Airbag covers and the manufacturing methods thereof; airbag devices
11505156 · 2022-11-22
Assignee
Inventors
Cpc classification
B60R21/235
PERFORMING OPERATIONS; TRANSPORTING
B60R21/201
PERFORMING OPERATIONS; TRANSPORTING
B60R21/2176
PERFORMING OPERATIONS; TRANSPORTING
B60R21/213
PERFORMING OPERATIONS; TRANSPORTING
B60R2021/161
PERFORMING OPERATIONS; TRANSPORTING
International classification
B60R21/235
PERFORMING OPERATIONS; TRANSPORTING
B60R21/201
PERFORMING OPERATIONS; TRANSPORTING
Abstract
An airbag cover, a method for manufacturing the same, and an airbag device in which a wound or folded cushion can be stowed in a shape so as to fit in a prescribed location in a vehicle cabin, and which can protect the cushion from an obstacle. An airbag cover that encloses a bag-like cushion that is wound or folded and stowed within a vehicle cabin and expands and deploys using gas supplied from a built-in inflater, wherein the airbag cover includes a first base material made from a plain woven fabric or non-woven fabric made of synthetic fibers, and a second base material integrally bonded to the first base material and having a higher initial tensile resistance value than that of the first base material.
Claims
1. An airbag cover that encloses a bag-shaped cushion that is wound or folded and stowed in a vehicle cabin that expands and deploys using gas supplied from a built-in inflater, comprising a first base material made up of a plain woven fabric or non-woven fabric of synthetic fibers and a second base material that is integrally bonded with the first base material, contains different fibers than the first base material, and has a higher initial tensile resistance value than the first base material, wherein the initial tensile resistance value is the value shown for tensile strength when a cloth with a prescribed shape is pulled under prescribed conditions with a prescribed tensile testing machine and the cloth is elongated by 5%.
2. The airbag cover according to claim 1, wherein the first base material and the second base material are bonded by the fiber polymers of one of the base materials penetrating between fibers of the other base material.
3. The airbag cover according to claim 1, wherein the first base material is formed by interweaving warp and weft yarns of at least nylon or polyester fibers.
4. The airbag cover according to claim 1, wherein the first base material is formed of a non-woven fabric containing at least one of rayon, nylon, polyester, polypropylene, acrylic, vinylon, aramid synthetic fibers, or glass fibers.
5. The airbag cover according to claim 1, wherein the second base material comprises a compressed body formed of a compressed ductile fabric material.
6. The airbag cover according to claim 5, wherein the ductile fabric material is a polymer non-woven fabric material mixed with single fibers or a non-woven fabric material containing a plurality of polymer fibers.
7. The airbag cover according to claim 5, wherein the ductile fabric material is a felt-like material.
8. The airbag cover according claim 5, wherein the ductile fabric material is formed of polyester fibers.
9. The airbag cover according to claim 1, wherein the second base material includes fibers having a melting point that differs by 30° C. or more from the melting point of the fibers included in the first base material.
10. The airbag cover according to claim 1, wherein the airbag cover is provided separately from the airbag module comprising an inflator and a cushion that incorporates the inflater.
11. An airbag device provided with an airbag cover that encloses a bag-shaped cushion that is wound or folded and stowed in a vehicle cabin that expands and deploys using gas supplied from a built-in inflator, comprising a first base material made up of a plain woven fabric or non-woven fabric of synthetic fibers and a second base material that is integrally bonded with the first base material, contains different fibers than the first base material, and has a higher initial tensile resistance value than the first base material, wherein the initial tensile resistance value is the value shown for tensile strength when a cloth with a prescribed shape is pulled under prescribed conditions with a prescribed tensile testing machine and the cloth is elongated by 5%.
12. The airbag device according to claim 11, wherein the airbag device is a side airbag device provided on the side of a vehicle seat and wherein the cushion expands and deploys towards the direction of the occupant in the vehicle seat.
