[0001] The present invention relates generally to panels. More particularly, the present
invention relates to a fabric panel for use in items such as chairs, furniture, and
luggage.
[0002] Chairs, furniture and other articles typically include rigid panels which may serve
various purposes. For example, many chairs are constructed of seat and backrest panels
which are formed or molded substrates onto which a padded composite structure is attached.
The chair panels are designed to support the weight of an occupant of the chair with
the foam padding being used to provide comfort to the occupant. However, such panels
are often bulky and can significantly increase the chair's overall weight while decreasing
the chair's stacking/storage density. Solid surface chair panels also provide very
little breathability, which contributes negatively to the comfort of the occupant.
[0003] Furniture such as dressers and so-called "entertainment centres" are usually constructed
of wood panels having a laminated and/or varnished exterior finish. These wood panels
add tremendous weight to the furniture. Additionally, wood finishes are notoriously
susceptible to damage. Most wood furniture panels are not designed to be easily removed
and replaced with a new and undamaged panel, so the furniture's wood finish must be
maintained in order to keep an aesthetically pleasing appearance.
[0004] One approach to resolving the disadvantages of prior art chair panels has been to
provide a single-layer elastic membrane that is pre-stretched and mounted to a molded
frame. However, the manufacture of such a chair is tremendously complicated and requires
a very large molding machine. Also, the structural support and user comfort exhibited
by the pre-stretched membranes has been found lacking.
[0005] What is needed, therefore, is a panel that overcomes problems and disadvantages associated
with prior art panels.
[0006] The present invention provides in a first aspect a panel comprising:
an envelope of resilient material, said envelope having an opening with a fastener
for closing the envelope; and
an envelope support frame being substantially rigid and formed in a closed loop, said
envelope support frame being positioned inside said envelope and tensioning the resilient
material of the envelope in one or more tension zones;
wherein said fastener is closed to envelop the envelope support frame with the
resilient material.
[0007] The present invention eliminates the difficulties and disadvantages of the prior
art by providing a panel which having an envelope fabricated from a resilient material.
The envelope includes an opening with a fastener for closing the envelope. A substantially
rigid envelope support frame formed in a closed loop is positioned inside the envelope
and tensions the resilient material of the envelope in one or more tension zones.
The fastener is closed to envelop the envelope support frame with the resilient material.
[0008] The panel may be configured to include a plurality of tension zones where each tension
zone represents a tension on the resilient material that is different than the tension
represented by each immediately adjacent tension zone. Tensions applied in the tension
zones may all be in a common direction. Use of multiple tension zones in this manner
is particularly suitable for panels that carry significant loads, such as the seat
panel of a chair or stool.
[0009] The present invention provides in a second aspect a multilayer support panel comprising:
an envelope of resilient material, said envelope including:
a first layer of the resilient material in opposed relation to a second layer of resilient
material; and
an opening with a fastener for closing the envelope; and
an envelope support frame being substantially rigid and formed in a closed loop, said
envelope support frame being positioned inside said envelope and tensioning each layer
of the resilient material of the envelope in one or more tension zones;
wherein said fastener is closed to envelop the envelope support frame with the
resilient material, said second layer of resilient material providing overload support
when loading on the first layer of resilient material causes said first layer of resilient
material to contact the second layer of resilient material.
[0010] In the second aspect of the invention, the envelope includes a first layer of resilient
material in opposed relation to a second layer of resilient material. The second layer
of resilient material functions to provide overload support when loading on the first
layer is sufficient to bring it into contact with the second layer.
[0011] The present invention provides in a third aspect a support panel comprising:
an envelope of resilient material, said envelope having an opening with a fastener
for closing the envelope; and
an envelope support frame being substantially rigid and formed in a closed loop, said
envelope support frame being positioned inside said envelope and tensioning the resilient
material of the envelope in a plurality of substantially parallel tension zones where
each tension zone represents a tension on the resilient material that is different
than the tension represented by a different tension zone;
wherein said fastener is closed to envelop the envelope support frame with the
resilient material.
