TWI806316B - 塗佈織物、用於製備其的方法以及包括其之氣囊 - Google Patents

塗佈織物、用於製備其的方法以及包括其之氣囊 Download PDF

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TWI806316B
TWI806316B TW110149009A TW110149009A TWI806316B TW I806316 B TWI806316 B TW I806316B TW 110149009 A TW110149009 A TW 110149009A TW 110149009 A TW110149009 A TW 110149009A TW I806316 B TWI806316 B TW I806316B
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TW202233923A (zh
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金孝殷
鄭一
金起定
許眞旭
朴志熏
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南韓商可隆工業股份有限公司
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Abstract

本申請案是有關於一種塗佈織物、用於製備其的方法以 及一種包括所述塗佈織物的氣囊。

Description

塗佈織物、用於製備其的方法以及包括其之氣 囊 [相關申請案的交叉參考]
本申請案主張在韓國智慧財產局中於2020年12月29日提出申請的韓國專利申請案第10-2020-0186479號及於2021年12月22日提出申請的韓國專利申請案第10-2021-0185280號的權益，所述韓國專利申請案的揭露內容全文併入本案供參考。
本申請案是有關於一種塗佈織物以及一種包括所述塗佈織物的氣囊。
氣囊是一種用於藉由在利用感測器偵測到碰撞衝擊之後使火藥爆炸且當由於碰撞或類似因素導致的外力施加至車輛時使供應至氣囊緩衝墊(airbag cushion)內部的氣體膨脹來保護車輛使用者的裝置。由於緩衝墊膨脹過程中所涉及的充氣機周圍產生高溫及高壓氣體，因此氣囊織物受損，此會導致緩衝墊的耐壓效能(pressure resistance performance)下降。
為防止此種現象，傳統上考慮使用高密度織造織物 (high-density woven fabric)或者增加塗佈重量(coating weight)，但此與氣囊緩衝墊變得更小且更輕的趨勢不匹配，且具有使可儲存性(storability)(可折疊性(foldability))劣化的問題。
本申請案的一個目的是提供一種能夠解決由傳統技術導致的上述問題的塗佈織物。
本申請案的另一目的是提供一種具有極佳可折疊性的塗佈織物。
本申請案的另一目的是提供一種即使在低重量及/或低密度下亦具有極佳耐熱性及耐久性的塗佈織物。
本申請案的又一目的是提供一種包括所述塗佈織物的氣囊。
本申請案的以上及其他目的可藉由下述本申請案來完全達成。
在一個實施例中，本揭露是有關於一種塗佈織物。具體而言，所述塗佈織物包括纖維基板(A)以及形成於所述纖維基板上的塗層(B)。
關於構成所述塗佈織物的纖維基板(A)與塗層(B)之間的連結關係，如本文中所使用的「在纖維基板上形成塗層」意指藉由塗層形成材料在纖維基板(及/或形成纖維基板的纖維)的 表面上形成膜(塗層)。
