The present disclosure is generally directed to composite elevator belts for use in lifting and lowering an elevator car. More particularly, the present disclosure is directed to composite elevator belts having, for example, a load carrier including a central layer and at least one outer layer, each outer layer defining a plurality of deformable pockets to reduce or neutralize tension and compression loads within the composite elevator belts. The present disclosure is also directed to methods for making composite elevator belts.
Elevators for vertically transporting people and goods are an integral part of modern residential and commercial buildings. A typical elevator system includes one or more elevator cars raised and lowered by a hoist system. The hoist system typically includes both driven and idler sheave assemblies over which one or more tension members attached to the elevator car are driven. The elevator car is raised or lowered due to traction between the tension members and drive sheaves. A variety of tension member types, including wire rope, V-belts, flat belts, and chains, may be used, with the sheave assemblies having corresponding running surfaces to transmit tractive force between the tension members and the sheave assemblies.
A limiting factor in the design of current elevator systems is the minimum bend radius of the tension members. If a tension member is flexed beyond its minimum bend radius, the compressive forces within the tension member may exceed the breaking strength of the tension member material, or may cause the material to buckle and fail. Continuous operation of the tension members below their minimum bend radii can cause fatigue at an increased and unpredictable rate and, under extreme circumstances, may result in a plastic deformation and failure. Thus, the minimum size of the sheaves useable in an elevator system is governed by the minimum bend radius of the tension members.
For several reasons, sheaves having a smaller diameter allow for more economical elevator system designs. First, the overall component cost of an elevator system can be significantly reduced by using smaller diameter sheaves and sheave assemblies. Second, smaller diameter sheaves reduce the motor torque necessary to drive the elevator system, thereby permitting use of smaller drive motors and allowing for smaller hoistway dimensions. Additionally, decreasing the bend radius of the tension members generally permits easier installation and decreases the spool size of the tension members.
Accordingly, minimizing the bend radius of elevator tension members and, conversely, increasing tension member flexibility is desirable. Among current tension member designs, composite belts having fiber or wire strands encased in a resin or polymer generally offer the greatest compromise of strength and flexibility. However, such belts must typically have a ratio of the bending diameter to the thickness of the load carrier of greater than 200 (that is, D/t>200, where “D” is bending diameter and “t” is load carrier thickness) to attain a sufficient fatigue life of the belt. For example, the minimum sheave diameter in a high rise elevator using known composite belts ranges from approximately 600 millimeters to approximately 1000 millimeters due to the stiffness of suitable resin casings. Typically, the resin must have a Young's modulus of approximately 2 gigapascals (GPa) or greater to adequately support the fibers or strands.
When a tension member is engaged with a sheave, the tension member is subjected to compression along an outer area in contact with the sheave and tension along an outer area away from the sheave. Frictional tractive force between the tension member and the pulley can impart additional compression to the outer surface of the tension member where the tension member is bent around the sheave. Many materials used to manufacture elevator tension members are significantly stronger in tension than compression. For example, carbon fiber, which is used in many composite belt designs, is typically only 20-70% as strong in compression as it is in tension. Additionally, carbon fiber and many other materials used in strands are brittle when subjected to compression. Therefore, tension members are typically more likely to fail, especially due to fatigue, as a result of internal compression experienced during the engagement with the sheave. Accordingly, the minimum bend radii of existing tension members is governed by internal compression loads due to bending.
In view of the foregoing, there exists a need for composite elevator belts which reduce or neutralize internal tension and/or compression loads such that the bending radius of the tension member is reduced while maintaining a high breaking strength. Additionally, there exists a need for methods and apparatuses for forming such composite elevator belts.
Embodiments of the present disclosure are directed to a composite elevator belt for engaging a sheave. The composite elevator belt includes a load carrier having at least one load carrier strand extending substantially parallel to a longitudinal axis of the load carrier and a resin coating surrounding the at least one load carrier strand and defining a plurality of predetermined, deformable cavities within the resin coating adjacent the at least one strand. When the elevator belt is bent around the sheave, the elevator belt defines a neutral bending zone located within the elevator belt generally coincident with the longitudinal axis, a tension zone radially outward of the neutral bending zone, and a compression zone radially inward from the neutral bending zone.
Embodiments of the present disclosure are directed to a composite elevator belt for engaging a sheave. The composite elevator belt includes a load carrier having at least one load carrier strand, in particular a plurality of load carrier strands, extending substantially parallel to a longitudinal axis of the load carrier and a resin coating surrounding the at least one load carrier strand and defining a plurality of predetermined, deformable cavities within the resin coating adjacent the at least one strand. When the elevator belt is bent around the sheave, the elevator belt defines a neutral bending zone located within the elevator belt generally coincident with the longitudinal axis, a tension zone radially outward of the neutral bending zone, and a compression zone radially inward from the neutral bending zone. The plurality of load carrier strands are arranged such that a space free of load carrier strands is provided between the load carrier strands. The space forms a straight continuous channel which travels from a first terminal end of the load carrier to an opposite terminal end of the load carrier.
Embodiments of the present disclosure are directed to a composite elevator belt for engaging a sheave. The composite elevator belt includes a load carrier having at least one load carrier strand, in particular a plurality of load carrier strands, extending substantially parallel to a longitudinal axis of the load carrier and a resin coating surrounding the at least one load carrier strand and defining a plurality of predetermined, deformable cavities within the resin coating adjacent the at least one strand. A first plurality of teeth extend transversely across a top surface of the resin coating. The first plurality of teeth comprise a root portion associated with the resin coating and a tip portion. When the elevator belt is bent around the sheave, the elevator belt defines a neutral bending zone located within the elevator belt generally coincident with the longitudinal axis, a tension zone radially outward of the neutral bending zone, and a compression zone radially inward from the neutral bending zone.
Embodiments of the present disclosure are directed to a composite elevator belt for engaging a sheave. The composite elevator belt includes a load carrier having at least one load carrier strand, in particular a plurality of load carrier strands, extending substantially parallel to a longitudinal axis of the load carrier and a resin coating surrounding the at least one load carrier strand and defining a plurality of predetermined, deformable cavities within the resin coating adjacent the at least one strand. A first plurality of teeth extend transversely across a top surface of the resin coating. The first plurality of teeth comprise a root portion associated with the resin coating and a tip portion. When the elevator belt is bent around the sheave, the elevator belt defines a neutral bending zone located within the elevator belt generally coincident with the longitudinal axis, a tension zone radially outward of the neutral bending zone, and a compression zone radially inward from the neutral bending zone. The plurality of load carrier strands are arranged such that a space free of load carrier strands is provided between the load carrier strands. The space forms a straight continuous channel which travels from a first terminal end of the load carrier to an opposite terminal end of the load carrier.
A “terminal end” refers to an outermost surface of the load carrier. It can be located at any position on the load carrier body, for example at a top surface and a bottom surface of the core layer of the load carrier. An “opposite terminal end” refers to a terminal end which is not the first terminal end. The opposite terminal end can be located when, starting from the first terminal end, the straight continuous channel free of load carrier strands is followed until the straight continuous channel terminates at an outermost surface of the load carrier. This outermost surface can be parallel to the first terminal end or not parallel to the first terminal end.
A “straight continuous channel” refers to the space within the load carrier which is free from load carrier strands. The straight continuous channel may comprise a thermoset material; a thermoplastic material; any combination of thermoset and thermoplastic materials; a polymer material; a polymer matrix material; a silicon matrix material; a sizing material, e.g., adhesive; or a polymer material which is reinforced with non-load carrying fibers. A straight continuous channel can also be referred to as an “inter-strand space” or more simply a “space”. The space is defined by the distance between two adjacent load carrier strands. A first space can be the same size as a second space, or different.
In some embodiments, the inter-strand space is greater in the thickness direction than the inter-strand space in the width direction. The inter-strand space in the width direction is preferably between 0 μm and 5 μm. The inter-strand space in the thickness direction is preferably between 3 μm and 50 μm. Most preferably, the inter-strand space in the thickness direction is half of the carbon fiber diameter. Preferably, the distance the straight continuous channel covers or the straight continuous channels cover, is the same as the thickness and/or width of the load carrier. In the case of a rectangular load carrier, the space can cover an uninterrupted distance across either the thickness of the load carrier, or, across the width of the load carrier or across both the thickness and the width of the load carrier. In the case of an elliptical load carrier, the largest distance the space covers is defined by the length of a first diameter which runs between two peripheral end points of the load carrier, which are positioned the furthest away from each other.
In some embodiments, the composite elevator belt has a cross-section along the longitudinal axis which shows the plurality of predetermined, deformable cavities having symmetry about a first axis, or symmetry about a first axis and at least one further axis.
In some embodiments, there is a plurality of spaces free of load carrier strands provided throughout the load carrier. Each space forms a straight continuous channel which travels from a first terminal end of the load carrier to an opposite terminal end of the load carrier.
In some embodiments, the plurality of load carrier strands are arranged into a plurality of groups.
In some embodiments, each group is encased with a further material.
In some embodiments, the further material is selected from the group comprising a sizing material, a polymer material, a silicon material or a combination of any thereof.
In some embodiments, the space free of load carrier strands covers a distance of between 0 μm to 50 μm.
In some embodiments the load carrier strand has a diameter in the range of 2 μm to 20 μm, more preferably, in the range of from 5 μm to 15 μm, most preferably, in the range of from 6 μm to 10 μm.
