The invention relates to a flywheel for stabilising the position of a spacecraft, comprising a hub means (1) for fastening the flywheel, a flywheel ring (4), which externally surrounds the hub means (1) circumferentially at a distance, a support means (3) for supporting the flywheel ring (4) on the hub means (1), and a vibration damping device (6, 8) having a tuned mass damper means (8) which is axially movable back and forth relative to the flywheel ring with respect to a rotation axis of the flywheel.

A vibration damper that damp vibrations transmitted between a drive unit and a support body. The vibration damper comprises: an elastic member interposed between the drive unit and the support body; a rotor supported by the drive unit or the support body; and a vibration translating mechanism that rotates the rotor and reciprocates the rotor between the drive unit and the support body, in response to the vibrations acting in a vibrating direction to isolate the drive unit and the support body away from each other and bring the drive unit and the support body closer together.

A segmented driveshaft for transmission of torque and thrust loads from one member to another along an eccentric axis of rotation. The segmented driveshaft includes a plurality of pivotally interconnected vertebrae that is distributed along a connecting rod that is pivotally connected to a drivetrain assembly. The each vertebra has male and female interlocks that are pivotally mated with the male and female interlocks of an adjacent vertebra. Interposed between the adjacent vertebrae are independent male and female pivots that pivotally engage with each another. The pivotally mated interlocks of adjacent vertebrae and the pivotally engaged pivots allow the driveshaft to extend between connecting points of a drivetrain assembly that have offset axes of rotation.

A flywheel apparatus includes a damper, and a mass ring including a first surface facing a first side in an axial direction, a second surface facing a second side and a first circumferential surface facing an inner side in a radial direction. The apparatus includes a drive plate including a first wall portion including a third surface being in contact with the second surface, and a plurality of protruding portions, each of the plurality of protruding portions including an end surface configured to fit to the first circumferential surface. The drive plate is configured such that the mass ring is concentrically attachable to the drive plate by the fitting of the end surfaces and the first circumferential surface to each other.

The invention relates to a flywheel for stabilising the position of a spacecraft, comprising a hub means (1) for fastening the flywheel, a flywheel ring (4), which externally surrounds the hub means (1) circumferentially at a distance, a support means (3) for supporting the flywheel ring (4) on the hub means (1), and a vibration damping device (6, 8) having a tuned mass damper means (8) which is axially movable back and forth relative to the flywheel ring with respect to a rotation axis of the flywheel.

A vibration damper that damp vibrations transmitted between a drive unit and a support body. The vibration damper comprises: an elastic member interposed between the drive unit and the support body; a rotor supported by the drive unit or the support body; and a vibration translating mechanism that rotates the rotor and reciprocates the rotor between the drive unit and the support body, in response to the vibrations acting in a vibrating direction to isolate the drive unit and the support body away from each other and bring the drive unit and the support body closer together.

A flywheel apparatus includes a damper, and a mass ring including a first surface facing a first side in an axial direction, a second surface facing a second side and a first circumferential surface facing an inner side in a radial direction. The apparatus includes a drive plate including a first wall portion including a third surface being in contact with the second surface, and a plurality of protruding portions, each of the plurality of protruding portions including an end surface configured to fit to the first circumferential surface. The drive plate is configured such that the mass ring is concentrically attachable to the drive plate by the fitting of the end surfaces and the first circumferential surface to each other.

A segmented driveshaft for transmission of torque and thrust loads from one member to another along an eccentric axis of rotation. The segmented driveshaft includes a plurality of pivotally interconnected vertebrae that is distributed along a connecting rod that is pivotally connected to a drivetrain assembly. The each vertebra has male and female interlocks that are pivotally mated with the male and female interlocks of an adjacent vertebra. Interposed between the adjacent vertebrae are independent male and female pivots that pivotally engage with each another. The pivotally mated interlocks of adjacent vertebrae and the pivotally engaged pivots allow the driveshaft to extend between connecting points of a drivetrain assembly that have offset axes of rotation.