Patent ID: 7805949

Claim:
A device for supporting and housing auxiliaries in a bypass turbojet, comprising: a first coaxial case ring and a second coaxial case ring, the first coaxial case ring is arranged inside the second coaxial case ring; and tubular radial arms which connect the first coaxial case ring and the second coaxial case ring, through which tubular radial arms fluid ducts and electric cables pass, a first tubular radial arm and a second tubular radial arm extending substantially in a vertical plane, the first radial arm being disposed above the second radial arm, wherein a lateral face of the first radial arm comprises a first detachable panel whose removal allows access to turbojet equipment situated radially inside the first case ring in alignment with the radial arm, the first detachable panel includes a radial portion fastened to the first radial arm and a cylindrical portion connected to the first case ring, and wherein a first portion of a fluid duct extends substantially radially inside the first radial arm and a second portion of the fluid duct extends substantially circumferentially inside the first case ring, a circumferential dimension of the second portion of the fluid duct is smaller than a circumferential dimension of the cylindrical portion of the first detachable panel.