In some embodiments where a plurality of spaces are present within the load carrier strand, each space can cover varying distances. For example, a composite belt comprising a load carrier comprising plurality of load carrier strands can have a space in the width direction of 0 μm and a space in the thickness direction of 10 μm; or a composite belt comprising a load carrier comprising a plurality of load carrier strands can have a first space in the width direction of 0 μm and a second space in the width direction of 1.5 μm, a first space in the thickness direction of 7 μm and a second space in the thickness direction of 20 μm. The distance of the space in the width direction can be one particular distance or a combination of various distances. The distance of the space in the thickness direction can be one particular distance or a combination of various distances. This can be adapted according to the flexibility requirements expected of the load carrier. Another example can be a composite belt comprising a load carrier comprising a plurality of load carrier strands having a space in the width direction of 0.5 μm and a space in the thickness direction of 3 μm. When at least two different sizes of inter-strand space are present within a load carrier, the larger of the two sizes is located in the width direction (i.e., laterally) or in the thickness direction (i.e., vertically).
In some embodiments, the plurality of load-carrier strands is arranged such that a higher strand density is located at a particular area. For example, a higher density of load-carrier strands can be located towards the center of the load-carrier, or located at the periphery of the load-carrier. Preferably, a higher strand density is located in the center of the load-carrier and a lower strand density is located at the periphery of the load-carrier. This arrangement allows for better flexibility of the load-carrier
In some embodiments the resin coating, which can also be referred to as a “core layer” or “matrix” comprises a material with a Young's modulus of less than 2 GPa. This is practicable in particular when teeth are included on the load carrier, and there is an advantageous arrangement of the load carrier strands. These combined features provide for a controlled buckling, which consequently allows for a material with a Young's modulus of 2 GPa or less, to be used as the resin coating.
In some embodiments the fiber volume ratio of the load carrier strands is in a range of from 40% to 70%.
In some embodiments the first plurality of teeth is reinforced with fibers. These can be any fibers as herein described, preferably the reinforcing fibers are smaller in length than the load carrier strands.
In some embodiments the first plurality of teeth is reinforced with fibers which are positioned in a transversal or criss-cross direction compared to the longitudinal direction of the load carrier strands.
In some embodiments the height of a tooth within the first plurality of teeth is in a range from 15 μm to 1 mm, preferably in a range from 200 μm to 600 μm.
The presence of teeth on a composite elevator belt affects the deflection, or buckling of the load carrier strands and consequently help reduce the compression force in the strands. When the fibers in a compression zone of the composite belt buckle, the neutral bending axes shifts in the direction of the tension zone and the overall stress in the belt decreases. Buckling can be activated by force or by a geometric imbalance. The introduction of teeth to the load carrier be it in a symmetrical or unsymmetrical pattern, helps introduce a force unbalance, which improves buckling and consequently reduces the compression forces in the load carrier strands. Teeth which are arranged in a symmetrical pattern on a load carrier allow the introduction of symmetrical repeatable buckling. Teeth which are arranged in an unsymmetrical pattern are preferred when issues such as vibration, noise or concentrated fiber fatigue arise. The teeth can be reinforced with fibers, either transversal, or in a criss-cross direction compared to the longitudinal unidirectional load carrier strands. The shape and dimensions of teeth are selected according to the strength and dimensions of the load carrier itself. Tooth shape can include rectangular, trapezoidal, triangular, rounded, among others.
The dimensions of the teeth, including, height, width and distance between each tooth, should be designed to take into consideration the possibility that some jacket material may enter the gap between the teeth. Should this happen, the height of the teeth for example is reduced. By taking this into consideration when designing the height of the teeth and by ensuring that the resultant tooth height, including the jacket layer, is a height which achieves the desired buckling effect, the reduction in compression forces in the load carrier strands can be optimized.
A preferred tooth height is between 40 microns and 1 mm. This applies to teeth used in a first plurality of teeth as well as to teeth used in a second or further plurality of teeth.
In some embodiments, when the elevator belt is bent around the sheave, the deformable cavities in the tension zone lengthen longitudinally relative to the longitudinal axis and retract radially relative to the longitudinal axis. When the elevator belt is bent around the sheave, the deformable cavities in the compression zone shorten longitudinally relative to the longitudinal axis and lengthen radially relative to the longitudinal axis.
In some embodiments, the load carrier includes a plurality of load carrier strands. The plurality of load carrier strands includes a first load carrier strand located in the tension zone and a second load carrier strand located in the compression zone.
In some embodiments, the first load carrier strand and the second load carrier strand each extend generally parallel to the longitudinal axis.
In some embodiments, when the elevator belt is bent around the sheave, the first load carrier strand is tensioned in a direction generally parallel to the longitudinal axis and the deformable cavities adjacent the first load carrier strand lengthen longitudinally in a direction generally parallel to the first load carrier strand and shorten radially in the direction generally perpendicular to the first load carrier strand to reposition the first load carrier strand radially closer to the neutral bending zone.
In some embodiments, when the elevator belt is bent around the sheave, the deformable cavities adjacent the second load carrier strand shorten longitudinally in a direction generally parallel to the first load carrier strand and lengthen radially in the direction generally perpendicular to the first load carrier strand inducing the second load carrier strand to deform into an undulating curve.
In some embodiments, when the elevator belt is bent around the sheave, the undulating curve of the second load carrier strand bends at least partially around the deformed cavities adjacent the second load carrier strand.
In some embodiments, the plurality of load carrier strands includes a third load carrier strand disposed between the first load carrier strand and the second load carrier strand and located in the neutral bending zone.
In some embodiments, each of the plurality of cavities encloses one of a gas, a liquid, and a deformable solid.
In some embodiments, a diameter of each of the plurality of cavities is between one-half and two times the diameter of the at least one load carrier strand.
In some embodiments, the at least one load carrier strand is non-continuous.
In some embodiments, the combined Young's modulus of the resin coating including the plurality of cavities is less than approximately 2 gigapascals.
In some embodiments, a total volume of the plurality of cavities in the compression zone is substantially equal to one third of a total volume of the resin coating, including the total volume of the plurality of cavities, in the compression zone.
In some embodiments, a total volume of the plurality of cavities in the tension zone is substantially equal to one third of a total volume of the resin coating, including the total volume of the plurality of cavities, in the tension zone.
In some embodiments, the composite elevator belt further includes a jacket layer disposed on the load carrier.
Still other embodiments of the present disclosure are directed to use of a composite elevator belt in an elevator system which includes an elevator shaft having a support frame, an elevator car movable along a vertical travel path defined by the elevator shaft, and a motor arrangement including at least one drive sheave rotatable via the motor arrangement.
Still other embodiments of the present disclosure are directed to methods of making a composite elevator belt for engaging a sheave. The method includes drawing a load carrier having at least one load carrier strand into a liquid resin bath, surrounding the at least one load carrier strand with a resin coating in the liquid resin bath, and defining a plurality of deformable cavities adjacent the at least one load carrier strand in the resin coating.
In some embodiments, the method further includes drawing the load carrier with the resin coating through a forming and curing die and curing the resin coating into a solidified form to define the plurality of deformable cavities in the resin coating.
In some embodiments, the method further includes depositing a jacket layer onto the resin coating after solidifying the resin coating into the solidified form.
In some embodiments, the method further includes intermixing an additive into the liquid resin bath, the additive being one of gas particles, liquid particles, and deformable solid particles. The plurality of deformable cavities are defined by the resin coating solidifying to surround the additive.
In some embodiments, a volume of the additive intermixed into the liquid resin bath is substantially equal to a volume of the liquid resin in the liquid resin bath.
In some embodiments, the method further includes intermixing a blowing agent into the liquid resin bath. Curing the resin coating causes the blowing agent to at least partially decompose into gas pockets in the liquid resin surrounding the load carrier strand. The plurality of deformable cavities are defined by the resin coating solidifying around the gas pockets.
In some embodiments, the method further includes drawing a second load carrier having at least one load carrier strand into a second liquid resin bath, surrounding the at least one load carrier strand of the second load carrier with a resin coating in the second liquid resin bath, and defining a plurality of deformable cavities adjacent the at least one load carrier strand of the second load carrier in the resin coating.
In some embodiments, the method further includes drawing the first load carrier with the resin coating having the plurality of deformable cavities formed therein into a forming and curing die, drawing the second load carrier with the resin coating having the plurality of deformable cavities formed therein into the forming and curing die, joining the first load carrier with the second load carrier together in the forming and curing die, and curing the resin coatings on the first load carrier and the second load carrier into solidified form in the forming and curing die.
In some embodiments, the method further includes drawing a third load carrier having at least one load carrier strand into a third liquid resin bath and surrounding the at least one load carrier strand of the third load carrier with a resin coating in the third liquid resin bath.
In some embodiments, the method further includes drawing the first load carrier with the resin coating having the plurality of deformable cavities formed therein into a forming and curing die, drawing the second load carrier with the resin coating having the plurality of deformable cavities formed therein into the forming and curing die, drawing the third load carrier with the resin coating into the forming and curing die interposed between the first load carrier and the second load carrier, joining the first load carrier with the second load carrier together with the third load carrier interposed between the first load carrier and the second load carrier in the forming and curing die, and curing the resin coatings on the first load carrier, the second load carrier, and the third load carrier into solidified form in the forming and curing die. Still other embodiments of the present disclosure are directed to methods of making a composite elevator belt for engaging a sheave. The method includes drawing a load carrier comprising at least one load carrier strand into a fiber arranger, followed by drawing the load carrier comprising at least one load carrier strand into a cavity printer to define a plurality of deformable cavities adjacent the at least one load carrier strand in the resin coating, curing the plurality of deformable cavities to produce a load carrier comprising a plurality of cured cavities, drawing the load carrier comprising a cured plurality of cavities into a liquid resin bath and surrounding the at least one load carrier strand with a resin coating in the liquid resin bath.