[0012] The present invention provides in a fourth aspect an apparatus for receiving an occupant
in a seated position, said apparatus comprising:
a seat frame; and
at least one panel attached to said seat frame for supporting an occupant of the apparatus,
said at least one panel including:
an envelope of resilient material, said envelope having an opening with a fastener
for closing the envelope; and
an envelope sub-frame being substantially rigid and formed in a closed loop, said
envelope sub-frame being positioned inside said envelope and tensioning the resilient
material of the envelope in one or more tension zones;
wherein said fastener is closed to envelop the envelope support frame with the
resilient material.
[0013] When the panel is to employed in a chair or other apparatus for receiving an occupant
in a seated position, the panel is preferably attached to the chair. This may be accomplished
by attaching a seat plate to the chair frame, attaching an envelope support frame
plate to the envelope support frame, and attaching the support frame plate to the
seat plate with a fastener such as a threaded bolt.
[0014] Preferred embodiments of the invention will now be described in further detail. Other
features, aspects, and advantages of the present invention will become better understood
with regard to the following detailed description, appended claims, and accompanying
drawings (which are not to scale) where:
FIG. 1 is a perspective view of a chair having panels according to the present invention;
FIG. 2 is a perspective view of the chair of FIG. 1 illustrating various stretch zones
in the chair panels;
FIG. 3 is plan view of a fabric envelope according to the present invention;
FIG. 4 is plan view of a panel sub-frame according to the present invention;
FIG. 5 is a side view of the panel sub-frame of FIG. 4;
FIG. 6 is a plan view of the panel sub-frame of FIG. 4 illustrating deformation of
the panel sub-frame prior to insertion into the fabric envelop of FIG. 3 during fabrication;
FIG. 7 is a plan view of the panel sub-frame of FIG. 4 illustrating an alternate deformation
of the panel sub-frame prior to insertion into the fabric envelope of FIG. 3 during
fabrication;
FIG. 8 is an end view of a fabric panel according to the invention; and
FIG. 9 is a cross-section view of the chair of FIG. 1 taken along section line 9-9.
[0015] Preferred embodiments of the present invention will now be described with reference
to the accompanying drawings, wherein like reference characters designate like or
similar parts throughout. The terminology used herein is intended to be interpreted
in its broadest reasonable manner, even though it is being utilized in conjunction
with a detailed description of certain specific preferred embodiments of the present
invention. This is further emphasized below with respect to some particular terms
used herein. Any terminology intended to be interpreted by the reader in any restricted
manner will be overtly and specifically defined as such in this specification.
[0016] FIG. 1 illustrates a chair 10 incorporating a seat panel 12 and a back rest panel
14 attached to a chair frame 16. The chair frame 16 is fabricated from tubular or
rod steel with welds at points 18. The seat panel 12 and back rest panel 14 are fabricated
from an envelope of resilient material that is stretchable with an internal sub-frame
tensioning the material of the envelope in one or more tension zones of the panel,
as more fully described below.
[0017] It will be understood that the particular chair style illustrated in FIG. 1 is not
limiting and that a panel 12, 14 according to the invention may be employed in a variety
of devices whose function is to receive an occupant in a seated position. For example,
a panel 12, 14 according to the invention may employed as the seating surface of a
stool. Additionally, a panel according to the invention is not limited to use in seating
devices, but rather, may be employed in various items of furniture, such as dressers
and entertainment centers, that require panels as well as numerous other items including
luggage and area dividers/partitions.
[0018] FIG. 2 illustrates various contiguous tension zones 20-34 representing different
loadings or tensions on the resilient material of the panels 12, 14 when an occupant
sits in the chair 10. In general, maximum loading is normally experienced in zone
22, which includes the crown 36 of the seat panel 12, and also in zone 26 which includes
that portion of the seat panel 12 that supports the occupant's ischial tuberosities.
A medium amount of loading is normally experienced in zone 24 where the back of the
occupant's thighs are normally supported. Minimal to no loading of the seat panel
12 by the occupant is typically experienced in zones 20 and 28.
