Tension member for elevator system

Abstract

A load bearing member is provided including at least one load bearing segment having a plurality of load carrying fibers arranged within a matrix material. At least a portion of the load bearing member has a radius of curvature when the load bearing member is untensioned.

Claims

1. A load bearing member, comprising: at least one load bearing segment including a plurality of load carrying fibers arranged within a matrix material, wherein at least a portion of the load bearing member has a radius of curvature when the load bearing member is untensioned, and wherein an untensioned length of the plurality of load carrying fibers arranged within the portion of the load bearing member having a radius of curvature that varies.

2. The load bearing member according to claim 1, wherein the plurality of load carrying fibers have a unidirectional orientation.

3. The load bearing member according to claim 1, wherein the plurality of load carrying fibers are substantially identical.

4. The load bearing member according to claim 1, wherein the plurality of load carrying fibers arranged at an outer portion of the radius of curvature have a longer untensioned length than a plurality of load bearing fibers arranged adjacent to an inside of the radius of curvature.

5. The load bearing member according to claim 1, wherein the at least one load bearing segment is formed as a pultrusion.

6. The load bearing member according to claim 1, wherein the load bearing member includes a plurality of load bearing segments spaced apart from one another by a distance.

7. The load bearing member according to claim 6, wherein each of the plurality of load bearing segments is substantially identical.

8. The load bearing member according to claim 1, wherein a coating layer surrounds at least a portion of the at least one load bearing segment and defines an engagement surface of the load bearing member.

9. An elevator system, comprising: a hoistway; a drive machine mounted within the hoistway, the drive machine having a traction sheave coupled thereto an elevator car movable within the hoistway; a counterweight movable within the hoistway; at least one load bearing member connecting the elevator car and the counterweight, the load bearing member being arranged in contact with the traction sheave such that operation of the drive machine moves the elevator car between a plurality of landings, the at least one load bearing member including: at least one load bearing segment including a plurality of load carrying fibers arranged within a matrix material, wherein at least a portion of the load bearing member has a radius of curvature when the load bearing member is untensioned and wherein an untensioned length of the plurality of load carrying fibers arranged within the portion of the load bearing member having a radius of curvature that varies.

10. The elevator system according to claim 9, wherein the traction sheave has a diameter between about 150 and 300 times a thickness of the load bearing member.

11. The elevator system according to claim 9, wherein the plurality of load carrying fibers have a unidirectional orientation.

12. The elevator system according to claim 9, wherein the plurality of load carrying fibers arranged adjacent an inner bend radius have a first untensioned length and the plurality of load carrying fibers arranged adjacent an outer bend radius have a second untensioned length, the first untensioned length being shorter than the second untensioned length.

13. The elevator system according to claim 9, wherein the at least one load bearing segment is formed as a pultrusion.

14. The elevator system according to claim 9, wherein the load bearing member includes a plurality of load bearing segments spaced apart from one another by a distance.

15. The elevator system according to claim 14, wherein each of the plurality of load bearing segments is substantially identical.

16. The elevator system according to claim 9, wherein the load bearing member includes a coating layer surrounding a portion of the at least one load bearing segment, the coating layer defining an engagement surface configured to contact the traction sheave.

17. The elevator system according to claim 9, wherein the curvature of the load bearing member when untensioned has a diameter between about 1.5 to about 2.5 time a diameter of the traction sheave.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) The subject matter, which is regarded as the invention, is particularly pointed out and distinctly claimed in the claims at the conclusion of the specification. The foregoing and other features, and advantages of the invention are apparent from the following detailed description taken in conjunction with the accompanying drawings in which:

(2) FIG. 1 is a perspective view of an example of a traction elevator system;

(3) FIG. 2 is a cross-sectional view of a load bearing member that would be included in a load bearing belt according to an embodiment of the invention;

(4) FIG. 3 is a cross-sectional view of a load bearing belt having a plurality of load bearing segments interconnected by a coating layer according to an embodiment of the invention; and

(5) FIG. 4a is a side view of a conventional load bearing member in an untensioned and tensioned configuration; and

(6) FIG. 4b is a side view of a load bearing member according to an embodiment of the invention in an untensioned and tensioned configuration; and

(7) FIG. 5 is a cross-sectional view of a load bearing member that would be included in a load bearing belt according to an embodiment of the invention.

