| 摘要 |
A support attachment for aircraft structural stringers is comprised of an elongated body having a first side for being extended transversely across a stringer secured to an aircraft bulkhead. The body has a second side opposite the first side, and available from the second side, there is a device for securing wire supports or other types of supports to the support attachment body. The body is constructed and arranged so that any materials such as cables supported thereby are supported from a centrally located position on the body with respect to the elongated direction and thereby centrally positioned transversely with respect to the stringer. There are slots through each end of the body transverse to the elongated direction thereof, the slots extending through the body from the first side to the second side. Straps slidable in the slots are adapted to be connected to the respective ends of the stringer. There are latching pawls on the second side of the body adjacent each of the respective slots and there are ratchets on the straps for engaging the pawls to lock the straps in the slots when the straps are connected to the stringer and pulled tightly through the slots away from the stringer.
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