Abstract: The invention concerns a disc (40) for a disc brake (30). According to the invention, the disc (40) is made of steel containing less than 0.3% by weight of Carbon.

Abstract: The invention relates to a brake pad or a disc brake caliper, comprising a support plate receiving a friction material. According to the invention, the support plate is made from low-alloy carbon steel containing less than 0.3% by weight of carbon and vanadium in an amount between 0.2 and 0.3% by weight.

Abstract: The invention concerns a brake pad (10) for a disc brake caliper, the pad (10) comprising a support plate (11). According to the invention, the support plate (11) has cooling fins (17), thus creating a convection zone (16).

Abstract: The invention relates to a brake pad for a disc brake caliper, comprising a support plate with a rear face presenting a support zone and a front face receiving a friction material with a friction zone intended to engage with a brake disc in a friction direction. According to the invention, the center of the support zone is offset relative to the center of the friction zone, in a direction opposite to the friction direction, by a value D, such that 0.1 ?E?D?2 ?E, where: ? is the friction coefficient of the friction zone against the disc; and E is the distance between the friction zone and the center of a mounting surface of the pad, measured orthogonally to the friction zone.

Abstract: A device for controlling the pressure of a tire of an aircraft wheel provided with a rim. The device includes a shell defining an open-ended housing; a system for controlling the pressure of a tire; and an annular band having a tensile strength of between 400 and 1500N. The system is received in the housing of the shell, and the annular band is positioned on a bearing face of the shell opposite the open-ended housing and against transverse retaining means. The device can be positioned around the rim to press the shell against the rim and close off the open-ended housing.

Abstract: The present invention concerns a landing gear (1) for a light aircraft, i.e. weighing less than 5.7 tonnes, the landing gear consisting of at least one wheel (3) attached to a chassis or to a fuselage of the aircraft by means of a connecting element (2). According to the invention, the wheel (3) is connected to the connecting element (2) via a system (4) of two damping cylinders arranged between the wheel (3) and the connecting element (2).

Abstract: The invention relates to a device for controlling the pressure of a tire of an aircraft wheel provided with a rim, remarkable in that it comprises: a shell defining an open-ended housing; a system for controlling the pressure of a tire; an annular band having a tensile strength of between 400 and 1500N; the pressure control system being received in the housing of the shell, and the annular band is positioned on a bearing face of the shell opposite the open-ended housing and against transverse retaining means, the device is able to be positioned around the rim to press the shell against the rim and close off the open-ended housing.

Abstract: The present invention concerns a landing gear (1) for a light aircraft, i.e. weighing less than 5.7 tonnes, the landing gear consisting of at least one wheel (3) attached to a chassis or to a fuselage of the aircraft by means of a connecting element (2). According to the invention, the wheel (3) is connected to the connecting element (2) via a system (4) of two damping cylinders arranged between the wheel (3) and the connecting element (2).

Abstract: A device for mounting an aircraft tail wheel includes a support plate having, on the one hand, an articulation shaft with an arm and, on the other hand, an articulation shaft with a fork receiving the freely rotating tail wheel, while the articulation shaft of the plate is positioned near a rotation shaft of the tail wheel.