13. The airbag device according to claim 12, wherein the second base material of the airbag cover is provided along the side of the vehicle seat so as to contact the seat frame built into the vehicle seat, and is formed to function as a counterforce surface to receive counterforces from the seat frame during expansion and deployment of the cushion.
14. The airbag device according to claim 11, wherein the airbag device is a curtain airbag device in which the cushion expands and deploys along the side walls of the vehicle body in the vehicle cabin.
15. The airbag device according to claim 14, wherein the second base material of the airbag cover is provided so as to contact the side wall of the vehicle body and is formed to function as a counterforce surface to receive counterforces from the side wall of the vehicle body during expansion and deployment of the cushion.
16. A manufacturing method of an airbag cover that encloses a bag-shaped cushion that is wound or folded and stowed in a vehicle cabin that expands and deploys using gas supplied from a built-in inflator, comprising a first base material made up of a plain woven fabric or non-woven fabric of synthetic fibers and a second base material that contains different fibers than the first base material and has a higher initial tensile resistance value than the first base material, wherein the initial tensile resistance value is the value shown for tensile strength when a cloth with a prescribed shape is pulled under prescribed conditions with a prescribed tensile testing machine and the cloth is elongated by 5%, such that the first base material and the second base material partially overlap and the overlapping portion is integrally bonded by thermal fusing.
17. The manufacturing method of the airbag cover according to claim 16, wherein thermal fusing is performed at a higher temperature than the melting temperature of either the first base material or the second base material.
18. The manufacturing method of the airbag cover according to claim 16, wherein a pressing process is added to the thermal fusing.
19. The manufacturing method of the airbag cover according to claim 16, wherein the second base material includes fibers having a melting point that differs by 30° C. or more from the melting point of the fibers included in the first base material.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
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EMBODIMENT OF THE INVENTION
(11) Preferred embodiments according to the present invention will hereinafter be described in detail with reference to the appended drawings. The dimensions, materials, other specific numerical values, etc. indicated in such embodiments are mere exemplifications for ease of understanding of the invention and do not limit the present invention unless otherwise noted. Note that in the present specification and drawings, elements having substantially identical functions and configurations are labeled with identical symbols in order to omit redundant descriptions along with the illustration of elements not directly related to the present invention.
(12) Note that regarding this embodiment, when a passenger is seated in a seat in a regular posture, the direction the passenger faces is referred to as the front, and the opposite direction is referred to as the rear. Moreover, when the passenger is seated in the seat in a regular posture, the right of the passenger is referred to as the right direction, and the left of the passenger is referred to as the left direction. Furthermore, when the passenger is seated in a regular posture, the direction towards the head of the passenger is referred to as up, and the direction towards the legs of the passenger is referred to as down. In addition, as needed, any diagrams used in descriptions below will indicate the front, rear, left, right, up, and down directions based on the passenger as described above as Fr, Rr, L, R, Up, and Down.
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(14) The side airbag device 100 is provided on the seatback 104 close to the outside of the vehicle, and includes a cushion 108 (see
(15) The cushion 108 is formed into a bag shape using, for example, a cut and sew method. Additionally, the cushion 108 is wound or folded and expands and deploys in an emergency using gas supplied from an inflater 110, which is a gas generator that is built in.
(16) Furthermore, the side airbag device 100 includes an airbag cover 114 that encloses an airbag module 112, which will be described in greater detail below. Note that the airbag module 112 includes the cushion 108 and the inflater 110.
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(18) As illustrated in
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(20) As illustrated in
(21) The airbag cover 114 includes a first base material 128 and a second base material 130 having different initial tensile resistance values (described below), and the first base material 128 and the second base material 130 are integrally bonded via a bonding part 132 formed by thermal fusing.
