Abstract: The invention relates to a mounting (1) for holding an elongate object (13) such as an electric cable in position relative to a structure (12). According to the invention, said mounting comprises: two parts for connecting the mounting to the structure (2, 3, 21, 22) each of which has a bearing surface (2a, 3a, 21a, 22a) suitable for resting each side of the structure against a bearing surface (12a, 12b) of the structure, said two connecting parts being assembled together by a clamping means (7, 8, 10), at least one supporting part (4, 23, 24) suitable for maintaining said elongate object (13) via a holding means (50, 31, 37, 69), characterized in that said mounting part is provided in the form of a substantially cylindrical railing (23, 24), secured to a connecting part.

Abstract: An insulation blanket to be connected at the inside surface (16) of an aircraft fuselage, includes at least one opening that allows a through element (20) to pass, at which is connected a sealing device, characterized in that this sealing device includes a core (28) that is combined with a body (30) that extends over a closed contour delimiting the opening (26), with the core (28) having a spring action that tends to flatten the body (30) against the through element (20) over at least a part of the circumference of the opening (26).

Abstract: The invention relates to a mounting (1) for holding an elongate object (13) such as an electric cable in position relative to a structure (12). According to the invention, said mounting comprises: two parts for connecting the mounting to the structure (2, 3, 21, 22) each of which has a bearing surface (2a, 3a, 21a, 22a) suitable for resting each side of the structure against a bearing surface (12a, 12b) of the structure, said two connecting parts being assembled together by a clamping means (7, 8, 10), at least one supporting part (4, 23, 24) suitable for maintaining said elongate object (13) via a holding means (50, 31, 37, 69), characterised in that said mounting part is provided in the form of a substantially cylindrical railing (23, 24), secured to a connecting part.

Abstract: An insulation blanket to be connected at the inside surface (16) of an aircraft fuselage, includes at least one opening that allows a through element (20) to pass, at which is connected a sealing device, characterized in that this sealing device includes a core (28) that is combined with a body (30) that extends over a closed contour delimiting the opening (26), with the core (28) having a spring action that tends to flatten the body (30) against the through element (20) over at least a part of the circumference of the opening (26).