In some embodiments, the method further includes drawing the load carrier with the resin coating into a forming and curing die.
In some embodiments, the method further includes depositing a jacket layer onto the resin coating.
In some embodiments, the method further includes drawing a second load carrier comprising at least one load carrier strand into a fiber arranger, followed by drawing the second load carrier comprising at least one load carrier strand into a cavity printer to define a plurality of deformable cavities adjacent the at least one load carrier strand in the resin coating, curing the plurality of deformable cavities to produce a second load carrier comprising a plurality of cured cavities, drawing the second load carrier comprising a cured plurality of cavities into a second liquid resin bath and surrounding the at least one load carrier strand of the second load carrier with a resin coating in the second liquid resin bath.
In some embodiments, the method further includes drawing the first load carrier with the resin coating having the plurality of deformable cavities formed therein into a forming and curing die, drawing the second load carrier with the resin coating having the plurality of deformable cavities formed therein into the forming and curing die, joining the first load carrier with the second load carrier together in the forming and curing die, curing the resin coatings on the first load carrier and the second load carrier into solidified form in the forming and curing die.
In some embodiments, the method further includes drawing a third load carrier comprising at least one load carrier strand into a fiber arranger, followed by drawing the third load carrier comprising at least one load carrier strand into a cavity printer to define a plurality of deformable cavities adjacent the at least one load carrier strand in the resin coating, curing the plurality of deformable cavities to produce a third load carrier comprising a plurality of cured cavities, drawing the third load carrier comprising a cured plurality of cavities into a third liquid resin bath and surrounding the at least one load carrier strand of the third load carrier with a resin coating in the third liquid resin bath.
In some embodiments, the method further includes drawing the first load carrier with the resin coating having the plurality of deformable cavities formed therein into a forming and curing die, drawing the second load carrier with the resin coating having the plurality of deformable cavities formed therein into the forming and curing die, drawing the third load carrier with the resin coating into the forming and curing die interposed between the first load carrier and the second load carrier, joining the first load carrier with the second load carrier together with the third load carrier interposed between the first load carrier and the second load carrier in the forming and curing die, curing the resin coatings on the first load carrier, the second load carrier, and the third load carrier into solidified form in the forming and curing die
Still other embodiments of the present disclosure are directed to an elevator system including an elevator shaft having a support frame, an elevator car movable along a vertical travel path defined by the elevator shaft, a motor arrangement including at least one drive sheave rotatable via the motor arrangement, and at least one composite elevator belt in frictional tractive engagement with and configured to bend around the drive sheave of the motor arrangement. The at least one composite elevator belt includes a load carrier having at least one load carrier strand extending substantially parallel to a longitudinal axis of the load carrier and a resin coating surrounding the at least one load carrier strand and defining a plurality of predetermined, deformable cavities within the resin coating adjacent the at least one strand. When the elevator belt is bent around the drive sheave, the elevator belt defines a neutral bending zone located within the elevator belt generally coincident with the longitudinal axis, a tension zone radially outward of the neutral bending zone, and a compression zone radially inward from the neutral bending zone.
In some embodiments, when the elevator belt is bent around the drive sheave, the deformable cavities in the tension zone lengthen longitudinally relative to the longitudinal axis and retract radially relative to the longitudinal axis. When the elevator belt is bent around the drive sheave, the deformable cavities in the compression zone shorten longitudinally relative to the longitudinal axis and lengthen radially relative to the longitudinal axis.
In some embodiments, the load carrier of the composite elevator belt includes a plurality of load carrier strands. The plurality of load carrier strands includes a first load carrier strand located in the tension zone and a second load carrier strand located in the compression zone.
In some embodiments, each of the plurality of cavities of the at least one composite elevator belt encloses one of a gas, a liquid, and a deformable solid.
In some embodiments a diameter of each cavity in the at least one composite elevator belt is between one-half and two times a diameter of each load carrier strand in the at least on composite elevator belt.
Further embodiments of the present disclosure will now be described in the following numbered clauses:
Clause 1. A composite elevator belt for engaging a sheave, the composite elevator belt comprising: a load carrier comprising at least one load carrier strand extending substantially parallel to a longitudinal axis of the load carrier; and a resin coating surrounding the at least one load carrier strand and defining a plurality of predetermined, deformable cavities within the resin coating adjacent the at least one strand; wherein, when the elevator belt is bent around the sheave, the elevator belt defines a neutral bending zone located within the elevator belt generally coincident with the longitudinal axis, a tension zone radially outward of the neutral bending zone, and a compression zone radially inward from the neutral bending zone.
Clause 2. A composite elevator belt for engaging a sheave, the composite elevator belt comprising: a load carrier comprising at least one load carrier strand, in particular, a plurality of load carrier strands, extending substantially parallel to a longitudinal axis of the load carrier; and a resin coating surrounding the at least one load carrier strand and defining a plurality of predetermined, deformable cavities within the resin coating adjacent the at least one strand; wherein, when the elevator belt is bent around the sheave, the elevator belt defines a neutral bending zone located within the elevator belt generally coincident with the longitudinal axis, a tension zone radially outward of the neutral bending zone, and a compression zone radially inward from the neutral bending zone; wherein the plurality of load carrier strands are arranged such that a space free of load carrier strands is provided between the load carrier strands; wherein the space forms a straight continuous channel which travels from a first terminal end of the load carrier to an opposite terminal end of the load carrier.
Clause 3. A composite elevator belt for engaging a sheave, the composite elevator belt comprising: a load carrier comprising at least one load carrier strand, in particular, a plurality of load carrier strands, extending substantially parallel to a longitudinal axis of the load carrier; and a resin coating surrounding the at least one load carrier strand and defining a plurality of predetermined, deformable cavities within the resin coating adjacent the at least one strand; and a first plurality of teeth extending transversely across a top surface of the resin coating, the first plurality of teeth comprising a root portion associated with the resin coating and a tip portion wherein, when the elevator belt is bent around the sheave, the elevator belt defines a neutral bending zone located within the elevator belt generally coincident with the longitudinal axis, a tension zone radially outward of the neutral bending zone, and a compression zone radially inward from the neutral bending zone.
Clause 4. A composite elevator belt for engaging a sheave, the composite elevator belt comprising: a load carrier comprising at least one load carrier strand, in particular, a plurality of load carrier strands, extending substantially parallel to a longitudinal axis of the load carrier; and a resin coating surrounding the at least one load carrier strand and defining a plurality of predetermined, deformable cavities within the resin coating adjacent the at least one strand; and a first plurality of teeth extending transversely across a top surface of the resin coating, the first plurality of teeth comprising a root portion associated with the resin coating and a tip portion; wherein, when the elevator belt is bent around the sheave, the elevator belt defines a neutral bending zone located within the elevator belt generally coincident with the longitudinal axis, a tension zone radially outward of the neutral bending zone, and a compression zone radially inward from the neutral bending zone; wherein the plurality of load carrier strands are arranged such that a space free of load carrier strands is provided between the load carrier strands; wherein the space forms a straight continuous channel which travels from a first terminal end of the load carrier to an opposite terminal end of the load carrier.
Clause 5. The composite elevator belt of any of clauses 1 to 4, wherein a cross-section of the elevator belt along the longitudinal axis shows the plurality of predetermined, deformable cavities having: a) symmetry about a first axis (A); or b) symmetry about a first axis A (A) and at least one further axis (B). Preferably, the plurality of cavities are arranged so that the cavities in the tension zone are a mirror inversion of the cavities in the compression zone, or the plurality of cavities in the compression zone and the plurality of cavities the tension zone are symmetrical.
Clause 6. The composite elevator belt of any of clauses 2, 4 to 5, wherein a plurality of spaces free of load carrier strands is provided throughout the load carrier and wherein each space forms a straight continuous channel which travels from a first terminal end of the load carrier to an opposite terminal end of the load carrier.
Clause 7. The composite elevator belt of any of clauses 2 to 6, wherein the plurality of load carrier strands are arranged into a plurality of groups.
Clause 8. The composite elevator belt of clause 7, wherein each group is encased with a further material.
Clause 9. The composite elevator belt of clause 8, wherein the further material is selected from the group comprising: a sizing material, a polymer material, a silicon material, or a combination of any thereof.
Clause 10. The composite elevator belt of any of clauses 2, 4 to 9, wherein the space covers a distance of between 0 μm to 50 μm
Clause 11. The composite elevator belt of any of clauses 1 to 10, wherein the load carrier strand has a diameter in the range of 2 μm to 20 μm.
Clause 12. The composite elevator belt of any of clauses 2, 4 to 11, wherein the space can be adapted to cover varying distances throughout the cross-section of the load carrier.
Clause 13. The composite elevator belt of any of clauses 1 to 12, wherein, when the elevator belt is bent around the sheave, the deformable cavities in the tension zone lengthen longitudinally relative to the longitudinal axis and retract radially relative to the longitudinal axis, and wherein, when the elevator belt is bent around the sheave, the deformable cavities in the compression zone shorten longitudinally relative to the longitudinal axis and lengthen radially relative to the longitudinal axis.
Clause 14. The composite elevator belt of any of clauses 1 to 13, wherein the load carrier comprises a plurality of load carrier strands, the plurality of load carrier strands comprising a first load carrier strand located in the tension zone and a second load carrier strand located in the compression zone.
Clause 15. The composite elevator belt of any of clauses 1 to 14, wherein the first load carrier strand and the second load carrier strand each extend generally parallel to the longitudinal axis.
