Patent ID: 11897595
Assignee: AIRBUS CANADA LIMITED PARTNERSHIP
Field: Transport (Mechanical engineering)
Classification: CPC B  F  H | IPC B  F  H

Claim 0:
1. A line or harness fastening system for an aircraft, comprising:
a clamp for attaching the line or harness to the aircraft;
a bobbin within the clamp and surrounding the line or harness, the bobbin comprising two separate complementary parts that fit together around the line or harness,
wherein the bobbin is smaller than the clamp and is circular in shape to enable rotation of the bobbin within the clamp,
wherein each of the two separate complementary parts of the bobbin include a pair of diametrically opposite tabs formed along an outer circumference of each of the two separate complementary parts, and
wherein each of the tabs of one of the complementary parts fits into a corresponding recess on the other of the complementary parts.