根據本申請案的實施例，塗層(B)包括黏結劑樹脂及填料，其中填料以分散狀態存在於塗層或黏結劑樹脂中。此時，填料可包括切斷式陶瓷纖維及/或其團聚物。具體而言，填料可為呈團聚狀態的陶瓷塊狀纖維(ceramic bulk fiber，CBF)(即，團聚CBF(agglomerated CBF))。
在一個實施例中，纖維基板可包括非陶瓷纖維。舉例而言，纖維基板可包括有機纖維。當纖維基板包括陶瓷纖維時，氣囊織物所基本需要的例如拉伸強度、撕裂強度及伸長率等特性並不好。
包含於纖維基板中的有機纖維的類型並無特別限制。舉例而言，纖維基板可包含選自聚酯纖維、聚芳醯胺纖維、耐綸纖維、碳纖維(carbon fiber，CF)、聚酮纖維、纖維素纖維、聚烯烴纖維及丙烯酸纖維之中的至少一者。
在一個實施例中，包含於纖維基板中的纖維可具有在450分特(dtex)至1,100分特範圍內的細度(fineness)。具體而言，細度的下限可為例如500分特或大於500分特、550分特或大於550分特或者600分特或大於600分特，且其上限可為例如1000分特或小於1000分特、900分特或小於900分特、800分特或小於800分特、700分特或小於700分特或者600分特或小於600分特。當所使用的纖維的細度滿足以上範圍時，確保適當水準的輕重量性質及機械性質是有利的。
在一個實施例中，纖維基板可為織造織物(woven fabric)或非織造織物(non-woven fabric)，或者可包括其中的一或多者。
在一個實施例中，纖維基板可包括一或多個層。舉例而言，纖維基板可為包括二或更多個(織造)織物層的層疊體(laminate)、包括二或更多個非織造層的層疊體或者包括一或多個(織造)織物層及一或多個非織造層的層疊體。
纖維基板可具有低密度特性，以便確保用於氣囊的(塗佈)織物的可折疊性。
在一個實施例中，纖維基板可為包含經線(warp thread)及緯線(weft thread)的織物，且織物的經密(warp density)及緯密(weft density)可分別在20線/英吋(th/inch)至55線/英吋範圍內。具體而言，經線或緯線的密度的下限可為例如25線/英吋或大於25線/英吋、30線/英吋或大於30線/英吋、35線/英吋或大於35線/英吋、40線/英吋或大於40線/英吋或者45線/英吋或大於45線/英吋，且其上限可為例如50線/英吋或小於50線/英吋或者45線/英吋或小於45線/英吋。所述密度可根據國際標準組織(International Organization for Standardization，ISO)7211-2(3.07節)來量測，但並不特別限於此。
在傳統技術的情形中，為確保織物的氣密性(airtightness)以及防止氣囊充氣時的損壞(或破損(breakage))，考慮在經線及緯線中的至少一者中使用以高密度(例如，70線/英吋)織造的纖維基板。然而，使用如上所述的高密度織物不僅會阻礙氣囊重量 的減輕，而且使氣囊的可折疊性及可儲存性差。在本申請案中，由於使用如上所述的低密度織物，織物及氣囊可以輕重量製成，且在確保氣囊的可折疊性及可儲存性方面是有利的。具體而言，由於本申請案的塗佈織物具有下述塗層，因此其耐熱性及耐久性亦是極佳的。
如上所述，根據本申請案的塗佈織物的塗層包含陶瓷纖維作為填料。由於陶瓷纖維是短纖維，且在塗層中或在用於形成塗層的組成物中具有彼此團聚的趨勢，因此相較於其他類型的填料而言，其可提供充分的耐熱性及耐久性。本文中所使用的陶瓷纖維(例如，陶瓷塊狀纖維(CBF))具有更強的團聚趨勢。因此，相較於具有相同大小的陶瓷填料(即，不呈纖維形式的傳統陶瓷填料)而言，本文中所使用的陶瓷纖維可提供優越的耐熱性(參見以下評價2)。