(22) Here, the initial tensile resistance value is a value expressed by the tensile strength when the pulled fabric is elongated 5% when a prescribed tensile tester is used to pull a fabric having a prescribed shape under prescribed conditions. An example of a method for measuring initial tensile resistance will be described below. A SHIMADZU (tensile testing machine) AUTOGRAPH AG-50kNG was used as a measuring device for tensile strength. A SHIMADZU (Kyowa Load Cell) Type SFL-50KNAG (P/N 340-43122-01) 50KN was used as the load cell. A SHIMADZU (extensometer) SES-1000 was used to measure the tensile length.
(23) The shape of the fabric test piece (sample piece) to be prepared had dimensions of 50 min×300 mm N66 plain woven fabric and PET non-woven fabric were prepared as the base materials. The N66 plain woven fabric was cut into 60 mm×300 mm, and then the warp threads were removed to make the dimensions exactly 50 mm×300 mm. The PET non-woven fabric was cut to 50 mm×300 mm. The N66 plain woven fabric was tested by pulling in the warp direction, and the PET non-woven fabric was tested by pulling in the MD (machine direction). The number of samples was n=5 for each.
(24) The specific test conditions are described below. Under normal temperature (20° C.±15° C.), normal humidity (relative humidity 45-85%) and normal pressure (pressure at which no special pressure reduction or pressurization is performed; normally a pressure equivalent to atmospheric pressure, approximately one atmosphere), the sample piece was first held using an air chuck with an initial chuck distance (initial length) of 100 mm and an initial load of 1.5 N. Next, the gripping part of the extensometer was held and placed near the center of the sample piece so that the distance therebetween was 50 mm. The sample piece was then pulled at a tensile speed of 100 mm/min, and the value of the tensile strength at 5% elongation relative to the initial length was used as the initial tensile resistance value.
(25) The first base material 128 is a base material including a plain woven fabric or a non-woven fabric made of synthetic fibers, and is formed by weaving together warp and weft yarns of nylon fibers or polyester fibers as an example. The first base material 128 can be formed by interweaving such fibers. However, no such limitation is intended, and a non-woven fabric of nylon, polyester, or polypropylene may be used as the first base material 128.
(26) The second base material 130 is a base fabric that includes different fibers than the first base material 128, has a higher initial tensile resistance than the first base material 128, and is formed of a ductile fabric material. The ductile fabric material may be a non-woven fabric including a plurality of polymer fibers, a felt-like material, or may be formed from polyester fibers. By forming the second base material 130 with such ductile fabric material, the initial tensile resistance value can be higher than that of the first base material 128.
(27) Because the first base material 128 and the second base material 130 are capable of maintaining their own shape based on their properties, through enclosing the wound or folded cushion 108, the cushion 108 can be stowed in a shape that fits in a prescribed location in the vehicle cabin, such as the occupant side of the side frame 120.
(28) Since the first base material 128 has a lower initial tensile resistance value than that of the second base material 130, the first base material 128 can easily deform following the shape of the prescribed location in which the cushion 108 is to be stowed. In other words, the first base material 128 is proficient in the function of keeping the cushion 108 in the desired stowed state. Also, providing a slit or the like in the soft first base material 128 enables a way of reliably breaking the cushion 108 without inhibiting expansion and deployment of the cushion 108, and as a result, the expansion behavior of the cushion 108 can be stabilized.
(29) The second base material 130 does not only have a relatively higher initial tensile resistance value than that of the first base material 128 and does not easily deform, but can also maintain a shape. As such, the second base material 130 is provided so as to contact the side frame 120 from the occupant side as illustrated in
(30) In particular, when the second base material 130 is formed of felt material rather than plastic, the felt is softer than plastic, and can be deformed to follow the shape of a prescribed location in which the cushion 108 is to be stowed, and weight reduction can be further achieved.
(31) The material of the bonding part 132 illustrated in
(32) Fibers configuring felt materials are randomly or pseudo-randomly entangled. Moreover, the felt can include two kinds of fibers of different configurations. Moreover, all mono-component composite fibers configuring the felt can be formed of PET homo-polymers, wherein bi-component composite fiber having a core and coating surrounding the cores can be used. The core and the coating of the bi-component composite fiber are configured to have different properties, in particular different melting points, with the coating having a significantly lower melting point than the core (for example, the core has a melting point of about 260° C. and the coating having a melting point of about 110° C. to 150° C.). As an example, the second base material 130 is more preferably a fiber having a melting point with a difference of 30° C. or higher than the melting point of the fibers included in the first base material 128.