[0019] With regard to the back rest panel 14, maximum loading by the occupant is normally
experienced in zone 32 where the occupant's lumbar region is supported. Minimal to
no loading is typically experienced at zones 30 and 34 of the back rest panel 14.
[0020] A preferred embodiment of an envelope 40 used for fabrication of a seat panel 12
is shown in FIG. 3. Although not required in the practice of the invention, the envelope
40 is preferably configured to account for the differential loading by an occupant
in zones 20-34 of FIG. 2. This can be accomplished by fabricating the envelope 40
from a resilient material that is stretchable. While many such materials are readily
available, a particularly suitable material in this regard is available from the Milliken
Company under the trade name C-Flex™, which is fabricated from monofiliment fibres
having a 672 durometer D-scale value. The C-Flex material has a tensile strength in
the warp direction of 1,075,630 kN/m
2 (156,000 psi) and a tensile strength in the filling direction of 1,337,630 kN/m
2 (194,000 psi). The C-Flex material has the added benefit of high breathability, which
significantly enhances occupant comfort.
[0021] The envelope 40 is shown in FIG. 3 in its relaxed state and includes an opening generally
shown at 42 with a fastener 44, for closing the envelope 40. Fastener 44 can be a
hook and loop, sliding track, adhesive, or any other fastener suitable for closing
an envelope made from a resilient material. The envelope 40 has a width W at the opening
42 that tapers or narrows towards the distal end 46 along at least a portion of the
length L of the envelope 40. The fastener 44, being essentially non-stretchable, is
made to approximate the width W of an envelope support frame, or sub-frame 50 (FIGS.
4 and 5) that is positioned within the envelope 40. The relatively narrow body of
the envelope 40 results in tension being placed on the envelope's resilient material
when the sub-frame 50 is contained within the envelope 40.
[0022] Tension placed on the envelope material when the sub-frame is positioned within the
envelope 40 may be essentially constant across the length L of the envelope 40. However,
in a preferred embodiment as shown in FIG. 3, the envelope 40 is configured so that
the level of tension placed on the envelope material with the sub-frame 50 in place
varies along the length L of the envelope 40 with each of the different tensions being
applied in a common direction. This can be accomplished by varying the width of the
relaxed envelope material so that the material is stretched to a greater extent in
those portions of the envelope 40 where the width is narrower. For example, the width
of the relaxed envelope material in high loading zones 22 and 26 is less than the
width in loading zones 20, 24 and 28 where loading is normally less. Also, it is preferable
that fabric lines and art work that may be present on the envelope material be deformed
commensurate with the contour of the relaxed envelope so that when the sub-frame 50
is positioned within the envelope 40, there is no deformation of the fabric lines
or art work in the finished panel 12.
[0023] With further reference to FIGS. 4 and 5, the envelope of sub-frame 50 is preferably
fabricated as a substantially rigid closed loop. The shape and contour of the sub-frame
50 will depend on the particular application. For example, the sub-frame 50 of FIGS.
4 and 5 is for use in the seat panel 12 shown in FIGS. 1 and 2, so this particular
sub-frame 50 is curved downward toward the front edge 52 of the seat panel 12 so that
a crown 36 is formed. The sub-frame 50 may be fabricated from a substantially rigid
material such as steel or titanium.
[0024] Various methods may be employed to position the sub-frame 50 within the envelope
40. One such method can be described with reference to FIG. 6. By applying force to
opposed sides 54, 56 of the sub-frame 50 in the general direction and position indicated
by arrows 58, 60, the width of the sub-frame 50 can be reduced by an amount X so that
the width of the sub-frame 50 under deformation becomes W - X. The deformed sub-frame
50 is then positioned in the envelope 40, the sub-frame 50 is released so that the
envelope periphery urges against the sub-frame 50, and the fastener 44 (if using a
sliding track fastener) is closed with slider 62 (FIG. 3) to envelop the sub-frame
50 within the envelope 40. The ends 64, 66 of the sliding track fastener 44 are then
removed and sealed to inhibit inadvertent opening of the fastener 44. An end view
of an assembly panel 12 employing a sliding track fastener 44 is shown in FIG. 8.
