Cable tensiometer for aircraft

• US 7,424,832 B1
• Filed: 09/04/2007
• Issued: 09/16/2008
• Est. Priority Date: 09/04/2007
• Status: Expired due to Fees

• Current Assignee: The Government Of The United States Of America, As Represented By The Secretary Of The Navy
• Original Assignee: United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration
• Inventors: Nunnelee, Mark
• Primary Examiner(s): THOMPSON, JEWEL VERGIE
• Application Number:
  US11/849,843
• Time in Patent Office: 378 Days
• Field of Search: 738/31, 738/624.6, 738/624.72
• US Class Current: 73/862.472
• CPC Class Codes: G01L 5/102 using sensors located at a non-interrupted part of the flexible member
• CPC Class Codes: G01L 5/107 for measuring a reaction force applied on an element disposed between two supports, e.g. on a plurality of rollers or gliders

Abstract

The invention is a cable tensiometer that can be used on aircraft for real-time, in-flight cable tension measurements. The invention can be used on any aircraft cables with high precision. The invention is extremely light-weight, hangs on the cable being tested and uses a dual bending beam design with a high mill-volt output to determine tension.

Claims

1. A cable tension measuring device, comprising:

a beam structure comprising first, second, and third extensions, the second extension located between and equidistant from the first and third extensions;

two pulleys, each rotatably attached to the first and third extensions, having an inner surface to accept a cable;

two openings on the first and third extensions, located below the pulleys to allow insertion of the cable on a bottom side of the inner surface and rotation of the pulleys;

a slot, located at a top of the second extension, comprising a width sufficient to accept the cable;

a guard, fastened to the top of the second extension, over the slot, to hold the cable in place within the slot;

an angle formed between the cable and a line parallel to the beam structure, extending between the bottom sides of the pulleys, when the cable is inserted on the inner surface on the bottom side of the pulleys and in the slot; and

,

at least two gages located on the beam structure capable of determining beam structure bending between the first and second extensions and between the second and third extensions.

2. The cable tension measuring device of claim 1, wherein the first and third extensions comprise equal heights and the second extension comprises a height less than the height of the first and third extensions.

3. The cable tension measuring device of claim 2, wherein the angle comprises between 2 degrees and 8 degrees.

4. The cable tension measuring device of claim 3, wherein the angle comprises about 5 degrees.

5. The cable tension measuring device of claim 2, wherein the height of the first and third extensions comprises between 1.5 inches and 8 inches.

6. The cable tension measuring device of claim 5, wherein the height of the second extension comprises between 0.8 inches and 5 inches.

7. The cable tension measuring device of claim 2, wherein the pulleys comprise a stainless steel inner surface and stainless steel ball bearings.

8. The cable tension measuring device of claim 2, wherein the slot and pulleys can accept cable having a width up to 0.5 inches.

9. The cable tension measuring device of claim 2, wherein the gages comprises strain gages.

10. The cable tension measuring device of claim 9, further comprising at least two strain gages each between the first and second extensions and the between the second and third extensions.

11. The cable tension measuring device of claim 10 wherein the at least four strain gages comprise a full bridge strain gage.

12. The cable tension measuring device of claim 1, wherein the beam structure and the extensions comprise an aluminum material.

13. The cable tension measuring device of claim 1, further comprising at least one hole through the first, second, and third extensions.

14. A method for determining the tension on a fixed cable, comprising the steps of:

providing a device comprising a beam structure comprising first, second, and third extensions, the second extension located between and equidistant from the first and third extensions, two pulleys, each rotatably attached to the first and third extensions, having an inner surface to accept a cable, two openings on the first and third extensions, located below the pulleys to allow insertion of the cable on a bottom side of the inner surface and rotation of the pulleys, a slot, located at a top of the second extension, comprising a width sufficient to accept the cable, an angle formed between the cable and a line parallel to the beam structure when the cable is inserted on the inner surface on the bottom side of the pulleys and in the second extension slot, and, at least two gages located on the beam structure capable of determining beam structure bending between the first and second extensions and between the second and third extensions;

inserting the cable on the inner surface and bottom of the pulleys and into the second extension slot;

fastening a guard over the slot to hold the cable in place; and

,

monitoring the gauges to determine bending of the beam structure.