The present invention relates generally to apparatuses, systems, and methods for testing of a mattress system, and more particularly testing of mattress and/or foundation firmness and/or durability.
Construction of a mattress and foundation system and the internal components of the system can have different effects upon the performance and feel of a mattress. Metal springs, foam layers, water, air, and other structures have been employed in mattress constructions, both separately or in combination with one another. These different mattress constructions result in a range of product characteristics in a mattress that may be offered to a consumer. Different and new constructions of mattresses, whether through selection of materials, use of new materials, varying thickness of materials, or positioning of materials are continually being utilized in new mattress products.
Both manufacturers and consumers may desire to better characterize or understand the performance and qualities of a particular mattress. Mattresses are not a one-time-use type product and instead may be often used for many years. As a result, the performance of a mattress over its entire life cycle may be of interest.
Some conventional industry testing procedures exist to characterize certain features of a mattress, but such procedures may not fully simulate the typical use of a mattress over the course of its life. Thus, there is a need to provide systems and methods for determining characteristics of a mattress, including firmness and durability.
Described herein are various embodiments of apparatuses, systems, and methods for testing of a mattress system. In some embodiments, the apparatuses, systems, and methods comprise testing of a mattress system for firmness. In some embodiments, the apparatuses, systems, and methods comprise testing of a mattress system for durability or longevity of its life, and any of the components therein.
In some embodiments described herein, an apparatus for testing a mattress system comprises a robotic arm assembly and a mannequin. The mannequin can be coupled to the robotic arm assembly such that the robotic arm assembly can position the mannequin in a plurality of positions upon the mattress system.
In other embodiments described herein, a system for testing a mattress system comprises a robotic arm assembly, a mannequin, and an operating system. The robotic arm assembly can include an arm and an end-of-arm attachment. The mannequin can be coupled to the end-of-arm attachment. The operating system of the system can direct the movement of the robotic arm assembly and mannequin about the mattress system.
In yet other embodiments, a method of testing a mattress system is described herein. In some embodiments, a method for testing a mattress system comprises applying a force upon a mattress system using a mannequin, sliding the mannequin from a first edge of the mattress system to an inner region of the mattress system, and rotating the mannequin on a surface of the mattress system. In some embodiments, the method can be repeated a plurality of times.
These illustrative aspects and embodiments are mentioned not to limit or define the invention, but to provide examples to aid understanding of the inventive concepts disclosed in this application. Other aspects, advantages, and features of the present invention will become apparent after review of the entire application.
Certain aspects and embodiments described herein relate to apparatuses, systems, or methods that can be used to test a mattress system for firmness and/or durability. The term “mattress system” herein refers to a mattress, a foundation (also known as a box spring), and/or both a mattress and a foundation. As such, apparatuses, systems, or methods described herein relate to apparatuses, systems or methods that can be used to test a mattress only, that can be used to test a foundation only, and/or that can be used to test both a mattress and a foundation. In some embodiments, the apparatuses, systems, or methods can test the mattress system, including but not limited to its external components, internal components, surface firmness and pressures, edge support, foam fatigue, innerspring fatigue, surface material fatigue, foundation fatigue, material relaxation and migration, and/or any other quantifiable measurement which may be interpreted as representative of the product life cycle.
In some embodiments, the apparatuses and systems can simulate human motion or movements upon a mattress surface. Some embodiments of the robotic testing system described herein can direct a mannequin such that specific forces are exerted upon a mattress system that simulate forces exerted on a mattress system by typical human motions or movements during use of the mattress system.
In some embodiments, during the sequence of movements of the mannequin, the robotic testing system can measure different force load responses of the mattress system. In some embodiments, the measured forces can be used to characterize the firmness, durability, surface motion, and/or material migration of a mattress system.
In some embodiments, the robotic testing system can provide information concerning the durability of the mattress system based on simulated human movements. In some embodiments, the robotic testing system can replicate surface fatigue or migration that occurs over the extended use of a mattress system life cycle. In some embodiments, the mattress system can be analyzed upon the completion of a plurality of cycles by inspecting the performance of the components of a mattress system. In some embodiments, the robotic testing system may generate a repeatable, surface impression, or similar visual defect.
In some embodiments, an apparatus for testing a mattress system may comprise a robotic arm assembly and a mannequin. The robotic arm assembly can be operably connected to the mannequin. The robotic arm assembly can be directed to move the mannequin to a plurality of positions upon a mattress by way of different directions and types of movements.
