Hollow article with pillar structural members
10357934 ยท 2019-07-23
Assignee
Inventors
Cpc classification
B29C49/4268
PERFORMING OPERATIONS; TRANSPORTING
B32B3/28
PERFORMING OPERATIONS; TRANSPORTING
B32B2264/065
PERFORMING OPERATIONS; TRANSPORTING
B32B27/302
PERFORMING OPERATIONS; TRANSPORTING
B29C49/22
PERFORMING OPERATIONS; TRANSPORTING
B29C49/4815
PERFORMING OPERATIONS; TRANSPORTING
B32B7/05
PERFORMING OPERATIONS; TRANSPORTING
B32B3/02
PERFORMING OPERATIONS; TRANSPORTING
B32B25/04
PERFORMING OPERATIONS; TRANSPORTING
Y10T428/24149
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
B32B2264/104
PERFORMING OPERATIONS; TRANSPORTING
International classification
B32B3/12
PERFORMING OPERATIONS; TRANSPORTING
B32B25/04
PERFORMING OPERATIONS; TRANSPORTING
B29C49/42
PERFORMING OPERATIONS; TRANSPORTING
B29C49/22
PERFORMING OPERATIONS; TRANSPORTING
B32B7/05
PERFORMING OPERATIONS; TRANSPORTING
B32B3/28
PERFORMING OPERATIONS; TRANSPORTING
B32B3/02
PERFORMING OPERATIONS; TRANSPORTING
B32B27/30
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A hollow article is provided, comprising a first wall and a second wall, where the first and second walls are positioned in opposing relationship and define a space therebetween. A plurality of protruding structural pillars extend from the second wall and span the space, each of the structural pillars having an end surface integrally bonded with an inside surface of the first wall.
Claims
1. A hollow blow-molded article comprising: a first wall; a second wall, wherein said first and second walls are positioned in opposing relationship and define a space therebetween; a reinforcement layer integrally bonded to at least a portion of an outside surface of said first wall; and a plurality of structural pillars formed as extensions of said second wall that protrude into said space, each of said structural pillars spanning said space and having an end surface integrally bonded with an inside surface of said first wall, wherein the plurality of structural pillars are arranged in a geometric array with said geometric array including at least one region of structural pillars in a high density arrangement and at least one region of structural pillars in a low density arrangement to achieve a desired structural rigidity of the hollow blow-molded article.
2. The hollow blow-molded article of claim 1, wherein each of said structural pillars has a hollow core.
3. The hollow blow-molded article of claim 1, wherein each of said structural pillars has a solid core.
4. The hollow blow-molded article of claim 1, wherein each of said structural pillars has a partially hollow core.
5. The hollow blow-molded article of claim 1, wherein said geometric array is selected from the group consisting of rectangular, equidistant collinear, triangular, hexagonal, and combinations thereof.
6. The hollow blow-molded article of claim 1, wherein said geometric array is arranged such that linear patterns defined by the structural pillars are non-parallel to one or more edgewalls of the hollow blow-molded article.
7. The hollow blow-molded article of claim 1, wherein a covering is integrally bonded to said reinforcement layer.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) The foregoing and other features and advantages of the invention will be apparent from the following description of the invention as illustrated in the accompanying drawings. The accompanying drawings, which are incorporated herein and form a part of the specification, further serve to explain the principles of the invention and to enable a person skilled in the pertinent art to make and use the invention. The drawings are not to scale.
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DETAILED DESCRIPTION OF EMBODIMENTS OF THE PRESENT INVENTION
(36) Specific embodiments of the present invention will now be described with reference to the Figures, wherein like reference numbers indicate identical or functionally similar elements. The following detailed description is merely exemplary in nature and is not intended to limit the invention or the application and uses of the invention. A person skilled in the relevant art will recognize that other configurations and arrangements can be used without departing from the scope of the invention. Although the description and drawings of the embodiments hereof exemplify the formation/use of structural pillars in load floors, the invention may also be used in other molding arrangements where it is deemed useful. Furthermore, there is no intention to be bound by any expressed or implied theory presented in the preceding technical field, background, brief summary or the following detailed description.