舉例而言，在本申請案的實施例中，陶瓷纖維具有其中切斷式短纖維成束或團聚的形狀(塊狀形狀)。在塗層中，所述纖維形成多個團聚物(agglomerate)，且該些團聚物分散存在於塗層或黏結劑樹脂中。
如在以下實驗例中確認，相較於使用大的塗佈量的比較例1及使用雙層織物的比較例2而言，使用其中分散存在切斷式陶瓷纖維的團聚物的塗層的實例可具有更為極佳的耐熱性及耐久性。
在一個實施例中，陶瓷纖維(即，陶瓷塊狀纖維(CBF)) 可具有在0.1毫米至2.0毫米範圍內的大小。此時，CBF的大小可藉由已知的光學顯微鏡或類似物來確認，且可意指CBF的形狀的尺寸之中的最大尺寸的長度。
具體而言，CBF(陶瓷塊狀纖維)的大小可為例如0.15毫米或大於0.15毫米、0.20毫米或大於0.20毫米、0.25毫米或大於0.25毫米、0.30毫米或大於0.30毫米、0.35毫米或大於0.35毫米、0.40毫米或大於0.40毫米、0.45毫米或大於0.45毫米、0.50毫米或大於0.50毫米、0.55毫米或大於0.55毫米、0.60毫米或大於0.60毫米、0.65毫米或大於0.65毫米、0.70毫米或大於0.70毫米、0.75毫米或大於0.75毫米、0.80毫米或大於0.80毫米、0.85毫米或大於0.85毫米、0.90毫米或大於0.90毫米、0.95毫米或大於0.95毫米、1.0毫米或大於1.0毫米、1.05毫米或大於1.05毫米、1.10毫米或大於1.10毫米、1.15毫米或大於1.15毫米、1.20毫米或大於1.20毫米、1.25毫米或大於1.25毫米、1.30毫米或大於1.30毫米、1.35毫米或大於1.35毫米、1.40毫米或大於1.40毫米、1.45毫米或大於1.45毫米或者1.50毫米或大於1.50毫米。並且，陶瓷塊狀纖維(CBF)的大小的上限可為例如1.95毫米或小於1.95毫米、1.90毫米或小於1.90毫米、1.85毫米或小於1.85毫米、1.80毫米或小於1.80毫米、1.75毫米或小於1.75毫米、1.70毫米或小於1.70毫米、1.65毫米或小於1.65毫米、1.60毫米或小於1.60毫米、1.55毫米或小於1.55毫米、1.50毫米或小於1.50毫米、1.45毫米或小於1.45毫米、1.40毫米或小於1.40毫米、1.35 毫米或小於1.35毫米、1.30毫米或小於1.30毫米、1.25毫米或小於1.25毫米、1.20毫米或小於1.20毫米、1.15毫米或小於1.15毫米、1.10毫米或小於1.10毫米、1.05毫米或小於1.05毫米、1.0毫米或小於1.0毫米、0.95毫米或小於0.95毫米、0.90毫米或小於0.90毫米、0.85毫米或小於0.85毫米、0.80毫米或小於0.80毫米、0.75毫米或小於0.75毫米、0.70毫米或小於0.70毫米、0.65毫米或小於0.65毫米、0.60毫米或小於0.60毫米或者0.55毫米或小於0.55毫米。被團聚成具有以上範圍的CBF可提供極佳的耐熱性及耐久性。
在根據本申請案的實施例中，團聚物的分散度可相對於塗層的面積藉由在所述塗層中視覺辨別出的團聚物所佔用的面積來表達。舉例而言，團聚物可佔用範圍介於塗層的總面積的1%至25%的面積。此面積可藉由利用光學顯微鏡分析塗層的表面來計算。具體而言，填料的分散度可藉由以下方法來確認：確認塗層的一個表面的總面積，確認塗層的一個表面上由填料(團聚物)所佔用的面積，且然後計算填料(團聚物)所佔用的塗層的面積的百分數。此時，塗層可被劃分成多個區，且對於每一所劃分的區量測的面積及其比率可被計算為平均值(算術平均數)。就此而言使用的光學顯微鏡的類型並無特別限制。具體而言，由團聚物所佔用的面積對塗層的總面積的比率可為例如5%或大於5%或者10%或大於10%，且其上限可為例如20%或小於20%或者15%或小於15%。
