Patent ID: 7628087

Claim:
A high speed, high load, aerospace linear screw actuator including, an outer housing which is fixed in use, an electric motor within the housing, the motor including a hollow rotatable output shaft, a rotatable but axially fixed nut driven by said output shaft, an elongated hollow axially translatable output member, said output member extending within said output shaft of said motor and cooperating with said rotatable nut, and, an elongate anchor member secured against rotation relative to said housing and extending within said output member, said anchor member cooperating with said output member to hold said output member against rotation whereby rotation of said nut relative to said output member causes axial translation of said output member relative to the housing, wherein said elongate anchor member includes an axially extending region of non-circular cross-section having first and second pairs of axially extending flat surfaces with which said output member cooperates throughout its range of axial movement to resist rotation of the output member, the output member cooperating with the flat surfaces through an intermediary of respective pairs of cylindrical rollers rotatably mounted on the output member for rotation about axes transverse to the length of movement of the output member, each pair of cylindrical rollers formed integrally with and carried on a common roller shaft, the shafts defining the axes of rotation of the respective pairs of cylindrical rollers, said rollers engaging said flat surfaces with full, straight line contact, respectively, and being mounted for rotation by bearings, the first and second pairs of flat surfaces being spaced on opposite sides of the axis of the output member, the flat surfaces of each pair being arranged with their planes parallel and spaced apart on opposite sides of the said axis.