Clause 16. The composite elevator belt of any of clauses 1 to 15, wherein, when the elevator belt is bent around the sheave, the first load carrier strand is tensioned in a direction generally parallel to the longitudinal axis and the deformable cavities adjacent the first load carrier strand lengthen longitudinally in a direction generally parallel to the first load carrier strand and shorten radially in the direction generally perpendicular to the first load carrier strand to reposition the first load carrier strand radially closer to the neutral bending zone.
Clause 17. The composite elevator belt of any of clauses 1 to 16, wherein, when the elevator belt is bent around the sheave, the deformable cavities adjacent the second load carrier strand shorten longitudinally in a direction generally parallel to the first load carrier strand and lengthen radially in the direction generally perpendicular to the first load carrier strand inducing the second load carrier strand to deform into an undulating curve.
Clause 18. The composite elevator belt of any of clauses 1 to 17, wherein, when the elevator belt is bent around the sheave, the undulating curve of the second load carrier strand bends at least partially around the deformed cavities adjacent the second load carrier strand.
Clause 19. The composite elevator belt of any of clauses 1 to 18, wherein the plurality of load carrier strands comprises a third load carrier strand disposed between the first load carrier strand and the second load carrier strand and located in the neutral bending zone.
Clause 20. The composite elevator belt of any of clauses 1 to 19, wherein each of the plurality of cavities encloses one of a gas, a liquid, and a deformable solid. The cavity material can for example be a silicon material with a young's modulus of less than 0.1 GPA, or a curable viscosity gel-like silicon material with a high viscosity. The cavity material preferably has a good impregnation behavior in the uncured state, this is beneficial for the production process. Curing can be activated for example by heat, an electronic beam or UV light.
Clause 21. The composite elevator belt of any of clauses 1 to 20, wherein a diameter of each of the plurality of cavities is between one-half and two times the diameter of the at least one load carrier strand.
Clause 22. The composite elevator belt of any of clauses 1 to 21, wherein the at least one load carrier strand is non-continuous.
Clause 23. The composite elevator belt of any of clauses 1 to 22, wherein the combined Young's modulus of the resin coating including the plurality of cavities is less than approximately 2 gigapascals.
Clause 24. The composite elevator belt of any of clauses 1 to 23, wherein a total volume of the plurality of cavities in the compression zone is substantially equal to one third of a total volume of the resin coating, including the total volume of the plurality of cavities, in the compression zone. Preferably, the matrix volume:fiber volume ratio is the same for the compression and tension zone. This is advantageous because if counter bending occurs, the tension zone can become the compression zone and vice versa. The fiber volume content in the neutral zone can be different, preferably higher than that in the tension and compression zones.
Clause 25. The composite elevator belt of any of clauses 1 to 24, further comprising a jacket layer disposed on the load carrier. The composite elevator belt can also comprises a first jacket layer extending in the longitudinal direction, wherein, when the load carrier comprises a first plurality of teeth comprising a root portion and a tip portion, the tip portion is associated with a bottom surface of the further jacket layer. It is also envisaged that the elevator belt can further comprise a second plurality of teeth comprising a root portion and a tip portion, wherein the tip portion is associated with a bottom surface of a second further jacket layer.
Clause 26. Use of the composite elevator belt of any of clauses 1 to 25 in an elevator system, the elevator system comprising: an elevator shaft having a support frame; an elevator car movable along a vertical travel path defined by the elevator shaft; and a motor arrangement comprising at least one drive sheave rotatable via the motor arrangement.
Clause 27. A method of making a composite elevator belt for engaging a sheave, the method comprising: drawing a load carrier comprising at least one load carrier strand into a liquid resin bath; surrounding the at least one load carrier strand with a resin coating in the liquid resin bath; and defining a plurality of deformable cavities adjacent the at least one load carrier strand in the resin coating.
Clause 28. The method of clause 27, further comprising: drawing the load carrier with the resin coating into a forming and curing die; and curing the resin coating into a solidified form to define the plurality of deformable cavities in the resin coating. Preferably the curing mode is different for the cavity material and the resin coating, this prevents instable boundary layers between the resin coating and cavities. Instable boundary layers could cause cracks or unwanted voids in the resin coating
Clause 29. The method of clause 27 or 28, further comprising depositing a jacket layer onto the resin coating after solidifying the resin coating into the solidified form.
Clause 30. The method of any of clauses 27 to 29, further comprising intermixing an additive into the liquid resin bath, wherein the additive comprises one of gas particles, liquid particles, and deformable solid particles, and wherein the plurality of deformable cavities are defined by the resin coating solidifying around the additive.
Clause 31. The method of any of clauses 27 to 30, wherein a volume of the additive intermixed into the liquid resin bath is substantially equal to a volume of the liquid resin in the liquid resin bath.
Clause 32. The method of any of clauses 27 to 31, further comprising intermixing a blowing agent into the liquid resin bath, wherein curing the resin coating causes the blowing agent to at least partially decompose into gas pockets in the liquid resin surrounding the load carrier strand, and wherein the plurality of deformable cavities are defined by the resin coating solidifying around the gas pockets.
Clause 33. The method of any of clauses 27 to 32, further comprising: drawing a second load carrier comprising at least one load carrier strand into a second liquid resin bath; surrounding the at least one load carrier strand of the second load carrier with a resin coating in the second liquid resin bath; and defining a plurality of deformable cavities adjacent the at least one load carrier strand of the second load carrier in the resin coating.
Clause 34. The method of any of clauses 27 to 33, further comprising: drawing the first load carrier with the resin coating having the plurality of deformable cavities formed therein into a forming and curing die; drawing the second load carrier with the resin coating having the plurality of deformable cavities formed therein into the forming and curing die; joining the first load carrier with the second load carrier together in the forming and curing die; and curing the resin coatings on the first load carrier and the second load carrier into solidified form in the forming and curing die.
Clause 35. The method of any of clauses 27 to 34, further comprising: drawing a third load carrier comprising at least one load carrier strand into a third liquid resin bath; and surrounding the at least one load carrier strand of the third load carrier with a resin coating in the third liquid resin bath.
Clause 36. The method of any of clauses 27 to 35, further comprising: drawing the first load carrier with the resin coating having the plurality of deformable cavities formed therein into a forming and curing die; drawing the second load carrier with the resin coating having the plurality of deformable cavities formed therein into the forming and curing die; drawing the third load carrier with the resin coating into the forming and curing die interposed between the first load carrier and the second load carrier; joining the first load carrier with the second load carrier together with the third load carrier interposed between the first load carrier and the second load carrier in the forming and curing die; and curing the resin coatings on the first load carrier, the second load carrier, and the third load carrier into solidified form in the forming and curing die.
Clause 37. A method of making a composite elevator belt for engaging a sheave, the method comprising: drawing a load carrier comprising at least one load carrier strand into a fiber arranger; drawing the load carrier comprising at least one load carrier strand into a cavity printer to define a plurality of deformable cavities adjacent the at least one load carrier strand in the resin coating; curing the plurality of deformable cavities to produce a load carrier comprising a plurality of cured cavities; drawing the load carrier comprising a cured plurality of cavities into a liquid resin bath; surrounding the at least one load carrier strand with a resin coating in the liquid resin bath.
Clause 38. The method according to clause 37 further comprising: drawing the load carrier with the resin coating into a forming and curing die.
Clause 39. The method according to any of clauses 37 to 38 further comprising: depositing a jacket layer onto the resin coating.
Clause 40. The method according to any of clauses 37 to 39 further comprising: drawing a second load carrier comprising at least one load carrier strand into a fiber arranger; followed by drawing the second load carrier comprising at least one load carrier strand into a cavity printer to define a plurality of deformable cavities adjacent the at least one load carrier strand in the resin coating; curing the plurality of deformable cavities to produce a second load carrier comprising a plurality of cured cavities; drawing the second load carrier comprising a cured plurality of cavities into a second liquid resin bath and surrounding the at least one load carrier strand of the second load carrier with a resin coating in the second liquid resin bath.
Clause 41. The method according to any of clauses 37 to 40 further comprising: drawing the first load carrier with the resin coating having the plurality of deformable cavities formed therein into a forming and curing die; drawing the second load carrier with the resin coating having the plurality of deformable cavities formed therein into the forming and curing die; joining the first load carrier with the second load carrier together in the forming and curing die; curing the resin coatings on the first load carrier and the second load carrier into solidified form in the forming and curing die.
Clause 42. The method according to any of clauses 37 to 41 further comprising: drawing a third load carrier comprising at least one load carrier strand into a fiber arranger; followed by drawing the third load carrier comprising at least one load carrier strand into a cavity printer to define a plurality of deformable cavities adjacent the at least one load carrier strand in the resin coating; curing the plurality of deformable cavities to produce a third load carrier comprising a plurality of cured cavities; drawing the third load carrier comprising a cured plurality of cavities into a third liquid resin bath and surrounding the at least one load carrier strand of the third load carrier with a resin coating in the third liquid resin bath.