在一個實施例中，陶瓷纖維可包含選自Si、Al、Ti、Zr、Ca及Mg之中的至少一者的氧化物、氮化物或碳化物。
在一個實施例中，陶瓷纖維可包含選自Si、Al、Ti、Zr、Ca及Mg之中的至少一者的氧化物。
在一個實施例中，陶瓷纖維可包含SiO2、CaO及MgO。如在以下實驗例中確認，當包含於塗層中的陶瓷纖維至少包含SiO2、CaO及MgO時，可確保極佳的耐熱性及耐久性。
在一個實施例中，陶瓷纖維可包含50重量%至60重量%的SiO2、20重量%至30重量%的CaO及10重量%至30重量%的MgO。如在以下實驗例中確認，當包含於塗層中的陶瓷纖維在以上含量範圍內包含SiO2、CaO及MgO時，可確保極佳的耐熱性及耐久性。
在一個實施例中，用於纖維基板的一個層的塗層的塗佈量可為100克每平方米(grams per square meter，gsm)(克/平方米(g/m2))或小於100gsm。具體而言，塗佈量的下限可為例如50gsm或大於50gsm、55gsm或大於55gsm、60gsm或大於60gsm、65gsm或大於65gsm、70gsm或大於70gsm、75gsm或大於75gsm、80gsm或大於80gsm、85gsm或大於85gsm、90gsm或大於90gsm或者95gsm或大於95gsm。並且，上限可為例如95gsm或小於95gsm、90gsm或小於90gsm、85gsm或小於85gsm、80gsm或小於80gsm、75gsm或小於75gsm、70gsm或小於70gsm、65gsm或小於65gsm或者60gsm或小於60gsm。一般而言，預期隨著 塗佈量的增加，由於塗佈而造成的效果增加。然而，由於本申請案的塗層是其中分散有陶瓷纖維填料的塗層，因此即使當塗佈量小時，亦可確保較不使用陶瓷纖維填料時或使用其他類型的填料時更高的塗佈效果(例如，耐熱性及耐久性)。塗佈量可根據ISO 3801(3.07節)來量測，但並不特別限於此。
在一個實施例中，包含於塗層中的黏結劑樹脂可包括選自矽酮樹脂及胺基甲酸酯樹脂之中的至少一者。矽酮樹脂或胺基甲酸酯樹脂的具體組分及性質並無特別限制。
根據本申請案的實施例，矽酮樹脂可用作黏結劑樹脂。在此種情形中，能夠形成矽酮黏結劑樹脂的材料的具體類型不受特別限制。舉例而言，矽酮樹脂可為或可包括藉由交聯或固化聚矽氧烷而形成的矽酮彈性體(silicone elastomer)。並且，已知能夠藉由加成聚合反應(polyaddition reaction)提供矽酮樹脂的矽氧烷化合物亦可用作所述矽酮黏結劑樹脂。另外，例如由埃肯矽酮(Elkem Silicones)製造的TCS 7516或TCS 7537等已知產品亦可用於形成包含所述矽酮黏結劑樹脂的塗層。
在一個實施例中，以總塗層的100重量%計，塗層可以20重量%或小於20重量%的量包含填料。此時，整個塗層的100重量%可意指以包含於塗層中的黏結劑樹脂及填料的固體含量計的總含量。作為另一選擇，以黏結劑樹脂、填料及其他組分(例如，添加劑)的固體含量計的總含量可視為整個塗層的100重量%。當填料的含量超過以上範圍時，塗佈溶液的黏度增加，且因此分 散不均勻，且無法充分獲得由於形成塗層而造成的效果。填料的含量的下限並無特別限制，且舉例而言，其可為1重量%或大於1重量%。具體而言，當考慮到由於使用填料而改善耐熱性及耐久性的效果時，使用至少5重量%的填料是較佳的。
