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US3607490A Expired / Lapsed US ⏱️ 0.0 years remaining

Method of making a flexible signal transmission cable for an aerodynamic body

Assignee: Airbus Defence and Space GmbH
•
Filing: 1970-03-19
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Granted: 1971-09-21
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Expires: 1990-03-19
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Abstract

Abstract A flexible electrical cable for transmitting control signals between a control station and a rapidly moving aerodynamic body includes at least two parallel enamel-insulated conductor wires cemented together in parallel relation and extending centrally through a tension member formed by a large number of thin individual filaments, and further includes a covering closely embracing the wires and the tension member and comprising superposed layers wound around the tension member in opposite respective angular directions. The conductor wires are high purity electrolytic copper having an elongation equal to or greater than 24 percent and, in the bare condition, a diameter of 0.07 mm. The tension member comprises a plurality of parallel filament strands, of 14 Mu diameter, or a polyester fiber having an elongation of substantially 7 percent to 8 percent. The covering layers comprise natural silk having a composition of 4 X 13/15 den. In producing the cable, the conductor wires, which are separately insulated in an enameling operation, are cemented together in parallel relation. The tension member filament strands are presorted and fed to a spinning device along with the parallel conductor wires. The tension member is covered, in two successive spinning operations, having the same spinning angle but different directions of rotation. The conductor wires are fed to the spinning device under a braking force of 40 g. The apparatus includes two serially arranged wire spinning devices, the first of which has a fixed spindle provided with an axially bore therethrough and a guide plate arranged close to the spinning head. The guide plate has a central opening for the conductor wires and plural openings for the tension member filament strands, these openings being arranged in a circle concentric with the central opening and at angular interval of 120*.

Inventors

  • 👤 Werner Heinzmann
  • 👤 Siegfried Pfahl

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-29 03:18
CPC Classifications
H; H01; H01B; H01B13/00; H01B13/02; G; G02; G02B; G02B6/00; G02B6/44; G02B6/4439; G02B6/4457; H01B7/00; H01B7/04; H01B7/043

Claims Analysis

Total Claims: 5
Claim 1
Independent Claim 60 words
A method, as claimed in claim 1, including the step of presorting the joined conductor wires and the carrier filament strands; feeding the wires and the strands in a controlled manner to a spinning device; and covering the bundle comprising the wires and the strands in two successive spinning operations having the same spinning angle but different directions of rotation.
Claim 2
Dependent Claim 78 words
A method, as claimed in claim 1, including the step of subdividing the carrier filament bundle forming the tension member, and prior to the spinning operation, into at least three individual carrier filament strands; feeding the subdivided carrier filament strands, prior to the first spinning operation into symmetrically embracing relation with the centrally located conductor wires; and maintaining the carrier filament strands angularly offset from each other by 120*around a small diameter circle centered on the conductive wires.
Claim 3
Dependent Claim 19 words
A method, as claimed in claim 3, including the step of feeding the carrier filament strands in ribbon form.
Claim 4
Dependent Claim 27 words
A method, as claimed in claim 3, in which the carrier filament strands and the conductor wires are fed perpendicularly at least during the first spinning operation.
Claim 5
Dependent Claim 28 words
A method, as claimed in claim 5, including the step of applying, to the conductor wires, a braking force of 40 g. during feeding of the conductor wires.

References Cited (Backward Citations)

No citation records indexed.

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1974-09-20 1975-03-22 1975-09-21 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1978-09-20 1979-03-22 1979-09-21 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1982-09-20 1983-03-22 1983-09-21 $7700.00 Window Closed / Lapsed

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