Methods and apparatuses for indicating and/or adjusting tension in pliant tension members, including aircraft recovery lines
First Claim
1. A tool for indicating tension in a flexible line, the tool comprising:
- a first support member releasable coupled to the flexible line suspended from a support structure, the first support member being positioned generally parallel to the flexible line, wherein the first support member comprises an elongated bar having a first contact member releasably coupled to a first portion of the flexible line and a second contact member releasably coupled to a second portion of the flexible line below the first portion of the flexible line; and
a second support member integral with the first support member and fixed at an acute angle relative to the first support member, the second support member having a center of gravity at a selected distance from the flexible line, wherein the second support member is generally horizontal when the tension in the flexible line is at a desired value.
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Accused Products
Abstract
Methods and apparatuses for measuring and adjusting tension in pliant tension members, including aircraft recovery lines. A tool for indicating tension in a pliant tension member in accordance with one embodiment of the invention, for example, can include a first support member releasably coupled to a flexible line suspended from a support structure. The first support member is positioned generally parallel to the flexible line. The tool can also include a second support member coupled to the first support member and positioned at an acute angle relative to the first support member. The second support member has a center of gravity at a selected distance from the flexible line. The second support member is generally horizontal when the tension in the flexible line is at a desired value.
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Citations
30 Claims
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1. A tool for indicating tension in a flexible line, the tool comprising:
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a first support member releasable coupled to the flexible line suspended from a support structure, the first support member being positioned generally parallel to the flexible line, wherein the first support member comprises an elongated bar having a first contact member releasably coupled to a first portion of the flexible line and a second contact member releasably coupled to a second portion of the flexible line below the first portion of the flexible line; and a second support member integral with the first support member and fixed at an acute angle relative to the first support member, the second support member having a center of gravity at a selected distance from the flexible line, wherein the second support member is generally horizontal when the tension in the flexible line is at a desired value. - View Dependent Claims (2, 3, 4, 5, 6, 7)
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8. An aircraft handling system, comprising:
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a support structure; a flexible recovery line suspended from the support structure in a generally downward direction and having an intercept portion positioned to intercept an unmanned aircraft in flight; and a tension indicating apparatus releasably carried by the recovery line and positioned to indicate the tension in the recovery line, the tension indication apparatus including— a first generally rigid bar releasably coupled to the recovery line and positioned generally parallel to the recovery line, wherein the first bar includes a first attachment device releasable coupled to a first portion of the recovery line and a second attachment device releasable coupled to a second portion of the recovery line below the first portion of the recovery line; and a second generally rigid bar integral with the first bar and fixed at an acute angle relative to the first bar, the second bar having a center of gravity at a selected distance from the recovery line, wherein the second bar is generally horizontal when the tension in the recovery line is at a desired value. - View Dependent Claims (9, 10, 11, 12, 13, 14, 15)
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16. A tool for indicating tension in a flexible recovery line suspended in a generally downward direction from an extendable boom, the recovery line having an intercept portion positioned to intercept an unmanned aircraft in flight, the tool comprising:
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a first generally rigid portion integral with a second generally rigid portion, wherein the second portion is fixed at an acute angle relative to the first portion, and wherein the first and second portions comprise elongated bars; a first engagement member and a second engagement member carried by the elongated bar of the first portion, the first engagement member being releasably coupled to a first portion of the recovery line and the second engagement member being releasably coupled to a second portion of the recovery line, wherein the second portion of the recovery line is lower than the first portion of the recovery line, and wherein the first portion is generally parallel with the recovery line after installation; and a weight having a known value carried by the second portion and spaced apart from the recovery line by a selected distance such that, when the tension in the recovery line is at a desired value, the second portion is generally horizontal. - View Dependent Claims (17)
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18. A method for indicating tension in a flexible line, the method comprising:
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releasably attaching a first support member of a tension indication tool to a flexible line suspended in a generally downward direction from a support structure with the first support member positioned generally parallel to the flexible line, the first support member including an elongated bar having a first contact member releasably coupled to a first portion of the flexible line and a second contact member releasably coupled to a second portion of the flexible line below the first portion of the flexible line, and wherein the tool includes a second support member integral with the first support member and fixed at an acute angle relative to the first support member, the second support member having a center of gravity at a selected distance from the flexible line; and adjusting the tension in the flexible line until the second support member is generally horizontal. - View Dependent Claims (19, 20, 21, 22, 23, 24)
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25. A method for handling an unmanned aircraft, comprising:
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deploying a flexible recovery line from an extendable boom, the recovery line being suspended from the boom in a generally downward direction and having an intercept portion positioned to intercept an unmanned aircraft in flight; applying tension to the recovery line; releasably attaching a first elongated bar of a tension indication tool to the recovery line with the first bar positioned generally parallel to the recovery line, the first bar including a first engagement member releasably coupled to a first portion of the recovery line and a second engagement member releasably coupled to a second portion of the recovery line below the first portion of the recovery line, and wherein the tool includes a second elongated bar integral with the first bar and fixed at an acute angle relative to the first bar, the second bar having a center of gravity at a selected distance from the recovery line; and adjusting the tension in the recovery line until the second bar is generally horizontal. - View Dependent Claims (26, 27, 28, 29, 30)
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Specification