(8) The detailed description explains embodiments of the invention, together with advantages and features, by way of example with reference to the drawings.

DETAILED DESCRIPTION OF THE INVENTION

(9) Referring now to FIG. 1, an example of elevator system 10 according to an embodiment of the invention is illustrated. The elevator system 10 includes an elevator car 14 configured to move vertically upwardly and downwardly within a hoistway 12 along a plurality of car guide rails (not shown). Guide assemblies mounted to the top and bottom of the elevator car 14 are configured to engage the car guide rails to maintain proper alignment of the elevator car 14 as it moves within the hoistway 12.

(10) The elevator system 10 also includes a counterweight 16 configured to move vertically upwardly and downwardly within the hoistway 12. The counterweight 16 moves in a direction generally opposite the movement of the elevator car 14 as is known in conventional elevator systems. Movement of the counterweight 16 is guided by counterweight guide rails (not shown) mounted within the hoistway 12. In the illustrated, non-limiting embodiment, at least one load bearing member 30 coupled to both the elevator car 14 and the counterweight 16 cooperates with a traction sheave 18 mounted to a drive machine 20. To cooperate with the traction sheave 18, at least one load bearing member 30 bends in a first direction about the traction sheave 18. In one embodiment, any additional bends formed in the at least one load bearing member 18 must also be in the same first direction.

(11) The drive machine 20 of the elevator system 10 is positioned and supported at a mounting location atop a support member 22, such as a bedplate for example, in a portion of the hoistway 12 or a machine room. Although the elevator system 10 illustrated and described herein has a 1:1 roping configuration, elevator systems 10 having other roping configurations and hoistway layouts are within the scope of the invention. In embodiments having alternative roping configurations, a twist may be arranged in the load bearing members 30, as known in the art, to avoid reverse bends or other arrangements where all bending of the load bearing members 30 occurs in the same direction.

(12) Referring now to FIGS. 2-3, a cross-section of an example of a load bearing member 30 according to an embodiment of the invention is illustrated in more detail. In the illustrated, non-limiting embodiment of FIG. 2, the load bearing member 30 includes a single tension member or load bearing segment 32 having a plurality of individual load carrying fibers 34 arranged unidirectionally within a rigid matrix material 36. The load bearing segment 32 may have a cross-section of any shape. As shown in the illustrated, non-limiting embodiment, the load carrying fibers 34 within the load bearing segment 32 are randomly distributed throughout the matrix material 36; however, a density of the load carrying fibers 34 across the area of the load bearing segment 32 remains nominally uniform. In other embodiments, however, the density of the fibers 34 may be non-uniform such that the load bearing segment 32 may have other desired properties.

(13) Exemplary load bearing fibers 34 used to form a load bearing segment 32 include, but are not limited to, carbon, glass, aramid, nylon, and polymer fibers for example. Each of the fibers 34 within a single load bearing segment 32 may be substantially identical or may vary. In addition, the matrix material 36 may be formed from any suitable material, such as polyurethane, vinylester, and epoxy for example. The materials of the fibers 34 and matrix material 36 are selected to achieve a desired stiffness and strength of the load bearing member 30.

(14) In another embodiment, the load bearing member 30 may include a plurality of load bearing segments 32. The segments 32 are generally the same length and may have substantially identical configurations, or may vary in one or more of size, shape, material, etc. As shown in FIG. 3, the plurality of load bearing segments 32 may be generally separated from one another by a distance. In the illustrated, non-limiting embodiment, the plurality of load bearing segments 32 are encased with a jacket or coating layer 38 to restrain movement of the load bearing segments 32 relative to one another and protect the load bearing segments 32 from impact. However, it should be understood that any load bearing member 30 may include a coating layer 38 including embodiments having only a single load bearing segment 32.