Clause 43. The method according to any of clauses 37 to 42 further comprising: drawing the first load carrier with the resin coating having the plurality of deformable cavities formed therein into a forming and curing die; drawing the second load carrier with the resin coating having the plurality of deformable cavities formed therein into the forming and curing die; drawing the third load carrier with the resin coating into the forming and curing die interposed between the first load carrier and the second load carrier; joining the first load carrier with the second load carrier together with the third load carrier interposed between the first load carrier and the second load carrier in the forming and curing die; curing the resin coatings on the first load carrier, the second load carrier, and the third load carrier into solidified form in the forming and curing die
Clause 44. An elevator system, comprising: an elevator shaft having a support frame; an elevator car movable along a vertical travel path defined by the elevator shaft; a motor arrangement comprising at least one drive sheave rotatable via the motor arrangement; and at least one composite elevator belt in frictional tractive engagement with and configured to bend around the drive sheave of the motor arrangement, the at least one composite elevator belt comprising: a load carrier comprising at least one load carrier strand extending substantially parallel to a longitudinal axis of the load carrier; and a resin coating surrounding the at least one load carrier strand and defining a plurality of predetermined, deformable cavities within the resin coating adjacent the at least one strand; wherein, when the elevator belt is bent around the drive sheave, the elevator belt defines a neutral bending zone located within the elevator belt generally coincident with the longitudinal axis, a tension zone radially outward of the neutral bending zone, and a compression zone radially inward from the neutral bending zone.
Clause 45. The elevator system of clause 44, wherein, when the elevator belt is bent around any of the drive sheaves or elevator, sheaves, the deformable cavities in the tension zone lengthen longitudinally relative to the longitudinal axis and retract radially relative to the longitudinal axis, and wherein, when the elevator belt is bent around the drive sheave, the deformable cavities in the compression zone shorten longitudinally relative to the longitudinal axis and lengthen radially relative to the longitudinal axis.
Clause 46. The elevator system of clause 44 or 45, wherein the load carrier of the composite elevator belt comprises a plurality of load carrier strands, and wherein the plurality of load carrier strands comprises a first load carrier strand located in the tension zone and a second load carrier strand located in the compression zone.
Clause 47. The elevator system of any of causes 44 to 46, wherein each of the plurality of cavities of the at least one composite elevator belt encloses one of a gas, a liquid, and a deformable solid.
Clause 48. The elevator system of any of clauses 44 to 47, wherein a diameter of each cavity in the at least one composite elevator belt is between one-half and two times a diameter of each load carrier strand in the at least on composite elevator belt.
These and other features and characteristics of composite elevator belts, methods of making the same, and use of the same in an elevator system will become more apparent upon consideration of the following description and the appended claims with reference to the accompanying drawings, all of which form a part of this specification, wherein like reference numerals designate corresponding parts in the various figures. It is to be expressly understood, however, that the drawings are for the purpose of illustration and description only and are not intended as a definition of the limits of the disclosure. As used in the specification and claims, the singular forms of “a”, “an”, and “the” include plural referents unless the context clearly dictates otherwise.
For purposes of the description hereinafter, the terms “upper”, “lower”, “right”, “left”, “vertical”, “horizontal”, “top”, “bottom”, “lateral”, “longitudinal”, and derivatives thereof shall relate to the disclosed apparatus as it is oriented in the figures. However, it is to be understood that the apparatus of the present disclosure may assume alternative variations and step sequences, except where expressly specified to the contrary. It is also to be understood that the specific systems and processes illustrated in the attached drawings and described in the following specification are simply exemplary examples of the apparatus disclosed herein. Hence, specific dimensions and other physical characteristics related to the examples disclosed herein are not to be considered as limiting.
As used herein, the terms “sheave” and “pulley” are used interchangeably to describe a wheel for tractive connection to a tension member of any type. It is to be understood that a “pulley” is encompassed by the recitation of a “sheave”, and vice versa, unless explicitly stated to the contrary.
As used herein, the terms “substantially” or “approximately”, when used to relate a first numerical value or condition to a second numerical value or condition, means that the first numerical value or condition is within 10 units or within 10% of the second numerical value or condition, as the context dictates and unless explicitly indicated to the contrary. For example, the term “substantially parallel to” means within plus or minus 10° of parallel. Similarly, the term “substantially perpendicular to” means within plus or minus 10° of perpendicular. Similarly, the term “substantially equal in volume” means within 10% of being equal in volume.
As used herein, the terms “transverse”, “transverse to”, and “transversely to” a given direction mean not parallel to that given direction. Thus, the terms “transverse”, “transverse to”, and “transversely to” a given direction encompass directions perpendicular to, substantially perpendicular to, and otherwise not parallel to the given direction.
As used herein, the term “diameter” means any straight line segment passing through a center point of a circle, sphere, ellipse, ellipsoid, or other rounded two- or three-dimensional object from one point on the periphery of said object to another point on the periphery of said object. Non-circular and non-spherical objects may have several such diameters of differing length, including a major diameter being the longest straight line segment meeting the aforementioned criteria, and a minor diameter being the shortest straight line segment meeting the aforementioned criteria.
As used herein, the term “associated with”, when used in reference to multiple features or structures, means that the multiple features or structures are in contact with, touching, directly connected to, indirectly connected to, adhered to, or integrally formed with one another.
Referring to the drawings in which like reference numerals refer to like parts throughout the several views thereof, the present disclosure is generally directed to a composite elevator belt for use in an elevator system to raise and lower an elevator car. It is to be understood, however, that the composite belt described herein may be used in many different applications in which tension members are utilized in traction with sheaves. The present disclosure is also directed to an elevator system utilizing the composite elevator belt. Further, the present disclosure is directed to methods of making the composite elevator belt.
Referring now to
Each load carrier 200 includes at least one outer layer 210 disposed on a central layer 220. Each of the at least one outer layers 210 may include one or more load carrier strands 211 arranged parallel to the longitudinal axis L of the composite elevator belt 100. In other embodiments, the load carrier strands 211 may be interrupted along the longitudinal axis L, and may or may not overlap one another. In still other embodiments, the load carrier strands 211 may be arranged in multiple layers spaced apart from one another in a direction perpendicular to the longitudinal axis L. In still other embodiments, the load carrier strands 211 may be entangled, discontinuous fibers arranged in a mat or roving. The load carrier strands 211 may be encased in a resin coating 212 which defines a cross-sectional profile of the outer layer 210 and fills any voids between the load carrier strands 211. The one or more load carrier strands 211 may account for between approximately 30% and approximately 60% of the total volume of each outer layer 210. However, the volume ratio of the load carrier strands 211 to the total volume of each outer layer 210 may be adjusted to balance the strength and flexibility of the composite elevator belt 100 for a particular application. Generally, increasing the volume ratio of the load carrier strands 211 to the total volume of each outer layer 210 increases the strength and decreases the flexibility of the composite elevator belt 100, while decreasing the volume ratio of the load carrier strands 211 to the total volume of each outer layer 210 decreases the strength and increases the flexibility of the composite elevator belt 100.
The central layer 220 may include one or more load carrier strands 221 arranged parallel to and continuous along the longitudinal axis L of the composite elevator belt 100. In other embodiments, the load carrier strands 221 may be interrupted along the longitudinal axis L, and may or may not overlap one another. In still other embodiments, the load carrier strands 221 may be arranged in multiple layers spaced apart from one another in a direction perpendicular to the longitudinal axis L. In still other embodiments, the load carrier strands 221 may be entangled, discontinuous fibers arranged in a mat or roving. The one or more load carrier strands 221 may be encased in a resin coating 222, which defines a cross-sectional profile of the central layer 220 and fills any voids between the load carrier strands 221. The resin coating 222 may be substantially free of any voids or impurities except for those unintentionally introduced during the manufacturing of the central layer 220. The one or more load carrier strands 221 may account for between approximately 60% and approximately 80% of the total volume of the central layer 220. However, the volume ratio of the load carrier strands 221 to the total volume of the central layer 220 may be adjusted to balance the strength and flexibility of the composite elevator belt 100 for a particular application. Generally, increasing the volume ratio of the load carrier strands 221 to the total volume of the central layer 220 increases the strength and decreases the flexibility of the composite elevator belt 100, while decreasing the volume ratio of the load carrier strands 221 to the total volume of the central layer 220 decreases the strength and increases the flexibility of the composite elevator belt 100.
As the at least one outer layer 210 may occupy either the compression zone CZ or the tension zone TZ of the composite elevator belt 100, the at least one outer layer 210 may be subject to greater loads due to bending than the central layer 220, which may be generally coincident with the neutral bending zone NZ. As such, the ratio of the volume of the load carrier strands 211 of each outer layer 210 to the total volume of that outer layer 210 may be less than the ratio of the volume of the load carrier strands 221 of the central layer 220 to the total volume of the central layer 220.
The resin coating 212 of each outer layer 210 defines a plurality of deformable cavities 213 interspersed throughout. The plurality of deformable cavities 213 are positioned adjacent to the load carrier strands 211, meaning each of the cavities 213 is spaced apart from the load carrier strands 211, in any direction from the longitudinal axis L, within the resin coating 212. Each of the plurality of cavities 213 encloses a material, which may be a solid, a liquid, or a gas, having a greater deformability than the deformability of the surrounding resin coating 212. The plurality of cavities 213 may account for approximately one third of the total volume of the resin coating 212, although the ratio of the volume of the cavities 213 to the total volume of the resin coating 212 may be adjusted to attain various levels of stress reduction in the composite elevator belt 100, as will be described in detail below with reference to
As shown in
Each cavity 213 in the compression zone CZ of the composite elevator belt 100 deforms by retracting or shortening along its first axis BX and lengthening or extending along its second axis BY. Deformation of the cavities 213 reduces or neutralizes the compression loads experienced by the load carrier strands 211 in the compression zone CZ by allowing the load carrier strands 211 to reposition within the outer layer 210 to a state of reduced stress. The lengthening of each cavity 213 along its second axis BY exerts a normal force FN on the load carrier strands 211 in a radial direction perpendicular to the longitudinal axis L. The normal forces FN exerted by the cavities 213 on opposite sides of the load carrier strands 211 counteract or neutralize the compressive stress experienced by the load carrier strands 211 due to bending the composite elevator belt 100 about the axis A. More specifically, the normal forces FN exerted by the cavities 213 induce the load carrier strands 211 into an undulating curve bending at least partially around the deformed cavities 213. Because an undulating curve inherently has a greater length than a similarly situated smooth curve, inducing the load carrier strands 211 into the undulating curve increases the length of each load carrier strand 211 in the compression zone CZ. The load carrier strands 211 may stretch to attain the increased length of the undulating curve in the compression zone CZ, thus subjecting the load carrier strands 211 to tensile stress which counteracts, and preferably exceeds, the compressive stress due to bending about the axis A. Reduction or elimination of the of the compressive stress on the load carrier strands 211 in the compression zone CZ allows the composite elevator belt 100 to attain a tighter bend radius without exceeding the maximum allowable internal compression. Additionally, replacement of the compressive stress in the load carrier strands 211 with tensile stress eliminates the risk of localized buckling failure and, as the materials used in the load carrier strands 211 are generally much stronger in tension than compression, the load carrier strands 211 may be expected to exhibit a longer service and fatigue life.