在一個實施例中，具有以上構造的塗佈織物的重量(克/平方米)可為350克/平方米或小於350克/平方米。具體而言，塗佈織物的重量的上限可為例如340克/平方米或小於340克/平方米、330克/平方米或小於330克/平方米、320克/平方米或小於320克/平方米、310克/平方米或小於310克/平方米或者300克/平方米或小於300克/平方米，且其下限可為例如280克/平方米或大於280克/平方米、290克/平方米或大於290克/平方米、300克/平方米或大於300克/平方米或者310克/平方米或大於310克/平方米。當塗佈織物的重量超過以上上限時，難以降低重量，且織物製備成本可能增加。此外，當塗佈織物的重量小於以上下限時，機械性質可能降低。塗佈織物的重量可根據ISO 3801(3.07節)來量測，但並不特別限於此。
在一個實施例中，具有以上構造的塗佈織物的厚度可在0.25毫米至0.40毫米範圍內。此時，織物的厚度是基於塗佈織物的一個層。具體而言，厚度的下限可為0.26毫米或大於0.26毫米、0.27毫米或大於0.27毫米、0.28毫米或大於0.28毫米、0.29毫米或大於0.29毫米或者0.30毫米或大於0.30毫米，且其上限可為例如0.39毫米或小於0.39毫米、0.38毫米或小於0.38毫米、0.37 毫米或小於0.37毫米、0.36毫米或小於0.36毫米、0.35毫米或小於0.35毫米。當厚度小於以上範圍的下限時，難以確保充分的機械性質，且當厚度超過以上範圍時，可折疊性不好。厚度可根據ISO 5084(3.09節)來量測，但並不特別限於此。
在根據本申請案的另一實施例中，提供一種製備塗佈織物的方法。
具體而言，所述用於製備塗佈織物的方法包括將包含黏結劑樹脂及填料的組成物塗佈至纖維基板上，且然後固化所塗佈的組成物。
在此種情形中，填料包含切斷式陶瓷纖維或其團聚物。另外，關於黏結劑樹脂及填料的細節與上述者相同，且因此將被省略。
可執行塗佈，以使得可在纖維基板(及/或形成纖維基板的纖維)的表面上形成所述組成物的膜(塗層)。就此而言，用於將組成物塗佈至纖維基板上的方法並無特別限制，且可根據已知方法適當地執行。
在一個實施例中，固化可在室溫或高於室溫的溫度下執行。室溫是在不特別執行溫度升高或溫度降低的狀態下的溫度，且意指為約15℃至35℃的溫度。此外，大於或等於室溫的溫度是執行溫度升高的溫度，且可意指超過35℃的溫度，例如，在40℃至300℃範圍內的溫度。在所述溫度下的固化時間並無特別限制，且可執行例如數秒(second，sec)至數十分鐘(minute，min)的 固化。
在根據本申請案的又一實施例中，提供一種氣囊。所述氣囊包含上述塗佈織物。
關於包含於所述氣囊中的塗佈織物的構造及特性的細節與上述者相同，且因此其說明將被省略。
在一個實施例中，塗佈織物可用作用於氣囊的加強織物。此時，加強織物意指一種被填補以防止氣囊及類似物的充氣部中的氣囊緩衝墊織物受損壞的構造。就此而言，其中在氣囊的構造之中填補有所述加強織物的構造可被稱為主面板(main panel)。因此，氣囊被構造成包括主面板以及附接至主面板的至少局部區域的加強織物。
在一個實施例中，主面板可具有大於或等於加強織物的面積的面積。
在一個實施例中，主面板可包含織物，所述織物包含選自聚酯纖維、聚芳醯胺纖維、耐綸纖維、碳纖維、聚酮纖維、纖維素纖維、聚烯烴纖維及丙烯酸纖維之中的至少一者。
在一個實施例中，主面板可包括經線及緯線的密度的範圍介於45線/英吋至55線/英吋的織物。
在一個實施例中，主面板可具有塗層。主面板的塗層可包括眾所習知的矽酮樹脂或胺基甲酸酯樹脂，但不限於此。當執行塗佈時，塗佈量可為20gsm至40gsm，但並不特別限於此。