(37) Turning now to
(38) To provide enhanced structural rigidity between first and second walls 12, 14 hollow article 10 is further provided with a plurality of tack off structures, each generally referred to herein as a structural pillar 18. As will be detailed below, structure pillar 18 is formed as an extension of second wall 14, and is dimensioned to span the separation between first and second walls 12, 14 such that the tip face of structural pillar 18 engages and bonds with the inside surface of first wall 12. As such, each structural pillar 18 provides a fixed attachment between first and second walls 12, 14.
(39) Structural pillar 18 may be presented in a number of forms, depending on the process of manufacture and desired performance requirement. For example, structural pillar 18 may be provided as a hollow structural pillar 18 as shown in
(40) As indicated above, structural pillar 18 is provided in the form of a plurality of structural pillars arranged in a pattern, generally but not limited to a geometric array, within hollow article 10 between first and second walls 12, 14. Exemplary structural pillar arrangement patterns in a hollow article 10 are shown in
(41) In some applications, it is desirable to have a covering material applied to one side of the hollow structure. For example, it may be desirable to apply a carpet material to one side of the hollow structure so as to meet desired performance and/or aesthetics characteristics. As such, provided in
(42) In addition or as an alternative to covering 34, one or more reinforcement layers may be integrally bonded to outside surface 36 of first wall 12. In the embodiment shown in
(43) A process for manufacturing the hollow structure having a carpet covering provided on one surface will now be presented having regard to
(44) Provided in second mold half 46 are a plurality of slidably displaceable core pins 52 for forming structural pillars 18. Core pins 52 are configured to protrude and retract from mold cavity 48 so as to form the above-mentioned extensions of second wall 14, each defining a corresponding structural pillar 18. To facilitate movement of core pins 52, core pins 52 are coupled to a common yoke plate 54 capable of lateral displacement through the action of one or more actuators 56. As will be appreciated, the stroke provided by the one or more actuators may be adjustable for allow for accurate positioning of end surface 58 of core pin 52 relative to the fully extended and fully retracted positions. For example, in the retracted position, end surface 58 may be partially protruding, flush, or partially recessed from cavity surface 60 to provide for desired finished product surface characteristics. It will be further appreciated that while a single yoke plate may be used to control the plurality of core pins, multiple yoke plates may be implemented to control banks or groupings of core pins. Still further, in some embodiments, each core pin may be controlled by an independent actuator.
(45) Continuing with
(46) Partial mold tool 42 closure is represented in
(47) As shown in
(48) On completion of the blow molding step, as shown in
(49) Turning now to
(50) Shown in
(51) Provided in second mold half 146 are a plurality of slidably displaceable core pins 152 for forming structural pillars 18. Core pins 152 are coupled to a yoke plate 154 capable of lateral displacement through the action of one or more actuators 156, permitting core pins 152 to be protruded and retracted from cavity 148. As detailed in
(52) Yoke plate 154 is configured with a series of conduits 184 to connect internal channels 180 of core pins 152 to a suitable air pump/vacuum device 186 through plenum 188 coupled to yoke plate 154. Yoke plate 154 and/or core pins 152 may be provided with suitable seals (not shown) to prevent egress of air during use. In other embodiments, yoke plate 154 may be configured with a network of channels to form a manifold capable of delivering air from a suitable air pump/vacuum device coupled directly thereto.
(53) Parison 50 is positioned between first and second mold halves 144, 146 of mold tool 142, with covering 34 being positioned between first mold half 144 and parison 50. Either prior to mold tool 142 closure, simultaneously with mold tool 142 closure, or subsequent to mold tool 142 closure, yoke plate 54 is displaced towards second mold half 46 so as to protrude core pins 152 from the cavity surface 160. In the embodiment shown, core pins 152 are partially protruded from cavity surface 160 prior to mold tool 142 closure, and are fully extended to the desired position prior to complete closure of mold tool 142. In other embodiments, core pins 152 are partially protruded from cavity surface 160 prior to mold tool 142 closure, and are fully extended to the desired position subsequent to complete closure of mold tool 142. In still further embodiments, core pins 152 are protruded from cavity surface 160 subsequent to complete closure of mold tool 142.