(33) The bi-component composite fibers can also be formed entirely of polyester, but the core can be molded from PET homo-polymers and the coating can be formed from copolymers (coPET). When such a PET and coPET are combined, while the melting point of the coating is lower than the melting point of the cores, overall, the fibers can be assuredly formed of PET.
(34) Both cores of the two component conjugate fibers and the single component fibers are formed of PET homopolymers and therefore have the same melting point, with the single component fibers having a melting point higher than the coating of the two component conjugate fibers. The two component conjugate fibers are equally distributed to the overall single component fibers in felt materials. The two component conjugate fibers can account for 30% to 60% of all fibers of felt materials, while all the remaining fibers can be the single component fibers. By including the bi-component composite fibers in the felt material of the second base material 130, heat treatment (thermal processing) of the felt material at a temperature higher than the melting point of the coating enables increasing the initial tensile resistance value of the second base material 130.
(35) As shown in Table 1, the stability of shape during airbag deployment was verified for embodiments 1 and 2, and the comparative example, in which several types of first base materials and second base materials were combined.
(36) TABLE-US-00001 TABLE 1 First base Second base material/initial material/initial First base Second base tensile resistance tensile resistance material material value [N] value [N] Results Embodiment N66 Plain PET + Co-PET 125 425 ∘ 1 woven non-woven base fabric (thermal material processing) Embodiment PET Non- PET + Co-PET 143 425 ∘ 2 woven non-woven fabric fabric (thermal processing) Comparative PET Non- PET + Co-PET 143 50 x Example woven Non-woven fabric fabric
(37) In embodiment 1, a N66 plain woven fabric was prepared as a first base material, and a PET+Co-PET non-woven fabric that was subjected to thermal processing was prepared as a second base material, and these were combined. Here, the N66 plain woven fabric is a fabric obtained by weaving nylon 66 fibers. In addition, the PET+Co-PET non-woven fabric is a fabric formed by using normal PET in the core portion of the fibers and using a Co-PET (Copolymer-PET: modified PET copolymer) in the coating (sheath) portion by chemical bonds, thermal bonds, needle punches, spun laces, stitch-bonds, or the like. Furthermore, thermal processing of the second base material is a process of heating and pressurizing at 150° C. to 200° C. for 20 seconds to 3 minutes to compress and harden the non-woven fabric to obtain a compressed body.
(38) In embodiment 1, the initial tensile resistance value of the first base material was “125”, the initial tensile resistance value of the second base material was “425”, an initial tensile resistance value higher than that of the first base material. As a result, in embodiment 1, the stability of the shape when the airbag was deployed was “0”, or in other words, good shape retention of the airbag module during installation, and the deployment behavior during deployment was stable and favorable.
(39) In embodiment 1, a PET non-woven fabric was prepared as a first base material, and a PET+Co-PET non-woven fabric that was subjected to thermal processing was prepared as a second base material, and these were combined. Here, the PET non-woven fabric is made of polyester (polyethylene terephthalate) fibers as a non-woven fabric using the spunbond method.
(40) In embodiment 2, the initial tensile resistance value of the first base material was “143”, the initial tensile resistance value of the second base material was “425”, an initial tensile resistance value higher than that of the first base material. As a result, in embodiment 2, the stability of the shape when the airbag was deployed was “0”, or in other words, good shape retention of the airbag module during installation, and the deployment behavior during deployment was stable and favorable.
(41) In the comparative example, a PET non-woven fabric was prepared as the first base material, and a PET+Co-PET non-woven fabric was prepared as the second base material, and these were combined. Here, no thermal processing is applied to the second base material in the comparative example.
