Abstract: A glazed unit extending along a main surface and formed by a first material, includes a soundproofing zone that extends along a first length l along the main surface, the soundproofing zone having a first thickness h1 of the material, the first thickness h1 varying, as a function of a coordinate x, along the first length l in proportion to a value of xn, where n is a real number strictly greater than 1, from a minimum thickness h1min to a maximum thickness h1max, the first length l being predetermined such that the minimum thickness h1min is less than or equal to one third of the maximum thickness h1max.

Abstract: A device for soundproofing a plate, includes a soundproofing part and a mounting part, wherein the mounting part is to be mounted secured to a border of the plate, the mounting part being mounted secured to the soundproofing part and having a second thickness h2 in contact with the soundproofing part, and the soundproofing part is made of a first material, and extends along a first length l in a first main direction, the soundproofing part having a first thickness h1 of the first material in a direction perpendicular to the first main direction the first thickness h1 varying, based on an x coordinate, along the first length l, proportionally to a value of xn, wherein n is a real number strictly greater than 1, from a minimal thickness h1min until h2, the first length l being so that h1min, is less than or equal to one third of h2.

Abstract: A seal of a glazed element of an aircraft, the seal being configured to receive an edge of a first glazed unit, the first glazed unit having a first face, the seal including a first surface adapted to be mounted on the first face so as to receive the first glazed unit, wherein the seal includes a first damping part, the first damping part including the first surface, and wherein a first material forming the first damping part has a first loss factor ?1 strictly greater than 0.10.