M435807 五、新型說明： 【新型所屬之技術領域】 本創作係關於一種吸震裝置，特別是一種利用氣 囊結構提供吸震效果之吸震裝置。 【先前技術】 隨著電子裝置之便攜性及輕薄化設計，其所使用 之各類電子零組件亦越來越精密且具有更小體積。以可 攜式電腦為例，由於其内部包括一些在使用狀態下會產 生振動之必要零組件，例如剩°八、散熱風扇等，而這些 振動有可能會透過電腦機殼或其他元件傳遞出去，進而 影響部分較精密零組件之精準度或效能，例如運用於資 料存取之硬碟或光碟機等，如此將可能導致系統不穩定 或資料存取發生問題。 因此，在可攜式電腦之裝置設計上如何能提供更 有效的振動抑止設計，以避免振動源直接傳遞振動至硬 碟或光碟機等零組件，實為一值得研究之課題。 【新型内容】 本創作之主要目的係提供一種利用氣囊結構提供 吸震效果之吸震裝置。 為達成上述之目的，本創作之吸震裝置係設置於 3 M435807 電子裝置中之震動元件與殼體之間，殼體包括固定座。 吸震裝置包括環狀氣囊組件及貫通部。環狀氣囊組件包 括至少一氣囊結構，各氣囊結構包括第一支撐部及第二 支撐部。第一支撐部用以連接震動元件；第二支撐部係 連接於第一支撐部，且第二支撐部之外徑與第一支撐部 之外徑之間形成支承面，供第二支撐部支承震動元件； 貫通部係位於環狀氣囊組件之中心部位，貫通部具有二 開放端，且貫通部供環狀氣囊組件連接於殼體之固定座 _ 上。 在本創作之一實施例中，至少一氣囊結構為單一 環狀氣囊結構；其中單一環狀氣囊結構更包括至少一内 凸出部，各内凸出部係徑向地朝内凸設。單一環狀氣囊 結構更包括至少一外凸出部，各外凸出部係自第一支撐 部徑向地朝外凸設。 在本創作之一實施例中，至少一氣囊結構為複數 # 氣囊結構；其中各氣囊結構更包括内凸出部，係徑向地 朝内凸設。其中各氣囊結構更包括外凸出部，係自第一 支撐部徑向地朝外凸設。 在本創作之一實施例中，各氣囊結構之第一支撐 部為一支撐懸臂，係連接於第二支撐部之支承面，且第 一支撐部係與對應之内凸出部保持一間距。 藉此設計，本創作之吸震裝置可藉由氣囊結構内 4 M435.807 之充填氣體達到吸震效果，並配合結構設計減少吸震裝 置與震動元件及/或殼體間之接觸面積，以減少振動傳 遞之路徑及能量。 由於本創作構造新穎，能提供產業上利用，且確 有增進功效，故依法申請新型專利。 【實施方式】 為了讓本創作之上述和其他目的、特徵和優點能 .更明顯易僅’下文特舉出本創作之具體實施例，並配合 所附圖式，作詳細說明如下。 在下述各實施例中，本創作之吸震裝置係應用於 電子裝置上’藉由本創作之吸震裝置設置於電子裝置之 震動元件及殼體之間。該電子裝置係為可攜式電腦、智 慧型手機、GPS、PDA等，亦可為桌上型電腦或其他設 置有震動元件（料、風料）之電子裝置，本創作並 不以此為限。 請參考圖1係本創作之吸震裝置丨之設置示意圖。 如圖1所示，本創作之吸震裝置丨設置於電子裝 置80之震動元件81及殼體82之間。電子裝置8〇之殼 體82可設置對應數量之固定座821 (例如圖丨共設置2 組固定座821)，而利用本創作之吸震裝置1之-端固 定於對應之固定座821上，並將震動元件 81兩側之固 5 M435807 定孔811分別結合於吸震裝置1之另一端，即可完成震 動元件81之組裝，以藉由本創作之吸震裝置1提供吸 震效果。在本實施例中，震動元件81係為喇八裝置， 本創作不以此為限。 請一併參考圖2及圖3。圖2係本創作之吸震裝置 1之第一實施例之立體結構圖。圖3係本創作之吸震裝 置1之第一實施例於使用狀態下之剖面圖。 如圖2及圖3所示，本創作之吸震裝置丨包括環 狀氣囊組件10及貫通部2〇。