根據本申請案，即使當考慮到氣囊及塗佈織物的重量減輕以及氣囊緩衝墊的可折疊性及可儲存性而在輕重量織物上形成低密度塗層時，亦可提供具有極佳的耐熱性及耐久性的用於氣囊的塗佈織物。
圖1a至圖1d示意性地示出充氣機損壞評價方法及其結果。具體而言，圖1a是用於示意性地示出安裝用於評價的充氣機及織物的方法的影像，且圖1b、圖1c及圖1d是藉由分別拍攝實例1、比較例1及比較例2的耐熱性評價結果而獲得的影像。
圖2是利用光學顯微鏡拍攝的根據本申請案實施例的塗層的表面的影像。可確認，在較暗的陰影中視覺辨別出填料的團聚形式。在圖2中確認的填料的大小在0.1毫米至2.0毫米範圍內。
圖3a及圖3b是根據填料的類型示出耐熱性及耐久性評價結果(熱棒評價(hot-rod evaluation))以及團聚特性的比較的圖。具體而言，圖3a是示出CBF(陶瓷塊狀纖維)在經歷熱棒評價的過程中提供更佳的耐熱性及耐久性的實驗結果。此外，圖3b是用於闡釋耐熱性及耐久性相依於填料的類型以及團聚特性而不同的原因的示意圖。如圖3b中所示，由於相較於其他陶瓷填料而言，CBF具有更強的團聚趨勢，因此在高溫/高壓條件下可抑制對塗層形成樹脂的損壞。
在下文中，將參照本發明的具體實例更詳細地闡述本發明的作用及效果。然而，該些實例僅是出於例示性目的而呈現，且因此本發明的範圍不以任何方式受到限制。
實例及比較例
實例1
塗佈組成物的製備：製備出了包含由埃肯矽酮製造的TCS 7516(其為矽酮系黏結劑樹脂)及陶瓷塊狀纖維(由55重量%的SiO2、25重量%的CaO及20重量%的MgO構成的陶瓷纖維)的組成物。此時，將陶瓷塊狀纖維的含量調節成在最終固化的塗層中為約10重量%。
塗佈織物的製備：自具有為550分特的細度的PET纖維製備出了織物。具體而言，製備出了具有為46×46線/英吋(經×緯)的織物密度的織物(1層)，且將所製備的組成物以約87gsm的水準塗佈至所述織物上。然後，使用熱空氣腔室在為160℃至190℃的溫度下施行固化達至少1分30秒，且製備出了織造織物。所製備的塗佈織物的重量為315克/平方米，且厚度為約0.33毫米(參見圖2)。
比較例1
塗佈組成物的製備：將由埃肯矽酮製造的TCS 7517製備為矽酮系黏結劑樹脂。
塗佈織物的製備：自具有為470分特的細度的PA66纖維製備出了織物。具體而言，製備出了具有為46×46線/英吋(經 ×緯)的織物密度的織物(1層)。然後，將所製備的塗佈組成物以約122gsm的水準塗佈至所製備的織物上(塗佈量較在實例1中多約50gsm)，且然後在與實例1中相同的條件下進行了固化。所製備的塗佈織物的重量為308克/平方米，且厚度為約0.33毫米。
比較例2
塗佈組成物的製備：製備出了由道康寧(Dow Corning)製造的DC3730，其為胺基甲酸酯系黏結劑樹脂。
塗佈織物的製備：自具有為470分特的細度的PA66纖維製備出了織物。具體而言，製備出了具有112×96線/英吋(經×緯)的織物密度的織物(黏結的2層)。不同於實例及比較例1，使用了雙層織物。然後，將所製備的組成物以為約69gsm的水準塗佈至織物上。所製備的塗佈織物的重量為512克/平方米，且厚度為約0.66毫米。
評價1：塗佈織物的耐熱耐久性的評價
藉由以下方法評價了在實例及比較例中製備出的塗佈織物的耐熱性。
1.熱棒評價
具體而言，製備出了柱狀棒(直徑為10毫米，長度為80毫米，且重量為50克)，且將所述棒加熱至所期望的600℃，並使其與塗佈織物接觸。然後，量測了直至所述棒完全熔化所述織物且然後落下為止的時間(以秒計)，且結果示出於下表1中。
2.充氣機損壞評價