If desired, a cover may be positioned over the closed fastener 44 for aesthetics.
Suitable methods for sealing the fastener ends 64, 66 include application of heat
to fuse the fastener ends 64, 66 closed, application of an adhesive to adhesively
close the fastener ends 64, 66, and use of a staple or any other suitable means for
closing the fastener ends 64, 66. If desired, the sliding track fastener 44 may be
fabricated from polyester or some other material that can be fused by application
of heat along the entire length of the fastener 44 to further inhibit the ability
of the fastener 44 to inadvertently open.
[0025] Another method for positioning the sub-frame 50 within the envelope 40 can be described
with reference to FIG. 7. By applying force to opposed sides 54, 56 of the sub-frame
50 in the general direction and position indicated by arrows 70, 72, the width of
the sub-frame 50 can be reduced by an amount Y so that the width of the sub-frame
50 becomes W - Y. The deformed sub-frame 50 is then slipped in the envelope 40, the
sub-frame 50 is released so that the envelope periphery urges against the sub-frame
50, and the fastener 44 is closed to envelop the sub-frame within the envelope 40.
If using a sliding track fastener 44, the ends 64, 66 of the fastener 44 are then
removed and sealed in accordance with the immediately preceding description.
[0026] In yet a further method for positioning the sub-frame 50 within the envelope 40,
the envelope 40 is stretched to allow insertion of the sub-frame 50. The deformed
envelope 40 is then released so that the periphery of the envelope urges against the
sub-frame 50, and the fastener is closed to envelop the sub-frame within the envelope
40. If using a sliding track fastener 44, the ends 64, 66 of the fastener 44 are then
removed and sealed in accordance with the above description.
[0027] Use of the particular envelope 40 shown in FIG. 3 results in an assembled panel 12
having a plurality of substantially parallel and contiguous tension zones 20-28 where
each tension zone represents a tension on the resilient material of the envelope 40
that is different than the tension represented by each immediately adjacent tension
zone. In a preferred embodiment of a seat panel 12 for use in a chair 10 of the type
shown in FIGS. 1 and 2, tension zone 20 of the assembled panel 12 will have a tension
of about 10 pounds per inch (1751.27 N/m) or less, tension zone 22 will have a tension
of about 65 pounds (11383.26 N/m) per inch, tension zone 24 will have a tension within
the range of about 30-35 pounds per inch (5253.81 - 6129.45 N/m) or less, tension
zone 26 will have a tension of about 65 pounds per inch (11,383.26 N/m), and tension
zone 28 will have a tension of about 10 pounds per inch (1751.27 N/m) or less, with
each of these tensions being applied in a common direction (i.e., for the envelope
40 of FIG. 3, in a direction substantially parallel with end 46). The use of multiple
tension zones 20-28 in the panel 12 eliminates the need for additional support structure
beneath or behind the high tension areas with little or no detrimental effect to the
occupant's comfort.
[0028] Referring again to FIG. 8, the assembled panel 12 includes a top layer 100 of resilient
material in opposed relation to a bottom layer 102 of resilient material with the
bottom layer 102 providing overload support in the event the top layer 100 receives
sufficient loading to bring it into contact with the bottom layer 102. In this regard,
the two layers 100, 102 complement one another and provide a significant level of
redundancy and integrity to the panel 12.
[0029] The assembled panel 12 may be attached to the chair frame 16 in a number of ways.
FIG. 9 illustrates how the panel 12 can be attached to the chair frame 16 in accordance
with a preferred embodiment. The attachment assembly employs two plates - a chair
plate 104 attached to the chair frame 16 by, for example, a weld 106 and a seat plate
108 attached to the sub-frame 50 by a weld 110. The two plates 104, 108 are attached
so as to be in alignment with one another when the panel 12 is properly positioned
with respect to the chair frame 16. In proper alignment, the two plates 104, 108 are
then attached to each other with use of a fastener, such as a threaded bolt 112, weld,
adhesive, or other suitable fastener. In a preferred embodiment, a total of four such
plate assemblies are used to secure the panel 12 to the chair frame 16.