In contrast to the cavities 213 in the compression zone CZ, the cavities 213 in the tension zone TZ deform by lengthening or extending along their first axes BX and retracting or shortening along their second axes BY as the composite elevator belt 100 bends about the axis A. Retraction of the cavities 213 along their second axes BY decreases the radial thickness of the resin coating 212 in the tension zone TZ, thereby shifting the load carrier strands 211 in the tension zone TZ closer to the neutral bending zone NZ. By moving closer to the neutral bending zone NZ, the tensile stress experienced by the load carrier strands 211 in the tension zone TZ is reduced. Consequently, the service and fatigue life of the load carrier strands 211 in the tension zone TZ is increased.
The deformation of the cavities 213 is shown in greater detail in
Referring now to
The composite elevator belts 100 are further routed around drive sheaves 1210 rotatable by at least one motor arrangement 1200. The drive sheaves 1210 frictionally engage the composite elevator belts 100 between opposing ends of the composite elevator belts 100 such that rotation of the drive sheaves 1210 increases or decreases the length of the composite elevator belts 100 between a first end the of the composite elevator belt 100 and the motor arrangement 1200. Rotation of the drive sheaves 1210 thus causes the elevator car 700 to raise or lower depending on the direction of rotation of the drive sheaves 1210 and the arrangement of the counterweight, end terminations 900, and elevator sheaves 400.
As may be appreciated from the elevator system 1000 of
Having described the structure and function of the composite elevator belt 100, one skilled in the art will appreciate that a variety of materials may lend themselves to use for the various components thereof. Examples of suitable materials are generally described below and are further discussed in U.S. patent application Ser. No. 13/092,391, published as U.S. Patent Application Publication No. 2011/0259677, the entirety of which is incorporated by reference herein. Materials may be selected for their advantageous mechanical properties as well as for their compatibility with manufacturing methods suitable for making the composite elevator belt 100.
The load carrier strands 211, 221 of the at least one outer layer 210 and the central layer 220 may be made from a variety of natural and synthetic materials which are flexible yet exhibit a high breaking strength. Suitable materials for the load carrier strands 211, 221 thus include glass fiber, aramid fiber, carbon fiber, nylon fiber, basalt fiber, metallic cable, and/or combinations thereof. Some methods of manufacturing the composite elevator belt 100 may utilize inductive heating of the load carrier strands 211, 221, making it advantageous that the material of the load carrier strands 211, 221 is electrically conductive. The load carrier strands 211, 221 may each have a diameter of, for example, between 0.4 μm and 1.2 μm, such as 0.7 μm.
The resin coating 212, 222 may be made of a polymer matrix material, such as a curable epoxy resin, suitable for deposition on the load carrier strands 211, 221 and flexible when cured. However, alternative resin types may also be utilized. The resin coating 212, 222 may include additives such as fire retardants and release agent to improve the functionality and/or the manufacturing process of the resin coating 212, 222. The material of the resin coating 212, 222 may be selected based on its curing properties, such as the curing rate and the responsiveness of the curing rate to heat. Additionally, the material of the resin coating 212 of the outer layers 210 may be selected for its intermixibility with additives used to form the plurality of cavities 213, as will be described in greater detail below. The material of the resin coating 212 of the outer layers 210 may also be selected to reduce stiffness. In particular, the inclusion of the plurality of cavities 213 in the resin coating 212 may allow for the use of material having a Young's modulus of less than approximately 2 gigapascal (approximately 290,000 pounds per square inch). That is, the combined Young's modulus of the resin coating 212, taking into account the plurality of cavities 213 and any additives contained therein, may have an overall Young's modulus of approximately 2 gigpascal (GPa). The material of the resin coating 212, 222 is preferably a thermoset, or partly a thermoset and thermoplastic, or a thermoplastic material. The curing process is preferably activated by heat, or an electron beam, or ultraviolet light. The Young's modulus of the resin coating 212, 222 is preferably between 300 megapascal (MPa) and 4000 MPa. Most preferably, the Young's modulus is around 1700 MPa, i.e. 1.7 GPa.
As briefly described above, the material enclosed by each of the plurality of cavities 213 may be any of a solid, a liquid, or a gas. The operative physical property of the material is that the material permits deformation of the associated cavity 213 under tension and compression loading of the composite elevator belt 100. In some embodiments, the material enclosed by each of the cavities 213 may be a gas pocket produced by a blowing agent activated during manufacturing of the resin coating 212 of the outer layer 210. For example, a chemical blowing agent such as azodicarbonamide may be heated during manufacturing of the resin coating 212 to decompose the azodicarbonamide into gases which become trapped in the resin coating 212 as the resin coating 212 cures, defining the cavities 213 around discrete gas pockets created by the azodicarbonamide. In other embodiments, the material enclosed by each of the cavities 213 may be a deformable solid. In still other embodiments, the material enclosed by each of the cavities 213 may be a pocket of liquid.
Some of the plurality of cavities 213 may enclose a different material than other of the plurality of cavities 213. In embodiments of the composite elevator belt 100 having more than one outer layer 210, each outer layer 210 may utilize the same or a different material in the cavities 213. Each of the plurality of cavities 213 may have a diameter or outer dimension of, for example, between one-half and twice the diameter of the load carrier strands 211 in the associated outer layer 210.
The jacket layer 300 may be made of a polymer material selected for flexibility and to promote friction with the sheaves 400 and drive sheaves 1200 of the elevator system 1000. Additionally, the material of the jacket layer 300 may be selected for wear resistance of the jacket layer 300 and/or to prevent galling and other damage to the sheaves 400 and drive sheaves 1200. Suitable materials for the jacket layer 300 thus include curable resins such as urethanes, in particular thermoplastic polyurethane (TPU). The material of the jacket layer 300 may be softer than the material of the load carrier 200 by, for example, a factor of ten.
Other embodiments of the present disclosure are directed to a method of manufacturing the composite elevator belt 100 described with reference to
The liquid resin in the second and third injection chambers 2200b, 2200c may be intermixed with an additive suitable for forming the plurality of cavities 213 in the resin coating 212. In some embodiments, the additive may be a blowing agent, such as azodicarbonamide, which decomposes into gas during the subsequent curing of the liquid resin. In other embodiments, the additive may be solid particles, liquid particles, or gas particles. The amount or volume of the chosen additive intermixed with the liquid resin may be governed to control the total volume of the cavities 213 ultimately defined in the finished resin coating 212. Measures may be undertaken to ensure that the additive is homogenously intermixed with the liquid resin so that the cavities 213 are subsequently defined having substantially uniform spacing in the finished resin coating 212. In some embodiments, the load carrier strands 211, 221 may be coated with an additive, such as a blowing agent, prior to being pulled into the injection chambers 2200a, 2200b, 2200c, alternatively or in addition to the additive intermixed with the liquid resin.
After the load carrier strands 211, 221 of the outer layers 210 and the central layer 220 are impregnated with liquid resin, the load carrier strands 211, 221 are pulled out of the injection chambers 2200a-2200c and into a forming and curing die 2300 where the outer layer 210 and central layer 220 are joined together. When entering the forming and curing die 2300, the liquid resin impregnating the load carrier strands 211, 221 remains in an at least partially liquid phase to facilitate adhesion of the outer layers 210 to the central layer 220. Within the forming and curing die 2300, final shaping of the outer layers 210 and the central layer 220 is performed, and the liquid resin impregnating the load carrier strands 211, 221 is cured to form the resin coatings 212, 222 of the outer layers 210 and central layer 220. Curing of the resin coatings 212, 222 may be achieved, for example, by induction heating of the load carrier strands 211, 221 and/or the liquid resin.
In embodiments of the composite elevator belt 100 in which a blowing agent is intermixed with the liquid resin of the outer layers 210, the forming and curing die 2300 may also provide heat to decompose the blowing agent prior to or concurrently with the curing of the resin coating 212 of the outer layers 210. Decomposition of the blowing agent forms gas pockets around which the cavities 213 of the resin coating 212 are defined as the resin coating 212 cures. Similarly, in embodiments of the composite elevator belt 100 in which solid particles and/or liquid particles are intermixed with the liquid resin of the outer layers 210, the resin coating 212 cures around the liquid particles and/or solid particles to define the cavities 213.