將熱屏蔽織物作為單層包裹於用於駕駛員氣囊(driver’s airbag，DAB)(百利得安全系統(Key Safety Systems，KSS))的雙充氣機(dual inflator)的夾具內部，並將實例及比較例的塗佈織物包裹成6層以製備樣本(參見圖1a)。然後，對展開氣囊的過程進行了仿真，以使得將高溫及高壓氣體施加至樣本。此時，將高溫及高壓氣體控制成以為180千帕至270千帕的最大壓力施加達40毫秒至80毫秒。
然後，量測了五層式(five-ply)塗佈織物之中的受損壞織物的數目(n)及在該些受損壞織物中發現的孔的數目(m)，並將n的加權值設定為10且將m的加權值設定為1，並將評價結果數字化如下。損壞評分越低，則耐熱性越佳。
損壞評分=(n×10)+(m×n×1)
Figure 110149009-A0305-02-0017-1
評價2：由填料帶來的耐熱性及耐久性的比較
如圖3a中所示，改變了在實例1中製備的塗佈織物的填料類型，並對上述熱棒評價結果進行了比較。具體而言，以5重量%同等地施加塗層中的填料的含量，且針對使用CBF(陶瓷塊狀纖維)、傳統陶瓷填料(雲母(D50數目分佈大小(D50 number distribution size)為約40微米)、二氧化矽(D50數目分佈大小為 約20微米至30微米)、滑石(D50數目分佈大小為約20微米至30微米))及CF(碳纖維)填料(大小為約2毫米至3毫米)的情形進行了熱棒評價。Y軸結果是在評價推進了約10次之後的算術平均值(單位：秒)。

Claims (12)

  1. 一種塗佈織物，包括：纖維基板(A)以及形成於所述纖維基板上的塗層(B)，其中所述塗層包含黏結劑樹脂及填料，其中所述填料分散於所述塗層中，其中所述填料包含切斷式陶瓷纖維及其團聚物中的至少一者，且其中所述切斷式陶瓷纖維包含SiO2、CaO及MgO。
  2. 如請求項1所述的塗佈織物，其中：所述切斷式陶瓷纖維包含50重量%至60重量%的SiO2、20重量%至30重量%的CaO及10重量%至30重量%的MgO。
  3. 如請求項1所述的塗佈織物，其中：所述黏結劑樹脂包含選自胺基甲酸酯樹脂及矽酮樹脂之中的至少一者。
  4. 如請求項1所述的塗佈織物，其中：以整個所述塗層的100重量%計，所述塗層以20重量%或小於20重量%的量包含所述填料。
  5. 如請求項1所述的塗佈織物，其中：所述塗層對所述纖維基板的一個層的塗佈量為100克每平方米或小於100克每平方米。
  6. 如請求項1所述的塗佈織物，其中：所述纖維基板包含選自聚酯纖維、聚芳醯胺纖維、耐綸纖維、 碳纖維、聚酮纖維、纖維素纖維、聚烯烴纖維及丙烯酸纖維之中的至少一者。
  7. 如請求項6所述的塗佈織物，其中：包含於所述纖維基板中的纖維具有在450分特至1,100分特範圍內的細度。
  8. 如請求項6所述的塗佈織物，其中：所述纖維基板是包括經線及緯線的織物，且所述織物的經密及緯密分別在20線/英吋至55線/英吋範圍內。
  9. 如請求項1所述的塗佈織物，其中：所述塗佈織物具有為350克/平方米或小於350克/平方米的重量。
  10. 如請求項1所述的塗佈織物，其中：所述塗佈織物具有為0.25毫米至0.40毫米的厚度。
  11. 一種用於製備塗佈織物的方法，包括：將包含黏結劑樹脂及填料的塗佈組成物塗佈至纖維基板上，且然後固化所塗佈的所述塗佈組成物，其中所述填料包含切斷式陶瓷纖維及其團聚物中的至少一者，且其中所述切斷式陶瓷纖維包含SiO2、CaO及MgO。
  12. 一種氣囊，包括如請求項1所述的塗佈織物。
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