(19)
(11)EP 1 780 125 A3

(12)EUROPEAN PATENT APPLICATION

(88)Date of publication A3:
16.01.2008 Bulletin 2008/03

(43)Date of publication A2:
02.05.2007 Bulletin 2007/18

(21)Application number: 06380215.1

(22)Date of filing:  27.07.2006
(51)International Patent Classification (IPC): 
B64D 41/00(2006.01)
B64D 27/26(2006.01)
(84)Designated Contracting States:
AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC NL PL PT RO SE SI SK TR
Designated Extension States:
AL BA HR MK YU

(30)Priority: 28.10.2005 ES 200502626

(71)Applicant: Airbus España, S.L.
28906 Getafe (Madrid) (ES)

(72)Inventors:
  • Martinez Rueda, José Román
    28300 Aranjuez (Madrid) (ES)
  • Rojo Carrión, José Alberto
    28007 Madrid (ES)
  • Sen Pacios, José Luis
    28943 Fuenlabrada (Madrid) (ES)
  • Melian Brinquis, Juan Pablo
    28007 Madrid (ES)
  • Rojo Saiz, Nicolás
    28032 Madrid (ES)
  • Martín Calvo, David
    28012 Madrid (ES)
  • Thomas, Steffan Prys
    28032 Madrid (ES)
  • Márquez Gavilán, Antonio
    28905 Getafe (Madrid) (ES)
  • García Patino, Maria Aranzazu
    28025 Madrid (ES)

(74)Representative: Ungria Lopez, Javier et al
Avda. Ramon y Cajal, 78
28043 Madrid
28043 Madrid (ES)

  


(54)Support system for auxiliary power unit


(57) Support system for auxiliary power unit which sustains an auxiliary power unit (1) of an aircraft to a fixed structure (2) belonging to a compartment of the auxiliary power unit (6) of said aircraft, made in a high mechanical strength material, and with high resistance to ignition, which comprises at least three fittings (3, 4, 5) of a substantially cylindrical shape, said fittings (3, 4, 5) being able to be hollow, and each one of them presenting a first end (7) comprising means of attachment of the support system (8) to the fixed structure (2) and a second end (9) comprising means of securing of the support system (8) which are joined to the auxiliary power unit (1) in the periphery of the extension of said auxiliary power unit (1), with at least a first forward fitting (4) and a second forward fitting (5) being located in the forward part of the auxiliary power unit (1), and at least one rear fitting (3) being located in the rear part of the auxiliary power unit (1).







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