The robotic arm assembly can comprise an arm and an end-of-arm structure configured to be coupled to a mannequin or other attachment. In some embodiments, the arm can have an extension reach such that the arm may reach appropriate regions or sections of conventional industry sized mattresses. In some embodiments, the length of reach and weight distribution or force exerted can vary dependent upon the desired test, size of mattress, or other factors. In some embodiments, the arm can be configured to exert a range of forces simulating those forces applied during human usage of a mattress system. In some illustrative embodiments, the arm can have an extension reach of at least 40 inches from its base. In some illustrative embodiments, the arm can exert up to 1000 pounds of force. In some illustrative embodiments, the arm can be configured to exert a minimum force of 350 pounds at a reach of 40 inches.
The end-of-arm structure of the robotic arm assembly can include an end-of-arm attachment capable of being adjusted in a plurality of directions and along a plurality of axes. In some embodiments, the end-of-arm attachment can be capable of being adjusted along at least six different axes. In some embodiments, the end-of-arm attachment can comprise a multi-axial load cell. In some embodiments, the end-of-arm attachment can be secured to a mannequin such that the mannequin can be positioned in a plurality of positions. The robotic arm assembly can direct the mannequin in a variety of movements including lateral movements, rotational movements, height adjustments, depth adjustments, and other like movements, all at a plurality of angles.
The mannequin may comprise different shapes and structures. In some embodiments, the mannequin can have various forms, such as a partial-body mannequin, a full-body mannequin, or any other shape. In some embodiments, the mannequin may comprise a body portion and leg portions. In other embodiments, the mannequin can simulate a waist region to the knee region of a human body. In some embodiments, a plurality of mannequins may be used.
In some embodiments, the mannequin may comprise at least one sensor. For example, the sensors can include accelerometers, pressure sensors, sensors to measure shear or torsion forces, and/or other like sensors. The sensors may be used to detect or measure movements or exerted forces during movement of the mannequin. Any collected data may be recorded via an operating system or computer. In some embodiments, the mattress system may include similar sensors to detect or measure different movements or forces in a similar fashion.
The weight and size of the mannequin can vary according to the preference and specifications of a testing protocol. In some embodiments, the mannequin can weigh from about 30 pounds to about 500 pounds. In some embodiments, the mannequin can weigh approximately 150 pounds. In some embodiments, the mannequin can be designed to simulate a specific percentile of the human population, for example, the 95th percentile.
In some embodiments, the end-of-arm attachment can comprise a multi-axial load cell. The multi-axial load cell can be operably coupled to the mannequin and the robotic arm assembly. In some embodiments, the coupling of the multi-axial load cell includes physical coupling as well as electrically coupling such that information may be transmitted via signals to and from the operating system. In some embodiments, the multi-axial load cell can be adjusted in a direction along at least six axes. In some embodiments, the multi-axial load cell can comprise at least one sensor. In some embodiments, the at least one sensor can measure the load response of force exerted by an end of the robotic arm assembly downward into the surface of a mattress system.
In some embodiments, the apparatus and systems described herein can comprise an operating system. In some embodiments, the operating system can comprise a computer having a processor and memory. The operating system can control and direct the movements of the robotic arm assembly and the mannequin. The operating system can include a processor having programmable code to direct a method or routine for the robotic arm assembly to follow during operation. The operating system can generate a plurality of signals to direct a sequence of movements of the robotic arm assembly.
In some embodiments, during operation of the apparatus and systems described herein, the end-of-arm attachment, for example the multi-axial load cell, can measure different stimuli and feedback generated as the robotic arm assembly is operated. In some embodiments, the stimuli and feedback data can be transmitted to the operating system for collection and storage. In some embodiments, the data can be processed and analyzed to determine different characteristics of the tested mattress system.
In some embodiments, the data provided by the load cell can be analyzed by the operating system such that the movement of the robotic arm assembly can be adjusted or altered automatically depending on the force response of the load cell. In some embodiments, a feedback loop can be utilized to direct the specific movement of the robotic arm assembly. The load cell can use a sensor to measure the output performance of the robotic arm assembly which can then in turn be used to give feedback to the operating system. The operating system may make adjustments or alterations of the movement of the robotic arm assembly to a desired or defined movement.
In some embodiments, the load cell can measure certain stimuli, signals, or data which can then be transmitted or communicated to the operating system. The operating system can comprise a processor and memory such that upon receipt of the data by the operating system, the data can be analyzed in real time. The operating system can then direct the robotic arm assembly to move in a specified manner based upon the analysis of the data by the operating system. In some embodiments, the feedback loop may more closely simulate human movement as a human may adjust or alter her movement dependent upon the feedback from the mattress system.
Referring to the Figures, the numbers used within each figure are consistent with every other figure. When a specific feature is labeled in one figure with a specific numeral, the same numeral will be used in other figures when denoting that specific feature.
