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Electrical cable with a bend retaining jacket capable of conforming to a substantial installation curve

  • US 5,619,015 A
  • Filed: 07/21/1995
  • Issued: 04/08/1997
  • Est. Priority Date: 07/21/1994
  • Status: Expired due to Term
First Claim
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1. An electrical cable for installation in an aircraft, comprising one or more electrical conductors (8), a connector (29) electrically connected to said conductors (8), a protective hose system (5, 6, 6A) enclosing said conductors (8), a bend maintaining jacket (25A) surrounding said protective hose system (5, 6, 6A) along at least part of said electrical cable, a support body (31) and at least one clamping device (11) cooperating in securing said protective hose system (5, 6, 6A) and said bend maintaining jacket (25A) to said connector (29), said support body (31) having a large diameter section (31A), a small diameter section (31B) and a shoulder (31C) interconnecting said large and small diameter sections (31A, 31B), said protective hose system comprising an electrical conducting hose (5) made of a metal-webbing having an end surrounding said small diameter section (31B) and an electrical insulating hose (6) made of a synthetic material webbing, said bend maintaining jacket (25A) having a first end formed as an end bushing (27) coaxially surrounding said insulating hose (6), said at least one clamping device (11) securing ends of said hoses (5, 6) and said end bushing (27) to said small diameter section (31B), whereby said jacket (25A) maintains any bend in said at least part of said electrical cable.

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