FR2986778B1 - Dispositif et procede d'assemblage d'un moteur d'aeronef a un mat d'aeronef - Google Patents

Dispositif et procede d'assemblage d'un moteur d'aeronef a un mat d'aeronef

Info

Publication number
FR2986778B1
FR2986778B1 FR1251337A FR1251337A FR2986778B1 FR 2986778 B1 FR2986778 B1 FR 2986778B1 FR 1251337 A FR1251337 A FR 1251337A FR 1251337 A FR1251337 A FR 1251337A FR 2986778 B1 FR2986778 B1 FR 2986778B1
Authority
FR
France
Prior art keywords
aircraft
mat
assembling
engine
aircraft engine
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
FR1251337A
Other languages
English (en)
Other versions
FR2986778A1 (fr
Inventor
Philippe Mereau
Mickael Matignon
Laurent Guillot
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.)
Airbus Operations SAS
Airbus SAS
Original Assignee
Airbus Operations SAS
Airbus 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 Airbus Operations SAS, Airbus SAS filed Critical Airbus Operations SAS
Priority to FR1251337A priority Critical patent/FR2986778B1/fr
Publication of FR2986778A1 publication Critical patent/FR2986778A1/fr
Application granted granted Critical
Publication of FR2986778B1 publication Critical patent/FR2986778B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B21/00—Means for preventing relative axial movement of a pin, spigot, shaft or the like and a member surrounding it; Stud-and-socket releasable fastenings
    • F16B21/10—Means for preventing relative axial movement of a pin, spigot, shaft or the like and a member surrounding it; Stud-and-socket releasable fastenings by separate parts
    • F16B21/12—Means for preventing relative axial movement of a pin, spigot, shaft or the like and a member surrounding it; Stud-and-socket releasable fastenings by separate parts with locking-pins or split-pins thrust into holes
    • 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
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • 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
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • B64D27/406—Suspension arrangements specially adapted for supporting thrust loads, e.g. thrust links
    • 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
    • Y02T50/40—Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Automatic Assembly (AREA)
FR1251337A 2012-02-13 2012-02-13 Dispositif et procede d'assemblage d'un moteur d'aeronef a un mat d'aeronef Active FR2986778B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1251337A FR2986778B1 (fr) 2012-02-13 2012-02-13 Dispositif et procede d'assemblage d'un moteur d'aeronef a un mat d'aeronef

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1251337A FR2986778B1 (fr) 2012-02-13 2012-02-13 Dispositif et procede d'assemblage d'un moteur d'aeronef a un mat d'aeronef

Publications (2)

Publication Number Publication Date
FR2986778A1 FR2986778A1 (fr) 2013-08-16
FR2986778B1 true FR2986778B1 (fr) 2015-02-06

Family

ID=46062508

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1251337A Active FR2986778B1 (fr) 2012-02-13 2012-02-13 Dispositif et procede d'assemblage d'un moteur d'aeronef a un mat d'aeronef

Country Status (1)

Country Link
FR (1) FR2986778B1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3096346B1 (fr) * 2019-05-23 2022-01-21 Airbus Operations Sas Aéronef comprenant deux attaches voilures avant comportant chacune au moins un élément de liaison vertical

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2638028A (en) * 1949-10-05 1953-05-12 Francis John Patsy Sleeve fastener
US6568894B2 (en) * 2000-10-04 2003-05-27 Golden Dove Marine Fastener devices, such as lock-pins
FR2887851B1 (fr) * 2005-06-29 2007-08-17 Airbus France Sas Mat d'accrochage de moteur pour aeronef
FR2901243B1 (fr) * 2006-05-16 2008-06-27 Airbus France Sas Dispositif d'accrochage d'un moteur d'aeronef
FR2916424B1 (fr) * 2007-05-23 2009-08-21 Airbus France Sa Mat d'accrochage de moteur pour aeronef comprenant une cale biaise pour la fixation de l'attache moteur avant

Also Published As

Publication number Publication date
FR2986778A1 (fr) 2013-08-16

Similar Documents

Publication Publication Date Title
FR2996635B1 (fr) Procede et dispositif d'affichage de parametres de vol sur un aeronef.
FR2978264B1 (fr) Un procede de rechargement automatique de logiciel et un dispositif de rechargement automatique de logiciel
FR2970552B1 (fr) Systeme et procede d'injection de combustible
FR2973946B1 (fr) Dispositif électronique a couches
FR2993418B1 (fr) Dispositif de charge d'un element portable et procede associe
FR3004546B1 (fr) Procede et dispositif de modification automatique d'un plan de vol lateral d'un aeronef.
FR2992292B1 (fr) Dispositif et procede d'assemblage d'une structure fixe d'inverseur de poussee d'un ensemble propulsif d'aeronef
FR2996257B1 (fr) Procede et un dispositif de determination du prelevement d'air sur un turboreacteur d'aeronef
FR2998268B1 (fr) Dispositif de stockage de carburant, aeronef et procede
FR2997731B1 (fr) Dispositif et procede d'alimentation d'un moteur-fusee
FR2970700B1 (fr) Dispositif d'accrochage d'un moteur d'aeronef a un mat
FR2991228B1 (fr) Procede et dispositif de realisation d'un panneau composite auto-raidi
FR3015329B1 (fr) Procede, dispositif et systeme d'assemblage d'une pluralite de panneaux
FR2950860B1 (fr) Dispositif d'accrochage d'un moteur a un mat d'aeronef
FR3000136B1 (fr) Procede de diagnostic d'un moteur suralimente et moteur associe
FR2986505B1 (fr) Procede d'optimisation de performances d'un aeronef, dispositif et aeronef
FR2996912B1 (fr) Dispositif et procede d'interaction a distance avec un systeme d'affichage
FR2996931B1 (fr) Procede et dispositif de gestion automatique du guidage d'un aeronef lors d'un arret complet des moteurs.
FR2970904B1 (fr) Dispositif d'assemblage d'un corps d'essieu et procede associe.
FR2986567B1 (fr) Procede de surveillance d'un moteur et dispositif
FR3010200B1 (fr) Procede et dispositif de normalisation de valeurs de parametres de fonctionnement d'un moteur d'aeronef
FR2980117B1 (fr) Engin volant a decollage et atterrissage vertical a rotor contrarotatif
FR2997778B1 (fr) Procede de construction d'un modele comportemental d'un moteur d'avion
FR2986278B1 (fr) Procede et dispositif de commande de la combustion d'un moteur a combustion interne a allumage commande
FR2973132B1 (fr) Dispositif et procede d'evaluation des capacites operationnelles d'un aeronef

Legal Events

Date Code Title Description
PLFP Fee payment

Year of fee payment: 5

PLFP Fee payment

Year of fee payment: 6

PLFP Fee payment

Year of fee payment: 7

PLFP Fee payment

Year of fee payment: 9

PLFP Fee payment

Year of fee payment: 10

PLFP Fee payment

Year of fee payment: 11

PLFP Fee payment

Year of fee payment: 12

PLFP Fee payment

Year of fee payment: 13