The multi-axial load cell 18 is operably connected to the mannequin 11. In some embodiments, the multi-axial load cell 18 can comprise at least one sensor that can collect or measure certain stimuli or feedback generated during the operation of the system 10. For example, the multi-axial load cell 18 can include a sensor that collects the load response of a force exerted by the end of the arm 13 downward into the top surface of the mattress 16. The collected data can then be transmitted to the operating system 15.
In a first position shown in
In a second position shown in
In a third position shown in
In a fourth position shown in
In a fifth position shown in
In a sixth position shown in
At each position shown in
After the mannequin 11 reaches the position shown in
In some embodiments, methods for testing a mattress system using the robotic testing system are described herein. In some embodiments, the method can comprise applying a force upon a mattress system via a mannequin, positioning the mannequin in an inner region of the mattress via a sliding movement, and rotating the mannequin on a surface of the mattress system. In some embodiments, the force can be applied upon a first edge of a mattress system. In other embodiments, the force can be applied to other portions of a mattress system, including an inner region. In some embodiments, the robotic arm assembly can apply a substantially constant force upon the mattress system at certain times or with certain movements. In some embodiments, the force can be in a range from approximately 50 to approximately 400 pounds. In other embodiments, the force can be approximately 200 pounds.
In some embodiments, the method can include positioning the mannequin in a second position in the inner region of the mattress system. In some embodiments, the mannequin can be moved via a sliding movement to a plurality of positions. In some embodiments, the mannequin can be positioned in a reclining position to simulate a human reclining on a mattress system in a horizontal orientation.
In some embodiments, the rotating the mannequin on a surface of the mattress step can include rotating the mannequin from a first orientation to a second orientation. In some embodiments, the mannequin can be rotated approximately 90 degrees.
In some embodiments, the movements of the mannequin can be reversed to simulate a person getting up after use of the mattress system. Some such methods can include rotating the mannequin from the second orientation to the first orientation, positioning the mannequin, being in the first orientation, to the first edge of the mattress system, and removing the force from the first edge of the mattress system by lifting the mannequin such that the mannequin does not contact the mattress system.
In some embodiments, the method can comprise holding the mannequin at specific points during the sequence of steps for a defined period of time. For example, after the mannequin has been rotated to the second orientation, the mannequin can remain stationary for approximately twenty seconds, or some other defined period of time.
In some embodiments, the method can be repeated a plurality of times to simulate repeated use of the mattress system by a human.
Some embodiments described herein can be used to measure the firmness of a mattress system, including but not limited to its external components, internal components, surface firmness and pressures, edge support, foam fatigue, innerspring fatigue, surface material fatigue, foundation fatigue, material relaxation and migration, or any other quantifiable measurement which may be interpreted as representative of the product life cycle. Some embodiments described herein can be used to determine the durability of a mattress system, including but not limited to its external components, internal components, surface firmness and pressures, edge support, foam fatigue, innerspring fatigue, surface material fatigue, foundation fatigue, material relaxation and migration, or any other quantifiable measurement which may be interpreted as representative of the product life cycle. The application of a repeated load by way of the robotic arm assembly may provide a more accurate reproduction of the forces applied to a mattress system by a human during usage, as compared to conventional load or impact tests. The robotic testing system can measure the load response of the mattress system as a result of the force extended by the end-of-arm attachment downward on the surface of the mattress system. Such measurements can be used to evaluate the performance of a mattress system over time and any changes in the performance of the mattress system as a result of normal human use.
In some embodiments, the robotic testing system can comprise a second mannequin. The second mannequin can be positioned upon a surface of a mattress system in a second region of the mattress system. In some embodiments, the second mannequin can include at least one sensor. In some embodiments, the second mannequin can measure or detect motion transfer or other forces applied upon the second mannequin as a result of movements of the first mannequin attached to a robotic arm assembly. In some embodiments, the second mannequin can be coupled to the robotic arm assembly. In other embodiments, the second mannequin may not be coupled to the robotic arm assembly. The second mannequin can be operably coupled to an operating system that can collect and store data from the second mannequin or its sensors.
The foregoing description of the embodiments, including illustrated embodiments, of the systems and products have been presented for the purpose of illustration and description and is not intended to be exhaustive or to limit the invention to the precise systems or forms disclosed. Numerous modifications, adaptations, and uses thereof will be apparent to those skilled in the art without departing from the scope of the description herein.
Number | Name | Date | Kind |
---|---|---|---|
5798703 | Sakai et al. | Aug 1998 | A |
7036164 | Dickerson | May 2006 | B2 |
7520836 | Couvillion et al. | Apr 2009 | B2 |
7712640 | Honer et al. | May 2010 | B2 |
8123685 | Brauers et al. | Feb 2012 | B2 |
20040003669 | Gladney et al. | Jan 2004 | A1 |
20080078030 | Lee et al. | Apr 2008 | A1 |
Number | Date | Country | |
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20140053653 A1 | Feb 2014 | US |