| 摘要 |
FIELD: engines and pumps.SUBSTANCE: invention relates to an element of an electrical connection of a turbo-machine such as an aircraft or propeller-turbine engine, as well as to an aircraft engine containing such an element. The element of electrical connection (10) of the turbo-machine, which includes wires (12) connected to connector (18) by means of tubular connection part (20) enveloping the end of the wires; insert (26) for protection of wires (12) against abrasion is installed in tubular connection part (20) and the insert mainly includes central tubular housing (27) containing wires and provided at least on some part of its length with a series of gaskets (38) supported from inner surface (28) of the tubular connection part of the connection element so that the central housing can be retained at some distance from the same inner surface.EFFECT: invention provides protection of wires against abrasion and as a result against power supply failure.10 cl, 6 dwg |