[0030] The foregoing description details certain preferred embodiments of the present invention
and describes the best mode contemplated. It will be appreciated, however, that no
matter how detailed the foregoing description appears, the invention can be practiced
in many ways without departing from the spirit of the invention. Therefore, the above
mentioned description is to be considered exemplary, rather than limiting, and the
true scope of the invention is that defined in the following claims and any equivalents
thereof.
1. A panel (12; 14) comprising:
an envelope (40) of resilient material, said envelope having an opening (42) with
a fastener (44) for closing the envelope (40); and
an envelope support frame (50) being substantially rigid and formed in a closed loop,
said envelope support frame(50) being positioned inside said envelope (40) and tensioning
the resilient material of the envelope (40) in one or more tension zones (20, 22,
24, 26, 28;30, 32, 34);
wherein said fastener (44) is closed to envelop the envelope support frame (50)with
the resilient material.
2. The panel of claim 1 wherein said one or more tension zones (20, 22, 24, 26; 30, 32
34) includes a plurality of contiguous tension zones (20, 22, 24, 26; 30, 32, 34)
where each tension zone (20, 22, 24, 26; 30, 32, 34) represents a tension on the resilient
material that is different than the tension represented by each immediately adjacent
tension zone (20, 22, 24, 26; 30, 32, 34).
3. The panel of claim 2 wherein tension represented by each of the tension zones (20,
22, 24, 26; 30, 32, 34) is applied to the resilient material in a common direction.
4. The panel of claim 2 or claim 3 wherein the tension in a first tension zone (22, 26)
is about 65 pounds per inch (11,383.26 N/m) and the tension in a second tension zone
(20, 28) is about 10 pounds per inch (1751.27 N/m) or less.
5. The panel of claim 2 or claim 3 wherein the tension in a first tension zone (22, 26)
is about 65 pounds per inch (11,383.26 N/m) and the tension in a second tension zone
(24) is about 35 pounds per inch (6129.45 N/m) or less.
6. The panel of any one of claims 2 to 5 wherein the width (W) of each tension zone (20,
22, 24, 26; 30, 32, 34) when the envelope (40) is in its relaxed state is different
than the width (W) of each immediately adjacent tension zone (20, 22, 24, 26; 30,
32, 34).
7. The panel of any one of claims 1 to 6, further comprising a chair frame (16) attached
to said envelope support frame (50).
8. A multilayer support panel (12) comprising:
an envelope (40) of resilient material, said envelope including:
a first layer (100) of the resilient material in opposed relation to a second layer
(102) of resilient material; and
an opening (42) with a fastener (44) for closing the envelope (40); and
an envelope support frame (50) being substantially rigid and formed in a closed loop,
said envelope support frame (50) being positioned inside said envelope (40) and tensioning
each layer (100,102) of the resilient material of the envelope (40) in one or more
tension zones (20, 22, 24, 26);
wherein said fastener (44) is closed to envelop the envelope support frame (50)
with the resilient material, said second layer (102) of resilient material providing
overload support when loading on the first layer of resilient material causes said
first layer (100) of resilient material to contact the second layer (102) of resilient
material.
9. The panel of claim 8 wherein said one or more tension zones (20,22, 24,26) includes
a plurality of contiguous tension zones (20, 22, 24, 26) where each tension zone (20,
22, 24, 26) represents a tension on the resilient material that is different than
the tension represented by each immediately adjacent tension zone (20, 22, 24, 26).
10. The panel of claim 9 wherein tension represented by each of the tension zones (20,
22, 24, 26) is applied to the resilient material in a common direction.
11. The panel of claim 9 or claim 10 wherein the tension in a first tension zone (22,
26) is about 65 pounds per inch (11,383.26 N/m) and the tension in a second tension
zone (24) is about 10 pounds per inch (1,751.27 N/m) or less.
12. The panel of claim 9 or claim 10 wherein the tension in a first tension zone is about
65 pounds per inch (11,383.26 N/m) and the tension in a second tension zone is about
35 pounds per inch (6129.45 N/m)or less.
