Aerial micromodule optical cable and a method of manufacturing said cable

Patent metadata

Field	Value
Publication number	US-10330879-B2
Application number	US-201515737471-A
Country	US
Kind code	B2
Filing date	Jun 26, 2015
Priority date	Jun 26, 2015
Publication date	Jun 25, 2019
Grant date	Jun 25, 2019

Abstract

A method of manufacturing an aerial micromodule cable with excess length of an optical core is disclosed, the cable comprising a cable jacket defining a cavity in which the optical core is arranged, said cable having two rigid strength members embedded in the wall of the jacket; the method comprising guiding the cable over a wheel; wherein a first plane (P1) intersecting the center of gravity (C1) of the cable cavity is parallel to a second plane (P2) intersecting the two rigid strength members, said first and second planes (P1, P2) being offset from each other, and wherein, during said guiding, the two rigid strength members are positioned closer to the wheel than the first plane (P1) so as to cause the optical core to have a core excess length of at least 0.05%.

First claim

The invention claimed is:

1. A method of manufacturing an aerial micromodule cable with excess length of an optical core, said cable comprising a cable jacket, an inner wall of said cable jacket defining a cable cavity in which the optical core is arranged, said cable having two rigid strength members embedded in the wall of said cable jacket;
said method comprises:
extruding said cable jacket around said optical core, to provide said cable, said optical core having no overlength relative to the cable jacket;
guiding the aerial micromodule cable over an outer circumference of a coupling wheel; said coupling wheel being the first wheel that receives the cable after said extruding; and
wherein, a first plane intersecting a center of gravity of the cable cavity is parallel to a second plane intersecting the two rigid strength members in the cable jacket, said first and second planes being offset from each other,
and wherein, during said guiding, the two rigid strength members are positioned closer to the outer circumference of the coupling wheel than the first plane so as to cause the optical core to have a core excess length of at least 0.05% relative to the length of the cable jacket.

2. The method according to claim 1 , wherein during said guiding, the coupling wheel rotates about a rotation axis parallel to said first plane and to said second plane.

3. The method according to claim 1 , wherein the first plane is a median transverse plane of the cable.

4. The method according to claim 1 , wherein the second plane is a median transverse plane of the cable.

5. The method according to claim 1 , wherein the first plane is a plane of symmetry of the cable cavity.

6. The method according to claim 1 , wherein the second plane divides the aerial micromodule cable into a first region and a second region, said first region comprising the first plane,
wherein, during said guiding, the center of gravity of the optical core is arranged in the first region such that the neutral axis of the cable is positioned between the center of gravity of the optical core and the second plane.

7. An aerial micromodule cable comprising:
a cable jacket comprising a wall defining a cable cavity;
an optical core comprising a layer of yarns or a tape, which is cabled around at least one micromodule
said optical core being arranged inside the cable cavity, said optical core being uncoupled from the cable jacket and only partially filling the cable cavity;
said cable having two rigid strength members embedded in the wall of said jacket; and
said cable having a first plane that intersects a center of gravity of the cable cavity and is parallel to a second plane intersecting the two rigid strength members in the cable jacket, said first plane and said second plane being offset from each other, wherein said optical core has an excess length of at least 0.05% relative to the length of the cable jacket.

8. The cable according to claim 7 , wherein a cross-section of the cable cavity is circular or ellipsoidal.

9. The cable according to claim 7 , wherein the optical core comprises at least one micromodule, each of said micromodule comprising 4 or 8 or 12 fibers.

10. The cable according to claim 7 , further comprising a visible indicator on the outer periphery of the cable that indicates a cable bend direction so that the optical core has excess length of at least 0.05%.

11. The cable according to claim 7 , wherein the first plane is a median transverse plane of the cable.

12. The cable according to claim 7 , wherein the second plane is a median transverse plane of the cable.

13. The cable according to claim 7 , wherein the first plane is a plane of symmetry of the cable cavity.

14. The cable according to claim 7 , wherein the second plane divides the aerial micromodule cable into a first region and a second region, said first region comprising the first plane,
wherein the center of gravity of the optical core is arranged in the first region such that the neutral axis of the cable is positioned between the center of gravity of the optical core and the second plane.

Assignees

• Draka Comteq Bv

Inventors

• Tatat Olivier
• Testu Jean-Marc

Classifications

• G02B6/4484

  with desired surplus length between fibres and protection features · CPC title

• G02B6/4432 Primary

  with fibre reinforcements · CPC title

• G02B6/4422

  of the overhead type · CPC title

• G02B6/4417

  High voltage aspects, e.g. in cladding · CPC title