(42) In the comparative example, the initial tensile resistance value of the first base material was “143”, the initial tensile resistance value of the second base material that was not subjected to thermal processing was “50”, which is an initial tensile resistance value lower than that of the first base material. As a result, in the comparative example, the stability of the shape when the airbag was deployed was “X”, or in other words, poor shape retention of the airbag module during installation, and the deployment behavior during deployment was not stable.
(43) Next, a method of molding the bonding part 132 and the compression body (second base material) 130 will be described with reference to
(44) First, as illustrated in
(45) When felt material is heated and compressed, the fibers are compressed into each other and the felt material becomes thinner (0.55 mm for example), deforming plastically into a compressed body. More specifically, when heated at temperatures higher than the melting point of the coating of the two component conjugate fibers, the coating is dissolved. Therefore, the coating is fused together at all positions in which fibers of the joining material are distributed. Here, because the joining material is heated at a temperature lower than the melting point of the cores of the bi-component composite fibers along with the overall structure of the single component fibers, the cores and the single component fibers are still in solid phase, and not fused together, with only the materials of the coating fused together.
(46) When heat and pressure are applied by the pressing devices 136, 138 and a prescribed heating time (for example 20 seconds or 100 seconds) elapses, as illustrated in
(47) Here, in the example of
(48) In the present invention, if there are locations that should not be bonded, for example, or when the airbag cover 114 is fused while enclosing the cushion 108, those areas not to be fused may be silicon-coated or covered with a silicon-coated fabric.
(49) The thermal fusing results in
(50) In addition, the results show that when a silicon coating is not applied to the adhesive surface of the first base material 128 (No. 1, 2, 5, and 6), the adhesive strength, or in other words the force required for separation, becomes stronger the higher the heating temperature and the longer the heating time. However, looking at the results from No. 5 and No. 6, an assumption can be made that the adhesive strength is saturated to some extent, as the adhesive strength does not become much stronger with longer heating times.
(51) Note that by adjusting the adhesive strength of the first base material 128 and the second base material 130, bonding parts with weak adhesive strength may be intentionally provided. In this manner, during the expansion and deployment of the cushion 108, the airbag cover 114 can reliably cleave through starting at the junction with weak adhesive force, and thus the deployment behavior can be stabilized without inhibiting the expansion and deployment of the cushion 108.
(52) By forming the bonding part 132 based on the results of such pressurized thermal fusing, an airbag cover 114 (see
(53) A procedure for wrapping the airbag cover 114 around the airbag module 112 to enclose the airbag cover will be described below with reference to
(54) With the airbag module 112 illustrated in
(55) The airbag cover 114 is configured by a first base material 128 and a second base material 130 that is a compressed body. A plurality of slits (or slots) 147 are formed in the first base material 128 starting at the bonding part 132 of the first base material 128 and the second base material 130. Bridge parts 139 are formed over the slits 147. A portion of the slits 147 and the bridge parts 139 are formed in the region of the second base material 130 as a compressed body. Additionally, the remaining portions of the slits 147 and the bridge parts 139 are formed in the region of only the first base material 128.
(56) In addition, the cushion 108 is wound or folded. As illustrated in
(57) First, as illustrated in
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(59) Furthermore, from this state, as illustrated by arrows H, I of
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(61) By providing the airbag cover 114 separately from the airbag module 112, the airbag cover 114 can be manufactured and then wound around to enclose the airbag module 112. Thus, the airbag cover 114 can be made in a separate location from the airbag module 112.
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(63) More specifically, regarding the side airbag device 100A, the airbag module 112 wrapped up in the airbag cover 114 is disposed on the side frame 120 via the inflater 110, and is stowed on a side opposite to the occupant side of the side frame 120.
