Embodiments disclosed herein relate to elevator systems, and more particularly to load bearing members to suspend and/or drive elevator cars of an elevator system.
Elevator systems are useful for carrying passengers, cargo, or both, between various levels in a building. Some elevators are traction based and utilize load bearing members such as belts for supporting the elevator car and achieving the desired movement and positioning of the elevator car.
Where a belt is used as a load bearing member, a plurality of tension elements, or cords, are embedded in a common jacket. The jacket retains the cords in desired positions and provide a frictional load path. In an exemplary traction elevator system, a machine drives a traction sheave with which the belts interact to drive the elevator car along a hoistway. Belts typically utilize tension members formed from steel elements, but alternatively may utilize tension members formed from synthetic fibers or other materials, such as carbon fiber composites.
In one embodiment, a belt for an elevator system includes a plurality of tension members arranged along a belt width and extending longitudinally along a length of the belt, a jacket material at least partially encapsulating the plurality of tension members, and a primary overlay layer applied to one or more of the plurality of tension members or at least a portion of the jacket material.
Additionally or alternatively, in this or other embodiments the primary overlay layer is formed from a non-woven carbon nanotube sheet.
Additionally or alternatively, in this or other embodiments the carbon nanotubes are multi-walled carbon nanotubes.
Additionally or alternatively, in this or other embodiments the primary overlay layer is formed from an intrumenscent material.
Additionally or alternatively, in this or other embodiments a secondary overlay layer is applied over the primary overlay layer.
Additionally or alternatively, in this or other embodiments the secondary overlay layer defines a traction surface of the belt.
Additionally or alternatively, in this or other embodiments the secondary overlay layer is an elastomeric material.
Additionally or alternatively, in this or other embodiments the primary overlay layer is formed at the plurality of tension members by one or more of wrapping, dipping, spraying, laminating or pultrusion process.
Additionally or alternatively, in this or other embodiments the primary overlay layer is configured to improve thermal performance of the belt.
In another embodiment, an elevator system includes a hoistway, an elevator car located in the hoistway and movable therein, and a belt operably connected to the elevator car to suspend and/or drive the elevator car along the hoistway. The belt includes a plurality of tension members arranged along a belt width and extending longitudinally along a length of the belt, a jacket material at least partially encapsulating the plurality of tension members, and a primary overlay layer applied to one or more of the plurality of tension members or at least a portion of the jacket material.
Additionally or alternatively, in this or other embodiments the primary overlay layer is formed from a non-woven carbon nanotube sheet.
Additionally or alternatively, in this or other embodiments the carbon nanotubes are multi-walled carbon nanotubes.
Additionally or alternatively, in this or other embodiments the primary overlay layer is formed from an intrumenscent material.
Additionally or alternatively, in this or other embodiments a secondary overlay layer is applied over the primary overlay layer.
Additionally or alternatively, in this or other embodiments the secondary overlay layer defines a traction surface of the belt.
The following descriptions should not be considered limiting in any way. With reference to the accompanying drawings, like elements are numbered alike:
A detailed description of one or more embodiments of the disclosed apparatus and method are presented herein by way of exemplification and not limitation with reference to the Figures.
Shown in
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 belts 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 belts 16 around the various components of the elevator system 10.
In some embodiments, the elevator system 10 could use two or more belts 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 belts 16 engage the one or more sheaves 18 or only one side of the one or more belts 16 engages the one or more sheaves 18. The embodiment of
The belts 16 are constructed to have sufficient flexibility when passing over the one or more sheaves 18 to provide low bending stresses, meet belt life requirements and have smooth operation, while being sufficiently strong to be capable of meeting strength requirements for suspending and/or driving the elevator car 12.
The belt 16 has a belt width 26 and a belt thickness 32, with an aspect ratio of belt width 26 to belt thickness 32 greater than one. The belt 16 further includes a back side 34 opposite the traction side 30 and belt edges 36 extending between the traction side 30 and the back side 34.