(54) Partial mold tool 142 closure is represented in
(55) Alternatively, the airflow through internal channel 180 of core pin 152 can be continual during engagement of core pin 152 with parison, so as to create a bull-nose formation, similar to that shown in
(56) In some embodiments, complete mold tool closure preceeds airflow through internal channel 180 of core pin 152, with expansion E serving span the gap distance to complete the engagement and bonding between end face 64 of the protrusion and inside surface 66 of first wall 12. In other words, final engagement and bonding between end face 64 of the protrusion and inside surface 66 of first wall 12 may be solely a function of expansion E, without further mechanical manipulation of parison 50.
(57) As will be appreciated, the timing of the passage of air through internal channel 180 of core pin 152 relative to the overall process is not intended to be limited to the examples provided above. For example, in some embodiments, airflow through internal channel 180 of core pin 152 may commence following complete closure of mold tool 142, for example where core pins 152 are extended and engage parison 50 only after mold tool 142 is closed. In still further arrangements, airflow through internal channel 180 may preceed, may be concurrent to or may follow either a parison preblow step and/or a full-pressure blow. For example, where core pins 152 are extended into parison subsequent to closure of mold tool 142, parison 50 may be subject to pressurization, either as a pre-blow or a full pressure blow, so as to ensure a complete seal of circumferential wall 62 to core pin 152 prior to airflow through internal channel 180.
(58) As described in the earlier embodiment of the process, parison 50 is blow molded into the final desired article, and depending on whether or not core pins 152 are maintained within the cavity during blow molding, the various forms detailed in
(59) In some embodiments, delivery of air through internal channels 180 of core pins 152 into protrusion is continued during retraction of core pins 152. The introduction of air into the protrusion during retraction serves to reduce the formation of a vacuum therein, reducing the likelihood of deformation (e.g. dimpling) due to vacuum suck-back, particularly on thin-walled structures.
(60) On completion of the blow molding step, similar to
(61) The delivery of air into the protrusion through core pins 152 has several advantages. As indicated above, air may be introduced when core pins 152 reach a terminal extension point (defining gap distance G), or on a continual basis to form the aforementioned bull-nose formation. Either way, the introduction of air creates an expanded region which cushions the engagement between end surface 64 of the protrusion and inside surface 66 of parison. This cushion effect serves to reduce the likelihood of mechanical compression of the material, reducing unwanted marking or read-through on surfaces generally caused by mechanical contact of molding surfaces during the molding process.
(62) In still further embodiments of the invention, core pins 52 and 152 may be provided with a heating component to deliver heat during the process of forming the protrusion into the parison. For example, as shown in
(63) The location of each structural pillar is noted by a corresponding feature 72 present on the outside surface 74 of second wall 14. Where structural pillar 18 is formed as a partially hollow structural pillar, that is where the core pins are partially left within the protrusion during blow molding, feature 72 is primarily in the form of a hollow bore 70a as seen in
(64) Hollow article 10 is made from a thermoplastic material that has sufficient strength and rigidity to meet the desired performance characteristics. In general, the performance characteristics relate to maximizing the area moment of inertia (MI.sub.a) about the plate neutral axis (NA), to obtain maximum plate stiffness (S). A non-limiting example of suitable materials includes polypropylene, polyethylene, ABS, ABS/PC, polyamide, PLA and PPS. To meet desired strength and rigidity requirements, the thermoplastic may additionally include a range of inorganic filler components, a non-limiting example of which includes glass, mica, calcium carbonate and talc, and/or organic filler components, a non-limited example of which includes jute, husk, and hemp.
(65) The above described structural pillar technology and associated processes may be applied to a range of hollow structures. For example, while exemplified above on a load floor where first and second walls 12, 14 are generally planar and parallel, the technology may be applied to alternate configurations, for example where first and second walls 12, 14 are arranged in a non-parallel configuration. An exemplary non-parallel configuration may include an arrangements where the first and second walls follow a curvature in the hollow article but remain generally parallel throughout. Another exemplary non-parallel configuration may include an arrangement where there is a change in thickness in the article arising from a variation in distance from first wall to second wall.