After curing is completed in the forming and curing die 2300, the load carrier 200, now including all of the outer layers 210 and the central layer 220 joined together, may optionally be pulled through a jacket extruder 2400 which deposits the jacket layer 300 onto external surfaces of the load carrier 100. The composite elevator belt 100 exits the jacket extruder 2400 fully formed.
A tractor 2500 located downstream of the jacket extruder 2400 and/or the forming and curing dies 2300 applies a pulling force to unwind the load carrier strands 211, 221 from the roving coil racks 2100a-2100c and pull the load carrier strands 211, 221 through the injection chambers 2200a-2200c, the forming and curing die 2300, and, optionally, the jacket extruder 2400. The finished composite elevator belt 100 is then wound into a spool by a spooler 2600.
Utilizing the apparatus 2000 described above, a method for making a composite elevator belt 100 includes partially forming the at least one outer layer 210 of the load carrier 100 by impregnating the load carrier strands 211 of the at least one outer layer 210 with liquid resin in the second and third injection chambers 2100b, 2100c. The liquid resin in the second and third injection chambers 2100b, 2100c may be intermixed with an additive selected from a group consisting of deformable materials and blowing agents. The central layer 220 of the load carrier 100 may be formed in substantially the same manner as the outer layers 210, namely by impregnating the load carrier strands 221 of the central layer 220 with liquid resin in the first injection chamber 2100a. The outer layers 210 and the central layer 220 may then be pulled from the forming and curing die 2300 to join the outer layers 210 to the central layer 220 and cure the liquid resin of the outer layers 210 and the central layer 220. Curing the liquid resin of the outer layers 210 forms a solid resin coating defining the plurality of cavities 213 around the additive intermixed with the liquid resin.
While the apparatus 2000 and method described above provide one embodiment for manufacturing the composite elevator belt 100, variations may be made to suit the requirements of a particular application. For example, the central layer 220, which, in the present embodiment, lacks the plurality of cavities 213 present in the outer layers 210, may be at least partially formed using a different process than the outer layers 210, or the central layer 220 may be pre-manufactured and joined to the partially-formed outer layers 210 in the forming and curing die 2300. In other embodiments, the central layer 220 may be made similarly to the outer layers 210 such that cavities 213 are formed in the central layer 220 in addition to the outer layers 210. In still other embodiments, additional tooling may be added to the apparatus 2000 to perform additional forming operations to the composite elevator belt 100, or to add further layers to the composite elevator belt 100. In still other embodiments, the load carrier 200 may include an outer layer 210 on only one side of the central layer 220, or the load carrier 200 may include multiple outer layers 210 stacked on and joined with each other on any side or sides of central layer 220.
A first jacket layer 50 is provided and extends parallel to the resin coating 212 in the longitudinal direction L. The first jacket layer 50 is spaced apart from the resin coating 212 by the first plurality of teeth 30 and is associated with the tip portions 33 of each of the first plurality of teeth 30. Between each adjacent pair of the first plurality of teeth 30, a transverse groove is defined by the top surface 21 of the core layer 212, a bottom surface 52 of the first jacket layer 50, and the flanks 31 of the adjacent teeth 30. Similarly, a second jacket layer 60 is provided and extends parallel to the resin coating 212 in the longitudinal direction L. The second jacket layer 60 is spaced apart from the resin coating 212 by the second plurality of teeth 40 and is associated with the tip portions 43 of each of the second plurality of teeth 40. Between each adjacent pair of the second plurality of teeth 40, a transverse groove is defined by the bottom surface 22 of the resin coating 212, a top surface 61 of the second jacket layer 60, and the flanks 41 of the adjacent teeth 40. These transverse grooves are void of resin coating 212 and jacket layer 50, 60 material. A top surface 51 of the first jacket layer 50 and a bottom surface 62 of the second jacket layer 60 define contact surfaces of the composite elevator belt 100 and are configured for tractive, frictional engagement with a running surface of a sheave 400 or drive sheave.
The resin coating 212 defines a plurality of deformable cavities 213 interspersed throughout. The plurality of deformable cavities 213 are positioned adjacent to the load carrier strands 211, meaning each of the cavities 213 is spaced apart from the load carrier strands 211, in any direction from the longitudinal axis L, within the resin coating 212. Each of the plurality of cavities 213 encloses a material, which may be a solid, a liquid, or a gas, having a greater deformability than the deformability of the surrounding resin coating 212. The plurality of cavities 213 may account for approximately one third of the total volume of the resin coating 212, although the ratio of the volume of the cavities 213 to the total volume of the resin coating 212 may be adjusted to attain various levels of stress reduction in the composite elevator belt 100, as described in detail with reference to
Each individual strand 211, or a group of strands G2, G4, G6 can be treated with a further material 27, preferably they are treated with this further material 27 before they are covered by the resin coating 212. The further material 27 can be applied to each strand 211 individually or to a group of strands G2, G4, G6. The further material 27 can be selected from the group consisting of: a resin material, a polymer matrix material, an adhesive material, e.g., sizing, a thermoset material, a thermoplastic material, or any combination thereof. The strands 10 shown in example
The example shown in
Each individual strand 211 or each individual group of strands G1, G3 can be treated with a further material 27, preferably they are treated with this further material 27 before they are covered by the resin coating 212. The further material 27 can be applied to each strand 211 individually or to a group of strands G1, G3. The further material 27 can be selected from the group consisting of: a resin material, a polymer matrix material, an adhesive material, e.g., sizing, a thermoset material, a thermoplastic material, or any combination thereof. The strands 211 shown in example
The example shown in
The resin coating 212 defines a plurality of deformable cavities 213 interspersed throughout. The plurality of deformable cavities 213 are positioned adjacent to the load carrier strands 211, meaning each of the cavities 213 is spaced apart from the load carrier strands 211, in any direction from the longitudinal axis L, within the resin coating 212. Each of the plurality of cavities 213 encloses a material, which may be a solid, a liquid, or a gas, having a greater deformability than the deformability of the surrounding resin coating 212. The plurality of cavities 213 may account for approximately one third of the total volume of the resin coating 212, although the ratio of the volume of the cavities 213 to the total volume of the resin coating 212 may be adjusted to attain various levels of stress reduction in the composite elevator belt 100, as described in detail with reference to
Each individual strand 211, or each individual group of strands G02, G04, G06 can be treated with a further material 27, preferably they are treated with this further material 27 before they are covered by the resin coating 212. The further material 27 can be applied to each strand 211 individually or to a group of strands G02, G04, G06. The further material 27 can be selected from the group consisting of: a resin material, a polymer matrix material, an adhesive material, e.g., sizing, a thermoset material, a thermoplastic material, or any combination thereof. The strands 211 shown in example
The example shown in
Each individual strand 211 or each individual group of strands G01, G03 can be treated with a further material 27, preferably they are treated with this further material 27 before they are covered by the resin coating 212. The further material 27 can be applied to each strand 211 individually or to a group of strands G01, G03. The further material 27 can be selected from the group consisting of: a resin material, a polymer matrix material, an adhesive material, e.g., sizing, a thermoset material, a thermoplastic material, or any combination thereof. The strands 211 shown in example
The example shown in
In each of the examples illustrated in
The distribution of strands 211 in
The distribution of strands 211 in
The load carrier 200 cross-sections depicted in any of
A first jacket layer 50 is provided and extends parallel to the resin coating 212 in the longitudinal direction L. The first jacket layer 50 is spaced apart from the resin coating 212 by the first plurality of teeth 30 and is associated with the tip portions 33 of each of the first plurality of teeth 30. Between each adjacent pair of the first plurality of teeth 30, a transverse groove is defined by the top surface 21 of the resin coating 212, a bottom surface 52 of the first jacket layer 50, and the flanks 31 of the adjacent teeth 30. Similarly, a second jacket layer 60 is provided and extends parallel to the resin coating 212 in the longitudinal direction L. The second jacket layer 60 is spaced apart from the resin coating 212 the second plurality of teeth 40 and is associated with the tip portions 43 of each of the second plurality of teeth 40. Between each adjacent pair of the second plurality of teeth 40, a transverse groove is defined by the bottom surface 22 of the resin coating 212, a top surface 61 of the second jacket layer 60, and the flanks 41 of the adjacent teeth 40. These transverse grooves are void of resin coating 212 and jacket layer 50, 60 material. A top surface 51 of the first jacket layer 50 and a bottom surface 62 of the second jacket layer 60 define contact surfaces of the composite elevator belt 100 and are configured for tractive, frictional engagement with a running surface of a sheave 200 or drive sheave 1200 of the elevator system 1000.
A first jacket layer 50 is provided and extends parallel to the resin coating 212 in the longitudinal direction L. The first jacket layer 50 is spaced apart from the resin coating 212 by the first plurality of teeth 30 and is associated with the tip portions 33 of each of the first plurality of teeth 30. Between each adjacent pair of the first plurality of teeth 30, a transverse groove is defined by the top surface 21 of the resin coating 212, a bottom surface 52 of the first jacket layer 50, and the flanks 31 of the adjacent teeth 30. Similarly, a second jacket layer 60 is provided and extends parallel to the resin coating 212 in the longitudinal direction L. The second jacket layer 60 is spaced apart from the resin coating 212 the second plurality of teeth 40 and is associated with the tip portions 43 of each of the second plurality of teeth 40. Between each adjacent pair of the second plurality of teeth 40, a transverse groove is defined by the bottom surface 22 of the resin coating 212, a top surface 61 of the second jacket layer 60, and the flanks 41 of the adjacent teeth 40. These transverse grooves are void of resin coating 212 and jacket layer 50, 60 material. A top surface 51 of the first jacket layer 50 and a bottom surface 62 of the second jacket layer 60 define contact surfaces of the composite elevator belt 100 and are configured for tractive, frictional engagement with a running surface of a sheave 200 or drive sheave 1200 of the elevator system 1000.