As shown in
Exemplary load carrying fibers 42 include, but are not limited to, carbon, glass, aramid, nylon, and polymer fibers, for example. Each of the load carrying fibers 42 may be substantially identical or may vary. In addition, the matrix material 44 may be formed from any suitable material, such as polyurethane, vinylester, and epoxy for example. The materials of the load carrying fibers 42 and the matrix material 44 are selected to achieve a desired stiffness and strength of the tension member 24.
The tension member 24 may be formed as thin layers, in some embodiments by a pultrusion process. In a standard pultrusion process, the load carrying fibers 42 are impregnated with the matrix material 44 and are pulled through a heated die and additional curing heaters where the matrix material 44 undergoes cross linking. A person having ordinary skill in the art will understand that controlled movement and support of the pulled load carrying fibers 42 may be used to form a desired linear or curved profile of the tension member 24. In an exemplary embodiment, the tension member 24 has a cross-sectional thickness of about 0.5 millimeters to about 5 millimeters. Further, in some embodiments the tension member 24 has a circular cross-section, while in other embodiments the tension member 24 may have other cross-sectional shapes, such as rectangular or oval. Further, in some embodiments, the tension members 24 may include a tension element member coating layer 46 to, for example, promote adhesion with the jacket material 28.
While eight tension members 24 are illustrated in the embodiment of
The belt 16 includes one or more primary overlay layers 48 formed from a carbon nanotube sheet. In some embodiments, the carbon nanotube sheet is a non-woven carbon nanotube sheet, and further may be a non-woven sheet of multi-walled carbon nanotubes. The primary overlay layer 48 is configured to enhance fire and thermal performance of the belt 16, protecting the tension members 24 and the jacket material 28 during a thermal event. While in some embodiments, the primary overlay layer 48 is formed from a carbon nanotube sheet.
In other embodiments the primary overlay layer may be formed from an intrumenscent material to promote char formation and therefore retards heat conduction and flame formation and spread. Examples of intrumenscent materials include a paper formed from such a material, or a coating including an intrumenscent material. Intumenscent coatings may include three halogen-free flame-retardant additives: an acid source such as phase II ammonium polyphosphate, a carbon source such as pentaerythritol, and a blowing agent such as melamine mixed together with flame-retardant fillers and a polymer binder. Aluminum hydroxide (Al(OH)3) and magnesium hydroxide (Mg(OH)2) are examples of flame-retardant fillers.
The primary overlay layer 48 may be applied entirely around a perimeter of the jacket material 28, or on selected surfaces, such as the traction side 30, the back side 34 and/or the belt edges 36. A secondary overlay layer 54 is applied over the primary overlay layer 48 to protect the primary overlay layer 48 from wear or other damage during operation of the elevator system 10. In some embodiments, the secondary overlay layer 54 is applied at the traction side 30 and the back side 34, while in other embodiments the secondary overlay layer 54 is selectably applied to the traction side 30, the back side 34 and/or the belt edges 36. The second overlay layer 54 may be formed from the same material as the jacket material 38 or alternatively may be formed from a different material to enhance traction and wear performance of the belt 16.
Referring now to
Referring now to
Use of the primary overlay layer 48 improves fire and thermal performance of the belt 16 and maintains friction and traction performance of the belt 16, especially when used in conjunction with the secondary overlay layer 54.
The term “about” is intended to include the degree of error associated with measurement of the particular quantity based upon the equipment available at the time of filing the application. For example, “about” can include a range of ±8% or 5%, or 2% of a given value.
The terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the present disclosure. As used herein, the singular forms “a”, “an” and “the” are intended to include the plural forms as well, unless the context clearly indicates otherwise. It will be further understood that the terms “comprises” and/or “comprising,” when used in this specification, specify the presence of stated features, integers, steps, operations, elements, and/or components, but do not preclude the presence or addition of one or more other features, integers, steps, operations, element components, and/or groups thereof.
While the present disclosure has been described with reference to an exemplary embodiment or embodiments, it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the present disclosure. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the present disclosure without departing from the essential scope thereof. Therefore, it is intended that the present disclosure not be limited to the particular embodiment disclosed as the best mode contemplated for carrying out this present disclosure, but that the present disclosure will include all embodiments falling within the scope of the claims.
This application claims the benefit of 62/480,864, filed Apr. 3, 2017 which is incorporated herein by reference in its entirety.
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