(15) In embodiments including a coating layer 38, the coating layer 38 defines an engagement surface configured to contact a corresponding surface of the traction sheave 18. Suggested materials for the coating layer 38 include the elastomers of thermoplastic and thermosetting polyurethanes, polyaramid, and rubber for example. Other materials may be used to form the coating layer 38 if they are adequate to meet the required functions of the load bearing member 30. For example, a primary function of the coating layer 38 is to provide a sufficient coefficient of friction between the load bearing member 30 and the traction sheave 18 to produce a desired amount of traction there between. The coating layer 38 should also transmit the traction loads to at least one load bearing segments 32. In addition, the coating layer 38 should be wear resistant and protect the one or more segments 32 from impact damage, exposure to environmental factors, such as chemicals for example, or more importantly, may provide a means for making the load bearing member 30 flame retardant.

(16) As previously described, the load bearing member 30 is configured to wrap at least partially around the traction sheave 18. In one embodiment, the traction sheave 18 has a diameter between 150 and 300 times the thickness of the load bearing member 30. With reference now to FIG. 4b, the load bearing member 30 is formed to include a radius of curvature when untensioned. The curvature of the load bearing member 30 when untensioned may have a diameter between about 1.5 to about 2.5 times the diameter of the traction sheave 18. As is clearly illustrated in FIGS. 4a and 4b, the distance that a load bearing member 30 having a radius of curvature must bend around a sheave 18 when tension is applied thereto is significantly less than the distance that a conventional linear load bearing member 30 must bend around a sheave 18 when tension is applied thereto. As a result, the bending stress experienced by a load bearing member 30 having a radius of curvature is significantly reduced, thereby improving the load bearing capacity and life of the load bearing member 30.

(17) In other embodiments, only a portion of the load bearing member 30, such as the drive portion configured to contact the traction sheave 18 for example, includes a radius of curvature when the load bearing member 30 is untensioned. As a result of forming the load bearing member 30 with a radius of curvature, the circumferential length of the load carrying fibers 34 may vary. For example, with reference to FIG. 5, the load carry fibers arranged on the outside of the curvature generally have a first unstressed length, and the length load carrying fibers 34 arranged adjacent the inside of the curvature would have a second unstressed length, shorter than the first unstressed length. By having the length of the fibers 34 generally decrease from the outside to the inside of the curvature, internal stresses of the load carrying member 30 may be eliminated.

(18) The one or more load bearing segments 32 of the load bearing member 30 may be fabricated by a pultrusion process. In a standard pultrusion process, the fibers are impregnated with a matrix material and are pulled through a heated die and additional curing heaters where the matrix undergoes cross linking. A person having ordinary skill in the art will understand that controlled movement and support of the pulled fibers may be used to form a desired linear or curved profile of the untensioned load bearing member 30.

(19) By forming the composite load bearing member 30 with an initial curvature, the bending stress of the load bearing member is reduced for a given thickness. Consequently, the thickness of the load bearing member 30 may be increased, thereby increasing the load carrying capability per unit width, before reaching a maximum allowable bending stress. In addition, during the packaging and shipment of a load bearing member 30 formed with an initial curvature, the stored energy of the coiled load bearing member 30 is lowered, thereby reducing the requirements of the shipping containers.

(20) While the invention has been described in detail in connection with only a limited number of embodiments, it should be readily understood that the invention is not limited to such disclosed embodiments. Rather, the invention can be modified to incorporate any number of variations, alterations, substitutions or equivalent arrangements not heretofore described, but which are commensurate with the spirit and scope of the invention. Additionally, while various embodiments of the invention have been described, it is to be understood that aspects of the invention may include only some of the described embodiments. Accordingly, the invention is not to be seen as limited by the foregoing description, but is only limited by the scope of the appended claims.