The resin coating 212 defines a plurality of deformable cavities 213 interspersed throughout. The plurality of deformable cavities 213 are positioned adjacent to the load carrier strands 211, meaning each of the cavities 213 is spaced apart from the load carrier strands 211, in any direction from the longitudinal axis L, within the resin coating 212. Each of the plurality of cavities 213 encloses a material, which may be a solid, a liquid, or a gas, having a greater deformability than the deformability of the surrounding resin coating 212. The plurality of cavities 213 may account for approximately one third of the total volume of the resin coating 212, although the ratio of the volume of the cavities 213 to the total volume of the resin coating 212 may be adjusted to attain various levels of stress reduction in the composite elevator belt 100, as described in detail with reference to
The central layer 220 may include one or more load carrier strands 221 arranged parallel to and continuous along the longitudinal axis L of the composite elevator belt 100. In other embodiments, the load carrier strands 221 may be interrupted along the longitudinal axis L, and may or may not overlap one another. In still other embodiments, the load carrier strands 221 may be arranged in multiple layers spaced apart from one another in a direction perpendicular to the longitudinal axis L. In still other embodiments, the load carrier strands 221 may be entangled, discontinuous fibers arranged in a mat or roving. The one or more load carrier strands 221 may be encased in a resin coating 222, which defines a cross-sectional profile of the central layer 220 and fills any voids between the load carrier strands 221. The resin coating 222 may be substantially free of any voids or impurities except for those unintentionally introduced during the manufacturing of the central layer 220. The one or more load carrier strands 221 may account for between approximately 60% and approximately 80% of the total volume of the central layer 220. However, the volume ratio of the load carrier strands 221 to the total volume of the central layer 220 may be adjusted to balance the strength and flexibility of the composite elevator belt 100 for a particular application. Generally, increasing the volume ratio of the load carrier strands 221 to the total volume of the central layer 220 increases the strength and decreases the flexibility of the composite elevator belt 100, while decreasing the volume ratio of the load carrier strands 221 to the total volume of the central layer 220 decreases the strength and increases the flexibility of the composite elevator belt 100.
As the at least one outer layer 210 may occupy either the compression zone CZ or the tension zone TZ of the composite elevator belt 100, the at least one outer layer 210 may be subject to greater loads due to bending than the central layer 220, which may be generally coincident with the neutral bending zone NZ. As such, the ratio of the volume of the load carrier strands 211 of each outer layer 210 to the total volume of that outer layer 210 may be less than the ratio of the volume of the load carrier strands 221 of the central layer 220 to the total volume of the central layer 220. The resin coating 212 of each outer layer 210 defines a plurality of deformable cavities 213 interspersed throughout. The plurality of deformable cavities 213 are positioned adjacent to the load carrier strands 211, meaning each of the cavities 213 is spaced apart from the load carrier strands 211, in any direction from the longitudinal axis L, within the resin coating 212. Each of the plurality of cavities 213 encloses a material, which may be a solid, a liquid, or a gas, having a greater deformability than the deformability of the surrounding resin coating 212. The plurality of cavities 213 may account for approximately one third of the total volume of the resin coating 212, although the ratio of the volume of the cavities 213 to the total volume of the resin coating 212 may be adjusted to attain various levels of stress reduction in the composite elevator belt 100, as described in detail with reference to
Other embodiments of the present disclosure are directed to a method of manufacturing the composite elevator belt 100 described with reference to
The liquid resin in the second and third injection chambers 2200b, 2200c may be intermixed with an additive suitable for forming the plurality of cavities 213 in the resin coating 212. In some embodiments, the additive may be a blowing agent, such as azodicarbonamide, which decomposes into gas during the subsequent curing of the liquid resin. In other embodiments, the additive may be solid particles, liquid particles, or gas particles. The amount or volume of the chosen additive intermixed with the liquid resin may be governed to control the total volume of the cavities 213 ultimately defined in the finished resin coating 212. Measures may be undertaken to ensure that the additive is homogenously intermixed with the liquid resin so that the cavities 213 are subsequently defined having substantially uniform spacing in the finished resin coating 212. In some embodiments, the load carrier strands 211, 221 may be coated with an additive, such as a blowing agent, prior to being pulled into the injection chambers 2200a, 2200b, 2200c, alternatively or in addition to the additive intermixed with the liquid resin.
After the load carrier strands 211, 221 of the outer layers 210 and the central layer 220 are impregnated with liquid resin, the load carrier strands 211, 221 are pulled out of the injection chambers 2200a-2200c and into a forming and curing die 2300 where the outer layer 210 and central layer 220 are joined together. When entering the forming and curing die 2300, the liquid resin impregnating the load carrier strands 211, 221 remains in an at least partially liquid phase to facilitate adhesion of the outer layers 210 to the central layer 220. Within the forming and curing die 2300, final shaping of the outer layers 210 and the central layer 220 is performed, and the liquid resin impregnating the load carrier strands 211, 221 is cured to form the resin coatings 212, 222 of the outer layers 210 and central layer 220.
Curing of the resin coatings 212, 222 may be achieved, for example, by induction heating of the load carrier strands 211, 221 and/or the liquid resin.
In embodiments of the composite elevator belt 100 in which a blowing agent is intermixed with the liquid resin of the outer layers 210, the forming and curing die 2300 may also provide heat to decompose the blowing agent prior to or concurrently with the curing of the resin coating 212 of the outer layers 210. Decomposition of the blowing agent forms gas pockets around which the cavities 213 of the resin coating 212 are defined as the resin coating 212 cures. Similarly, in embodiments of the composite elevator belt 100 in which solid particles and/or liquid particles are intermixed with the liquid resin of the outer layers 210, the resin coating 212 cures around the liquid particles and/or solid particles to define the cavities 213.
After curing is completed in the forming and curing die 2300, the load carrier 200, now including all of the outer layers 210 and the central layer 220 joined together, may optionally be pulled through a jacket extruder 2400 which deposits the jacket layer 300 onto external surfaces of the load carrier 100. The composite elevator belt 100 exits the jacket extruder 2400 fully formed.
A tractor 2500 located downstream of the jacket extruder 2400 and/or the forming and curing dies 2300 applies a pulling force to unwind the load carrier strands 211, 221 from the roving coil racks 2100a-2100c and pull the load carrier strands 211, 221 through the fiber arrangements 2700a, 2700b, 2700c; the cavity printer; 2800a, 2800b, 2800c; the cavity curing 2900a, 2900b, 2900c; the injection chambers 2200a-2200c; the forming and curing die 2300; and, optionally, the jacket extruder 2400. The finished composite elevator belt 100 is then wound into a spool by a spooler 2600.
Utilizing the apparatus 2000 described above, a method for making a composite elevator belt 100 includes partially forming the at least one outer layer 210 of the load carrier 100 by impregnating the load carrier strands 211 of the at least one outer layer 210 with liquid resin in the second and third injection chambers 2100b, 2100c. The liquid resin in the second and third injection chambers 2100b, 2100c may be intermixed with an additive selected from a group consisting of deformable materials and blowing agents. The central layer 220 of the load carrier 100 may be formed in substantially the same manner as the outer layers 210, namely by impregnating the load carrier strands 221 of the central layer 220 with liquid resin in the first injection chamber 2100a. The outer layers 210 and the central layer 220 may then be pulled from the forming and curing die 2300 to join the outer layers 210 to the central layer 220 and cure the liquid resin of the outer layers 210 and the central layer 220. Curing the liquid resin of the outer layers 210 forms a solid resin coating defining the plurality of cavities 213 around the additive intermixed with the liquid resin.
While the apparatus 2000 and method described above provide one embodiment for manufacturing the composite elevator belt 100, variations may be made to suit the requirements of a particular application. For example, the central layer 220, which, in the present embodiment, lacks the plurality of cavities 213 present in the outer layers 210, may be at least partially formed using a different process than the outer layers 210, or the central layer 220 may be pre-manufactured and joined to the partially-formed outer layers 210 in the forming and curing die 2300. In other embodiments, the central layer 220 may be made similarly to the outer layers 210 such that cavities 213 are formed in the central layer 220 in addition to the outer layers 210. In still other embodiments, additional tooling may be added to the apparatus 2000 to perform additional forming operations to the composite elevator belt 100, or to add further layers to the composite elevator belt 100. In still other embodiments, the load carrier 200 may include an outer layer 210 on only one side of the central layer 220, or the load carrier 200 may include multiple outer layers 210 stacked on and joined with each other on any side or sides of central layer 220.
The cavity curing 2900 shown in
While several examples of a composite elevator belt for an elevator system, as well as methods for making the same, are shown in the accompanying figures and described in detail hereinabove, other examples will be apparent to and readily made by those skilled in the art without departing from the scope and spirit of the present disclosure. For example, it is to be understood that aspects of the various embodiments described hereinabove may be combined with aspects of other embodiments while still falling within the scope of the present disclosure. Accordingly, the foregoing description is intended to be illustrative rather than restrictive. The assembly of the present disclosure described hereinabove is defined by the appended claims, and all changes to the disclosed assembly that fall within the meaning and range of equivalency of the claims are to be embraced within their scope.
Number | Date | Country | Kind |
---|---|---|---|
2018064854 | Jun 2018 | EP | regional |
Filing Document | Filing Date | Country | Kind |
---|---|---|---|
PCT/EP2018/082168 | 11/22/2018 | WO | 00 |