13. The panel of any one of claims 9 to 12 wherein the width (W) of each tension zone
(20, 22, 24, 26) when the envelope (40) is in its relaxed state is different than
the width (W) of each immediately adjacent tension zone (20, 22, 24, 26).
14. The panel of any one of claims 8 to 13, further comprising a chair frame (16) attached
to said envelope support frame (50).
15. A support panel (12, 14) comprising:
an envelope (40) of resilient material, said envelope (40) having an opening (42)
with a fastener (44) for closing the envelope (40); and
an envelope support frame (50) being substantially rigid and formed in a closed loop,
said envelope support frame (50) being positioned inside said envelope (40) and tensioning
the resilient material of the envelope (40) in a plurality of substantially parallel
tension zones (20, 22, 24, 26, 28; 30, 32,34) where each tension zone (20, 22, 24,
26, 28; 30, 32,34) represents a tension on the resilient material that is different
than the tension represented by a different tension zone (20, 22, 24, 26, 28; 30,
32,34);
wherein said fastener (44) is closed to envelop the envelope support frame (50)
with the resilient material.
16. The panel of claim 15 wherein the tension in a first tension zone (20, 22, 24, 26,
28; 30, 32,34) is about 65 pounds per inch (11,383.26 N/m) and the tension in a second
tension zone (20, 22, 24, 26, 28; 30, 32,34) is about 10 pounds per inch (1751.27
N/m) or less.
17. The panel of claim 15 wherein the tension in a first tension zone (20, 22, 24, 26,
28; 30, 32,34) is about 65 pounds per inch (11,383.26 N/m) and the tension in a second
tension zone (20, 22, 24, 26, 28; 30, 32,34) is about 35 pounds per inch (6129.45
N/m) or less.
18. The panel of any one of claims 15 to 17 wherein the width (W) of each tension zone
(20, 22, 24, 26, 28; 30, 32,34) when the envelope (40) is in its relaxed state is
different than the width (W) of each immediately adjacent tension zone (20, 22, 24,
26, 28; 30,32,34).
19. An apparatus for receiving an occupant in a seated position, said apparatus comprising:
a seat frame (16); and
at least one panel (12) attached to said seat frame for supporting an occupant of
the apparatus, said at least one panel (12) including:
an envelope (40) of resilient material, said envelope (40) having an opening (42)
with a fastener (44) for closing the envelope (40); and
an envelope sub-frame (50) being substantially rigid and formed in a closed loop,
said envelope sub-frame (50) being positioned inside said envelope (40) and tensioning
the resilient material of the envelope (40) in one or more tension zones (20, 22,
24, 26, 28);
wherein said fastener (44) is closed to envelop the envelope sub-frame (50) with
the resilient material.
20. The apparatus of claim 19, further comprising:
a seat plate (104 attached to the seat frame (16);
a sub-frame plate (108)attached to the envelope sub-frame (50); and
a fastener (112) for attaching the sub-frame plate (108) to the seat plate (104).
21. The panel of claim 19 or claim 20 wherein said one or more tension zones (20, 22,
24, 26, 28) includes a plurality of contiguous tension zones (20, 22, 24, 26, 28)
where each tension zone (20, 22, 24, 26, 28)represents a tension on the resilient
material that is different than the tension represented by each immediately adjacent
tension zone (20, 22, 24, 26, 28).
22. The panel of claim 21 wherein tension represented by each of the tension zones (20,
22, 24, 26, 28) is applied to the resilient material in a common direction.
23. The panel of claim 21 or claim 22 wherein the tension in a first tension zone is about
65 pounds per inch (11,383.26 N/m) and the tension in a second tension zone is about
10 pounds per inch (1,751.27 N/m) or less.
24. The panel of claim 21 or claim 22 wherein the tension in a first tension zone is about
65 pounds per inch (11,383.26 N/m) and the tension in a second tension zone is about
35 pounds per inch (6129.45 N/m) or less.
25. The panel of any one of claims 21 to 24 wherein the width (W) of each tension zone
(20, 22, 24, 26) when the envelope (40) is in its relaxed state is different than
the width (W) of each immediately adjacent tension zone (20, 22, 24, 26).