초록 ▼

A device (22) fitted with ribs is placed on a cylindrical rod (20) so that it is fixed to it in bending. The device (22) is formed of at least three ribs connected to each other at their ends, and at least one pair of elements in the form of a star connecting the ribs together, at least close to its

A device (22) fitted with ribs is placed on a cylindrical rod (20) so that it is fixed to it in bending. The device (22) is formed of at least three ribs connected to each other at their ends, and at least one pair of elements in the form of a star connecting the ribs together, at least close to its central region. This device enables the rod (20) to apply an approximately radial force to the center of the rod through an actuator onto webs (24) bearing on its ends, minimizing the mass for a given spacing of the webs (24). The device is particularly applicable to the control of aircraft control surfaces.

대표청구항 ▼

1. Device for transmission of forces in approximately the radial direction from a longitudinal axis of the said device, between a central region and two end regions of the device, the said device being characterized in that it comprises at least three ribs distributed around the said longitudinal ax

1. Device for transmission of forces in approximately the radial direction from a longitudinal axis of the said device, between a central region and two end regions of the device, the said device being characterized in that it comprises at least three ribs distributed around the said longitudinal axis and connected to each other in the said end regions, and at least one pair of elements in the shape of a star connecting the ribs on each side of the said central region. 2. Force transmission device according to claim 1, in which the said device is made in a single part. 3. Force transmission device according to claim 1, in which the ribs are uniformly distributed around the said longitudinal axis. 4. Force transmission device according to claim 1, in which the said device is symmetric about a median plane perpendicular to the said longitudinal axis. 5. Force transmission device according to claim 1, in which all ribs are identical. 6. Force transmission device according to claim 1, in which the ribs are connected to each other in the said end regions by two first rings and each of the star shaped elements comprises a second ring at its center, the first and second rings along the said longitudinal axis. 7. Force transmission mechanism comprising a force transmission device according to claim 6 and a cylindrical rod acting as a pivot pin passing through the first and second rings so that it is fixed in bending to the force transmission device, the cylindrical rod acting in bearing for a first part between a pair of star shaped elements adjacent to the central region and a second part beyond the first rings. 8. Force transmission mechanism according to claim 7, in which the elements forming bearings are inserted between the cylindrical rod and each of the first and second rings. 9. Force transmission mechanism according to claim 7, in which the cylindrical rod passes through two approximately plane webs, that can be fixed to the second part, beyond the first rings, the two webs being designed to be fixed to the second part, the said webs forming a double eye plate articulated onto a single eye plate connected to the first part through the cylindrical rod, and forming two single eye plates articulated on two double eye plates linked to a fixed external structure through a second cylindrical rod acting as a pivot pin centered on an axis of rotation of the second part with respect to the fixed structure, this axis of rotation being parallel to the said longitudinal axis. 10. Mechanism according to claim 7, in which the first part is a rod of an actuator with linear control supported by the fixed structure and the second part is an aircraft control surface.