OVERBRAIDED NON-METALLIC TENSION MEMBERS
20180155870 ยท 2018-06-07
Inventors
- Scott Alan Eastman (Glastonbury, CT, US)
- Daniel A. Mosher (Glastonbury, CT, US)
- Wenping Zhao (Glastonbury, CT, US)
Cpc classification
D07B1/22
TEXTILES; PAPER
D07B2801/10
TEXTILES; PAPER
B66B7/068
PERFORMING OPERATIONS; TRANSPORTING
D07B2801/10
TEXTILES; PAPER
D07B1/162
TEXTILES; PAPER
International classification
D07B1/16
TEXTILES; PAPER
D07B1/06
TEXTILES; PAPER
Abstract
A tension member for a lifting and/or hoisting system includes a core including a plurality of load carrying fibers arranged in a matrix material, and an outer layer secured to the core including a plurality of outer fibers arranged around a perimeter of the core. The outer layer includes one or more outer fibers arranged off-axis relative to the load carrying fibers of the core. A method of forming a tension member for an elevator system includes arranging a plurality of load carrying fibers along a length of the tension member, retaining the plurality of load carrying fibers in a matrix material to define a core, and enclosing the core in an outer layer including a plurality of outer fibers arranged around a perimeter of the core. The outer layer includes one or more outer fibers arranged off-axis relative to the load carrying fibers of the core.
Claims
1. A tension member for a lifting and/or hoisting system comprising: a core including a plurality of load carrying fibers arranged in a matrix material; and an outer layer secured to the core including a plurality of outer fibers arranged around a perimeter of the core, the outer layer including one or more outer fibers arranged off-axis relative to the load carrying fibers of the core.
2. The tension member of claim 1, wherein the outer layer includes a plurality of outer fibers braided to form the outer layer.
3. The tension member of claim 1, wherein the plurality of load carrying fibers comprise one or more of carbon, glass, aramid, nylon, and polymer fibers.
4. The tension member of claim 1, wherein the matrix material is one or more of polyurethane, vinylester or epoxy.
5. The tension member of claim 1, wherein the plurality of outer fibers are formed from the same material as the plurality of load carrying fibers.
6. The tension member of claim 1, wherein the core is formed by a pultrusion process.
7. The tension member of claim 1, wherein the plurality of load carrying fibers extend along an axial length of the tension member.
8. A belt for suspending and/or driving an elevator car, comprising: a plurality of tension members extending along a length of the belt, each tension member including: a core including a plurality of load carrying fibers arranged in a matrix material; and an outer layer secured to the core including a plurality of outer fibers arranged around a perimeter of the core, the outer layer including one or more outer fibers arranged off-axis relative to the load carrying fibers of the core; and a jacket at least partially encapsulating the plurality of tension members to retain the plurality of tension members.
9. The belt of claim 8, wherein the plurality of tension members are arranged along a lateral width of the belt.
10. The belt of claim 8, wherein the outer layer includes a plurality of outer fibers braided to form the outer layer.
11. The belt of claim 8, wherein the plurality of load carrying fibers comprise one or more of carbon, glass, aramid, nylon, and polymer fibers.
12. The belt of claim 8, wherein the plurality of outer fibers are formed from the same material as the plurality of load carrying fibers.
13. A method of forming a tension member for an elevator system comprising: arranging a plurality of load carrying fibers along a length of the tension member; retaining the plurality of load carrying fibers in a matrix material to define a core; and enclosing the core in an outer layer including a plurality of outer fibers arranged around a perimeter of the core, the outer layer including one or more outer fibers arranged off-axis relative to the load carrying fibers of the core.
14. The method of claim 13, wherein enclosing the core in an outer layer includes braiding the plurality of outer fibers around the core.
15. The method of claim 13, further comprising impregnating the outer layer with an outer matrix material.
16. The method of claim 13, further comprising forming the tension member via a continuous manufacturing process.
17. The method of claim 16, further comprising cutting the tension member to a selected length.
18. The method of claim 13, wherein the plurality of outer fibers are formed from the same material as the plurality of load carrying fibers.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0024] The subject matter is particularly pointed out and distinctly claimed at the conclusion of the specification. The foregoing and other features, and advantages of the present disclosure are apparent from the following detailed description taken in conjunction with the accompanying drawings in which:
[0025]
[0026]
[0027]
[0028]
[0029]
[0030] The detailed description explains disclosed embodiments, together with advantages and features, by way of example with reference to the drawings.
