA Système de stockage-compression d'hydrogène

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4825648A (en) * 1987-03-02 1989-05-02 General Electric Company Turbofan engine having a split cowl
GB2266080A (en) * 1992-04-16 1993-10-20 Rolls Royce Plc Mounting arrangement for a gas turbine engine.
FR2905975B1 (fr) * 2006-09-20 2008-12-05 Snecma Sa Conduite de soufflante pour une turbomachine.
US20080258016A1 (en) * 2007-04-23 2008-10-23 Gukeisen Robert L Nacelle assembly without lower bi-fi splitter
US9126691B2 (en) * 2007-05-30 2015-09-08 United Technologies Corporation Access door for gas turbine engine components

Also Published As

Publication number Publication date
US20110142608A1 (en) 2011-06-16
FR2953810A1 (fr) 2011-06-17
US8585352B2 (en) 2013-11-19

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