Method and apparatus for breaking ice accretions on an aerial cable

• US 6,518,497 B1
• Filed: 06/07/2002
• Issued: 02/11/2003
• Est. Priority Date: 06/07/2002
• Status: Expired due to Fees

• Current Assignee: Jean-Louis Laforte, Marc-André Allaire
• Original Assignee: Jean-Louis Laforte, Marc-André Allaire
• Inventors: LaForte, Jean-Louis, Allaire, Marc-André
• Primary Examiner(s): Reichard, Dean A.
• Assistant Examiner(s): Nino, Adolfo
• Application Number:
  US10/165,408
• Time in Patent Office: 249 Days
• Field of Search: 174/40.R, 174/40.TD, 174/45.TD, 307/147
• US Class Current: 174/40.00R
• CPC Class Codes: H02G 7/16 Devices for removing snow or ice from lines or cables

Abstract

A method and an apparatus for de-icing aerial cables are provided. The cable is gripped and slowly twisted for a predetermined number of turns within the elastic domain of deformation of the cable. Mechanical elastic energy is therefore accumulated in the cable. The cable is then released and untwisted under the spring back effect, releasing the energy accumulated therein which breaks and shakes off the ice accumulated on the cable.

Claims

1. A method for breaking ice accretions formed on an aerial cable, said aerial cable having a longitudinal axis, a rigidly fixed first end and a second end opposed thereto, the method comprising the steps of:

a) gripping a portion of the aerial cable proximate to the second end thereof;

b) rotating the portion of the aerial cable around the longitudinal axis to twist said aerial cable for a predetermined number of turns, thereby accumulating elastic energy therein; and

c) releasing the portion of the aerial cable, thereby liberating the accumulated elastic energy therein, instantly untwisting said cable and breaking the ice accretions formed thereon.

2. The method according to claim 1, comprising the additional step of repeating steps a) to c) until said aerial cable is free of ice accretions.

3. The method according to claim 1, wherein the predetermined number of turn step b) is between 100 and 200 turns.

4. The method according to claim 1, wherein steps a) to c) are remotely triggered.

5. The method according to claim 1, wherein the aerial cable has an elastic domain of deformation, the predetermined number of turns being selected to maintain the aerial cable within said elastic domain.

6. The method according to claim 1, wherein step b) comprises twisting said aerial cable at a rotation speed between 1 and 10 rpm.

7. The method according to claim 1, wherein the aerial cable has a plurality of strands forming a whorl, the rotating of step b) being done in a direction of said whorl.

8. The method according to claim 1, wherein the aerial cable has a plurality of strands forming a whorl, the rotating of step b) being done against a direction of said whorl.

9. An apparatus for breaking ice accretions formed on an aerial cable, said aerial cable having a longitudinal axis, a rigidly fixed first end and a second end opposed thereto, the apparatus comprising:

gripping means for gripping a portion of the aerial cable proximate the second end thereof;

a motorised rotating assembly engageable with said gripping means for rotating the portion of the aerial cable around the longitudinal axis to twist said aerial cable, thereby accumulating elastic energy therein; and

a release mechanism for releasing the portion of the aerial cable, thereby liberating the accumulated elastic energy therein, instantly untwisting said cable and breaking the ice accretions formed thereon.

10. The apparatus according to claim 9, wherein the gripping means comprise a metallic sleeve cold pressed on the portion of the cable.

11. The apparatus according to claim 9, wherein the motorised rotating assembly comprises an electric motor having a rotatable motor shaft, said electric motor being mounted on a rigid structure proximate to the portion of the aerial cable.

12. The apparatus according to claim 11, wherein said motorised rotating assembly further comprises an output shaft and a gear train coupling said output shaft to the motor shaft.

13. The apparatus according to claim 12, wherein said output shaft extends along the longitudinal axis of the aerial cable proximate to the second end thereto.

14. The apparatus according to claim 13, wherein the release mechanism comprises a magnetic clutch coupled to the output shaft of the motorised rotating assembly.

15. The apparatus according to claim 14, wherein said magnetic clutch comprises:

an electromagnet coaxially mounted on the output shaft of the motorised rotating assembly;

a conducting ring extending around the electromagnet and being separated therefrom by an air gap, the conducting ring between rigidly fixed to the gripping means; and

current supplying means for supplying current to the electromagnet.

16. The apparatus according to claim 14, further comprising a control unit connected to the electric motor and the magnetic clutch for controlling therethrough the twisting and untwisting of the aerial cable.

17. The apparatus according to claim 16, further comprising a power supply powering the electric motor, magnetic clutch and control unit.

18. The apparatus according to claim 16, further comprising a torque sensor coupled to the portion of the aerial cable for measuring a torque applied thereon by said motorised rotating assembly, the torque sensor being connected to the control unit.

19. The apparatus according to claim 16, further comprising an ice detector for detecting the ice accretions formed on said aerial cable, said ice detector being connected to the control unit.