A wire harness includes: a flexible conductor; a flexible restricting member extending along the conductor and restricting a path of the conductor; a flexible armoring member through which the conductor and the restricting member are inserted; a first holding member including a first recessed part and fixed to the vehicle body, the first recessed part having a first end of the restricting member inserted therein; and a second holding member including a second recessed part and fixed to the movable body, the second recessed part having a second end of the restricting member inserted therein. Respective ends of the armoring member are fixed to the first holding member and the second holding member. The respective ends of the restricting member are held by the first recessed part and the second recessed part.

A cable assembly is used to connect elements of a computing system. The cable assembly may include a first cable and a connector. The first cable includes an external portion having a first conductor, an electromagnetic (EMC) shielding jacket for the first conductor and a connector disposed at an end of the first conductor. Further, the first cable includes an internal portion comprising a second conductor and a connector disposed on an end of the second conductor. However, the internal portion lacks an EMC shielding jacket for the second conductor. The external portion of the first cable and the internal portion of the first cable form a continuous cable. The connector device comprises a shield area configured to electrically couple with a chassis of a node of a computer system and a retainer configured to physically couple the cable assembly with the chassis. The connector is configured to electrically couple the external portion of the first cable with the chassis, and wherein the external portion of the first cable meets the internal portion of the first cable at the connector device.

A wire harness includes: a flexible conductor; a flexible restricting member extending along the conductor and restricting a path of the conductor; a flexible armoring member through which the conductor and the restricting member are inserted; a first holding member including a first recessed part and fixed to the vehicle body, the first recessed part having a first end of the restricting member inserted therein; and a second holding member including a second recessed part and fixed to the movable body, the second recessed part having a second end of the restricting member inserted therein. Respective ends of the armoring member are fixed to the first holding member and the second holding member. The respective ends of the restricting member are held by the first recessed part and the second recessed part.

A grommet may include a hollow body part configured to be penetrated by a wire, a first mounting part formed at one end of the body part, a second mounting part formed at the other end of the body part, a deformable part configured to connect the first mounting part and the second mounting part and configured to allow deformation of the body part, and at least one length adjustment part formed on the body part and configured to allow a change in length of the body part.

A grommet may include a hollow body part configured to be penetrated by a wire, a first mounting part formed at one end of the body part, a second mounting part formed at the other end of the body part, a deformable part configured to connect the first mounting part and the second mounting part and configured to allow deformation of the body part, and at least one length adjustment part formed on the body part and configured to allow a change in length of the body part.

A wing assembly for an aircraft, the wing assembly having a fixed wing and a wing tip device moveably mounted at the end of the fixed wing. A wiring harness extends between the fixed wing and the wing tip device, a length of the wiring harness being encased in a length of protective sleeve. The protective sleeve is pre-shaped, for example pre-molded, to follow a path along a helical curve.

A wing assembly for an aircraft, the wing assembly having a fixed wing and a wing tip device moveably mounted at the end of the fixed wing. A wiring harness extends between the fixed wing and the wing tip device, a length of the wiring harness being encased in a length of protective sleeve. The protective sleeve is pre-shaped, for example pre-molded, to follow a path along a helical curve.