(66) Presented in
(67) As shown, mold tool 242 comprises two mold halves, namely a first mold half 244 and a second mold half 246. In a closed configuration, first and second mold halves 244, 246 together define a mold cavity 248. Provided in second mold half 246 are a plurality of slidably displaceable core pins for forming the structural pillars. The core pins are coupled to a corresponding yoke plate 254a, 254b based on the desired stroke distance, each yoke plate being capable of lateral displacement through the action of one or more actuators (not shown), permitting the core pins to be protruded and retracted from cavity 248.
(68) In hollow article 10 shown in
(69) Presented in
(70) As shown, mold tool 342 comprises two mold halves, namely a first mold half 344 and a second mold half 346. In a closed configuration, first and second mold halves 344, 346 together define a mold cavity 348. Provided in first mold half 344 is a first plurality of slidably displaceable core pins 352a for engaging the parison on the side corresponding to first wall 12. Provided in second mold half 346 is a second plurality of slidably displaceable core pins 352b for engaging the parison on the side corresponding to second wall 14. The core pins 352a, 352b are coupled to respective yoke plates 354a, 354b, each yoke plate being capable of lateral displacement through the action of one or more actuators (not shown), permitting the core pins to be protruded and retracted from cavity 348. As such, the resulting a hollow article 10 provides a first set of structural pillars 18c that extend from first wall 12 and engage the inside surface of second wall 14, and a second set of structural pillars 18d that extend from second wall 14, and engage the inside surface of first wall 12.
(71) While the above example presents the protrusions from each side as forming an independent structural pillar, in some embodiments the mold tool is configured with aligned opposing core pins such that the protrusions extending from each side are in opposing relationship to form a hollow article 10 having structural pillars 18 as shown in
(72) In the processes described above, additional parison manipulation/forming steps may be incorporated. For example, preseal plates may be incorporated on the mold tool to pinch one or both of the downstream or upstream ends of the parison. On presealing the parison, an optional pre-blow operation may be used to expand the parison prior to mold closure. For certain applications, a pre-stretch of the parison may be necessary, in which case a stretcher plate may be used on the downstream end, the stretcher plate having a plurality of elongated arms that engage and stretch the parison as required. To introduce pressurized air into the parison, blow needles or tubes may be arranged from either the top, bottom or sides of the mold tool.
(73) While the exemplary embodiments presented above show the core pins as having a circular cross-section, it will be appreciated that non-circular cross-sectional profiles may also be used. For example, the core pins may have cross-sectional profiles such as, but not limited to oval, square, cruciform, and any polygonal configuration such as, but not limited to pentagonal, hexagonal and octagonal.
(74) While the structural pillars shown herein have been exemplified as having a substantially constant cross-sectional diameter along the length dimension, in some embodiments, the cross-section of the pillar may vary in diameter or average width. In other words, in some embodiments, the outside surface of the circumferential walls of the structural pillar may not be parallel along the length dimension, such as for example when the structural pillar is presented as having an hour-glass-like shape.
(75) While the solid-core structural pillars shown herein have been exemplified as being substantially solid throughout, in some embodiments the solid-core structural pillars may comprise additional voids wherein no thermoplastic material is present.
(76) While the various processes exemplified above have a covering included in the forming of the hollow structure, it will be appreciated that the covering is optional.
(77) While various embodiments according to the present invention have been described above, it should be understood that they have been presented by way of illustration and example only, and not limitation. It will be apparent to persons skilled in the relevant art that various changes in form and detail can be made therein without departing from the scope of the invention. Thus, the breadth and scope of the present invention should not be limited by any of the above-described exemplary embodiments, but should be defined only in accordance with the appended claims and their equivalents. It will also be understood that each feature of each embodiment discussed herein, and of each reference cited herein, can be used in combination with the features of any other combination. All patents and publications discussed herein are incorporated by reference herein in their entirety.