(64) The second base material 130, which has a relatively high initial tensile resistance value and is resistant to deformation, is provided so as to contact the side frame 120 from the side opposite the occupant side; the cushion 108 is formed so as to function as a counterforce surface that receives the counterforce from the side frame 120 during expansion and deployment of the cushion 108 and is disposed on the side of the cushion 108 in a stowed state closer to an obstacle such as the edge 134 of the side frame 120. As a result, the second base material 130 can maintain a shape such that the cushion 108 avoids obstructions, and also protects the cushion 108 from obstructions even when the cushion 108 is stowed, as well as when the cushion 108 is expanded and deployed, preventing failures such as bursts and the like.
(65) The side airbag devices 100, 100A configured in this manner easily break the slits 147 (
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(67) Regarding an airbag cover 114B illustrated in
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(69) The curtain airbag device 100B restrains the occupant by expanding and deploying a cushion 158 based on pressure of the gas supplied from an inflater 156 during an emergency, such as a side collision. As illustrated in
(70) The vehicle further includes a roof side rail 170 and a cover 172 that covers the roof side rail 170 on the side of the vehicle interior. Note that in the diagrams, the cover 172 is illustrated by a two-dot dashed line. The roof side rail 170 is positioned on the upper side of the interior of the vehicle and forms the vehicle body side wall.
(71) The cushion 158 is wound or folded over the entire vehicle front-rear direction and is stowed between the roof side rail 170 and the cover 172 in the J-J cross-section illustrated in
(72) Regarding the curtain airbag device 100B, as illustrated in
(73) Therefore, according to the curtain airbag device 100B, by disposing the second base material 130, which has a relatively high initial tensile resistance value and is resistant to deformation, on the side of the cushion 158 in a stowed state close to the obstacle (here, the roof side rail 170), the cushion 158 is protected from the obstruction and prevents defects such as bursts and the like. Furthermore, because the first base material 128 has a lower initial tensile resistance value than that of the second base material 130, the cushion 158 can be easily deformed following the shape of the prescribed location in which the cushion 158 is to be stowed, and the cushion 158 can be stowed in a shape that fits in the prescribed location.
(74) Thus, the airbag cover 114 can be applied to any of the side airbag devices 100, 100A and the curtain airbag device 100B, and furthermore, the wound or folded cushions 108, 158 can be stowed in a location fit in a prescribed location in the vehicle cabin while protecting the cushions 108, 158 from obstructions.
(75) Preferred embodiments of the present invention were described with reference to the appended drawings, however, it goes without saying that the present invention is not limited to such examples. It is clear that a person of ordinary skill in the art could conceive of various modifications or revisions within the scope set forth by the claims, and it would be understood that these modifications or revisions would belong to the technical scope of the present invention.
(76) Moreover, although the embodiment above describes an example in which a side airbag device or curtain airbag device equipped with an airbag cover according to the present invention is applied to an automobile, the airbag cover can also be applied to aircraft, ships, or the like in addition to automobiles, while obtaining the same effects.
INDUSTRIAL APPLICABILITY
(77) The present invention can be used in an airbag cover that encloses a cushion that is stowed in a vehicle cabin and expands and deploys for the purpose of protecting an occupant in an emergency, a method for manufacturing the same, and can be used for an airbag device provided with an airbag cover.
EXPLANATION OF CODES
(78) 100, 100A: side airbag device; 100B: curtain airbag device; 102: vehicle seat; 104: seatback; 106: side door; 108, 158: cushion; 110, 156: inflater; 112: airbag module; 114, 114A, 114B: airbag cover; 116: seat back frame; 118: upper frame; 120: side frame; 122: seat cushion; 124: seat frame; 126, 142: stud bolts; 128, 128A, 128B: first base material; 130: second base material; 132, 132A, 132B: bonding part; 134: side frame edge; 136, 138: pressing devices, 139, 139A: first base material bridge part, 140A: first base material warp, 140b: first base material weft; 144, 146: cushion insertion hole; 147, 147A: first base material slit (slot); 148, 150: first base material insertion hole; 152, 154: second base material insertion hole; 160, 162: side window; 164: front pillar; 166: center pillar; 168: rear pillar; 170: roof side rail; 172: cover; 174: tab