Method and an arrangement in condition monitoring of an elevator rope
US-2015362450-A1 · Dec 17, 2015 · US
USRE47035E · US · E1
| Field | Value |
|---|---|
| Publication number | US-RE47035-E |
| Application number | US-80549004-A |
| Country | US |
| Kind code | E1 |
| Filing date | Mar 19, 2004 |
| Priority date | Dec 31, 1998 |
| Publication date | Sep 11, 2018 |
| Grant date | Sep 11, 2018 |
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A tension member termination device optimized for terminating flat tension members having compressible outer coatings, the device including a wedge and a socket each having cooperating surfaces positioned at a predetermined angle for clamping the tension member therebetween. The angle reliably secures the tension member while avoiding deleterious pressure and stress upon the tension member. The invention also provides a safety clamp for optional use with the tension member termination device.
Opening claim text (preview).
What is claimed is: 1. A termination device for a tension member, the tension member having a width W and an elastomer coating that has a maximum compressive stress capability σ c , the tension member being subjected to a tensile force T, the termination device comprising: a socket; and a wedge that fits within the socket with the tension member wrapped around the wedge, the wedge having a clamping surface that includes a length L and is disposed at an angle ϕ, which is measured from a centerline of the wedge to the clamping surface and which relates to the length L in accordance with the formula defining a minimum of the angle ϕ: ϕ≥tan −1 ϕ=tan −1 (T/(σ c *L*W)). 2. A method for terminating a tension member having a width W and an elastomer coating that has a maximum compressive stress capability σ c , comprising: feeding the tension member into an aperture of a socket; wrapping the tension member around a wedge having a clamping surface that includes a length L and is disposed at an angle ϕ, which is measured from a centerline of the wedge to the clamping surface; feeding the tension member back through the aperture; and applying a tensile force T in the tension member so that the tension member is compressed between the wedge and the socket, wherein the tensile force T is applied in accordance with the formula defining a minimum of the angle ϕ: ϕ≥tan −1 ϕ=tan −1 (T/(σ c *L*W)). 3. A method according to claim 2 further comprising: positioning the tension member in a back-to-back arrangement; placing a pair of plates on either side of the tension member; inserting a plurality of fasteners through the plates; tightening the fasteners; and clamping the tension member between the plates in a double overlap arrangement. 4. A termination device for a tension member, the tension member having a width W and a compressible coating that has a predetermined maximum compressive stress capability σ c , the compressible coating being subject to compressive creep, the tension member being subjected to a tensile force T, the termination device comprising: a socket; and a wedge that fits within the socket with the tension member wrapped around the wedge, the wedge having a clamping surface that includes a length L and is disposed at an angle ϕ, which is measured from a centerline of the wedge to the clamping surface and which relates to the length L in accordance with the formula defining a minimum of the angle ϕ: ϕ=tan −1 (T/(σ c *L*W)). 5. A method for terminating a tension member having a width W and a compressible coating that has a predetermined maximum compressive stress capability σ c , the compressible coating being subject to compressive creep, the method comprising: feeding the tension member into an aperture of a socket; wrapping the tension member around a wedge having a clamping surface that includes a length L and is disposed at an angle ϕ, which is measured between a centerline of the wedge and the clamping surface; feeding the tension member back through the aperture; and applying a tensile force T in the tension member so that the tension member is compressed between the wedge and the socket, wherein the tensile force T is applied in accordance with the formula defining a minimum of the angle ϕ: ϕ=tan −1 (T/(σ c *L*W)). 6. A termination device for a tension member, the tension member having a width W and comprised of a plurality of inner load carrying cords and a compressible coating, wherein the compressible coating defines a traction surface for the tension member and the compressible coating has a predetermined maximum compressive stress capability σ c , the compressible coating being subject to compressive creep if the maximum compressive stress capability is exceeded, the tension member being subjected to a tensile force T, the termination device comprising: a socket; and a wedge that fits within the socket with the tension member wrapped around the wedge, the wedge having a clamping surface that includes a length L and is disposed at an angle ϕ, which is measured between a centerline of the wedge and the clamping surface and which relates to the length L in accordance with the formula that defines a minimum of the angle ϕ: ϕ=tan −1 (T/(σ c *L*W)). 7. A method for terminating a tension member having a width W and comprised of a plurality of inner load carrying cords and a compressible coating, wherein the compressible coating defines a traction surface for the tension member and has a predetermined maximum compressive stress capability σ c , the compressible coating being subject to compressive creep if the predetermined maximum compressive stress capability is exceeded, the method comprising: feeding the tension member into an aperture of a socket; wrapping the tension member around a wedge having a clamping surface that includes a length L and is disposed at an angle ϕ, which is measured between a centerline of the wedge and the clamping surface; feeding the tension member back through the aperture; and applying a tensile force T in the tension member so that the tension member is compressed between the wedge and the socket, wherein the tensile force T is applied in accordance with the formula that defines a minimum of the angle ϕ: ϕ=tan −1 (T/(σ c *L*W)).
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