DETAILED DESCRIPTION
[0031] Shown in
[0032] The sheaves 18 each have a diameter 20, which may be the same or different than the diameters of the other sheaves 18 in the elevator system 10. At least one of the sheaves could be a traction sheave 52. The traction sheave 52 is driven by a machine 50. Movement of drive sheave by the machine 50 drives, moves and/or propels (through traction) the one or more tension members 16 that are routed around the traction sheave 52. At least one of the sheaves 18 could be a diverter, deflector or idler sheave. Diverter, deflector or idler sheaves are not driven by a machine 50, but help guide the one or more tension members 16 around the various components of the elevator system 10.
[0033] In some embodiments, the elevator system 10 could use two or more tension members 16 for suspending and/or driving the elevator car 12. In addition, the elevator system 10 could have various configurations such that either both sides of the one or more tension members 16 engage the one or more sheaves 18 or only one side of the one or more tension members 16 engages the one or more sheaves 18. The embodiment of
[0034] Referring now to
[0035] Exemplary load carrying fibers 26 used to form the core 24 include, but are not limited to, carbon, glass, aramid, nylon, and polymer fibers, for example. Each of the load carrying fibers 26 within the core 24 may be substantially identical or may vary. In addition, the matrix material 28 may be formed from any suitable material, such as polyurethane, vinylester, and epoxy for example. The materials of the load carrying fibers 26 and the matrix material 28 are selected to achieve a desired stiffness and strength of the tension member 16.
[0036] The core 24 may be formed as thin layers, in some embodiments by a pultrusion process. In a standard pultrusion process, the load carrying fibers 26 are impregnated with the matrix material 28 and are pulled through a heated die and additional curing heaters where the matrix material 28 undergoes cross linking. A person having ordinary skill in the art will understand that controlled movement and support of the pulled load carrying fibers 26 may be used to form a desired linear or curved profile of the untensioned core 24. In an exemplary embodiment, the core 24 has a cross-sectional thickness of about 0.5 millimeters to about 4 millimeters. In another embodiment, the core 24 has a cross-sectional thickness of 1 millimeter. Further, in some embodiments the core 24 has a circular cross-section, while in other embodiments the core 24 may have other cross-sectional shapes, such as rectangular or oval.
[0037] The tension member 16 further includes an outer layer 30 formed from braided or woven fibers that substantially envelops the core 24. The outer layer 30 may be applied to the core 24 by, for example wrapping around the core 24 or braiding around the core 24. The outer layer 30 is formed from fibers of, for example, carbon, glass, aramid, nylon, or polymer fibers. In some embodiments, the outer layer 30 material is the same as the core 24 material, while in other embodiments the materials may differ. Further, in other embodiments the outer layer 30 is formed from metallic wires. The braiding of the outer layer 30 orients fibers off-axis relative to the core 24 to support off-axis stresses on the tension member 16. Further, the outer layer 30 can have lower stiffness which reduces bending stresses and allows the overall tension member 16 to have a larger thickness or diameter than just an aligned fiber tension member. While in the embodiment of
[0038] Referring now to
[0039] Referring now to
[0040] The tension members 16 are at least partially enclosed in the jacket 36, to restrain movement of the tension members 16 in the belt 34 and protect the tension members 16. In embodiments including the jacket 36 defines a traction surface 38 configured to contact a corresponding surface of the traction sheave 52. Exemplary materials for the jacket 36 include the elastomers of thermoplastic and thermosetting polyurethanes, polyamide, thermoplastic polyester elastomers, and rubber, for example. Other materials may be used to form the jacket 36 if they are adequate to meet the required functions of the belt 34. For example, a primary function of the jacket 36 is to provide a sufficient coefficient of friction between the belt 34 and the traction sheave 52 to produce a desired amount of traction therebetween. The jacket 36 should also transmit the traction loads to the tension members 16. In addition, the jacket 36 should be wear resistant and protect the tension members 16 from impact damage, exposure to environmental factors, such as chemicals, for example. One or more additive materials may be incorporated into the jacket 36 to enhance performance such as traction and environmental resistance. In embodiments with the jacket 36, the outer layer 30 with the off-axis fibers promotes improved adhesion between the tension members 16 and the jacket 36.
[0041] Referring now to
[0042] While the present disclosure has been described in detail in connection with only a limited number of embodiments, it should be readily understood that the present disclosure is not limited to such disclosed embodiments. Rather, the present disclosure can be modified to incorporate any number of variations, alterations, substitutions or equivalent arrangements not heretofore described, but which are commensurate in spirit and/or scope. Additionally, while various embodiments have been described, it is to be understood that aspects of the present disclosure may include only some of the described embodiments. Accordingly, the present disclosure is not to be seen as limited by the foregoing description, but is only limited by the scope of the appended claims.