環狀氣囊組件ι〇包括至 少-氣囊結構1卜在本實施例中，至少_氣囊結構^ 係為-體成型之單-環狀氣囊結構，而貫通部係位 於環狀氣囊組件10之中心部位，貫通部2G具有二開放 端，使得貫通部20以-通道形式自環狀氣囊組件^之 -端貫通另-端。氣囊結構u Μ之中空部可充填氣 體’例如—般空氣錢㈣惰性氣體；而環狀氣囊组件 10可採用具彈性之聚合或塑性材料製成。 此氣囊結構U包括第一支撐部U1及第二 112°第一支標部111用以連接震動元件81之固定《 81卜固定部811係直接套設於第一支稽部⑴上·: 二支標部112錢接於第―支撐部111，第二支撐部 之外徑Μ大於第-支擇部lu之外經叫， 部112之外徑D2與第—切部⑴之外徑 M435807 成支承面1121。於固定震動元件81時，此支承面1121 可供第二支撐部112支承震動元件81。 貫通部20用以供環狀氣囊組件10連接於殼體82 之固定座821上，且藉由貫通部20之設置使得環狀氣 囊組件10之内徑D3小於第一支撐部111之外徑D1及 第二支撐部112之外徑D2。 請一併參考圖2及圖4。圖4係本創作之吸震裝置 1之第一實施例於使用狀態下之俯視圖。 如圖2及圖4所示，在本實施例中，氣囊結構_ 11 更包括複數個内凸出部113，各内凸出部113係徑向地 朝内凸設，即凸設於氣囊結構11形成貫通部20之内 壁，用以減少固定座821與環狀氣囊組件10之接觸面 積。當環狀氣囊組件10套設於固定座821上時，藉由 凸設之複數個内凸出部113，使得環狀氣囊組件10與 固定座821之間僅形成複數線接觸，而能大幅減少環狀 氣囊組件10與固定座821間之接觸面積。此外，在設 計上可令固定座821之徑長不小於貫通部20中心至内 凸出部113之距離，以使環狀氣囊組件10能較緊密地 套設於固定座821上。此處各内凸出部113係採用一半 圓柱形式，延伸至貫通部20之兩端端口，但本創作不 以此為限。而内凸出部113之設置數量可依設計不同而 改變，在本創作之較佳實施例中，氣囊結構11可包括 7 M435807 至少二個内凸出部113，以與固定座821形成如正三角 形頂點之至少二個接觸位置（如圖所示則為矩形之四個 接觸位置）’但不以本實施例為限。 氣囊結構11更包括複數個外凸出部114,各外凸出 部114係自第一支撐部U1徑向地朝外凸設，即凸設於 第一支撐部111之外側表面’用以減少震動元件之 固定部811與第一支擇部U1之接觸面積。當震動元件 81之固定部811套設於第一支撐部lu上時，藉由凸設 之複數個外凸出部114，使得固定部8U與第一支撐部 1Π之間僅形成複數線接觸，而能大幅減少固定部811 與第-支撐部111間之接觸面積。此外，在設計上可令 固定部811之孔徑長度不大於第一支撐部111之外徑加 上外凸出部U4之厚度，以使震動元件81之固定部811 能較緊密地套設於第—支擇部U1上。此處各外凸出部 114係採用一半圓柱形式’自第二支撐部112之支承面 延伸至第一支樓部111之頂端’並可與前述内凸出部 113搭配以形成類似整體圓柱狀之結構，但本創作不以 此為限。此外，外凸出部113之設置數量亦可 凸出部依設計不同而改變，不以本實施例為限。“ 請參考圖5係本創作之吸震裝置la之第二實施例 之結構立體圖。 本實施例係為前述第__實施例之變化形式。如圖$ M435807 所示，在本實施例中，氣囊結構Ua之複數個内凸出部 113a係徑向地朝内凸設’而各内凸出部113a係採用環 狀形式之結構，藉以使得環狀氣囊組件1 〇a與固定座 (圖未示）之間僅形成複數環狀之線接觸，亦能大幅減 少環狀氣囊組件l〇a與固定座間之接觸面積。但本創作 並不以此為限。 請參考圖6係本創作之吸震裝置lb之第三實施例 之剖視圖。 本實施例亦為前述第一實施例之變化形式。如圖6 所示，在本實施例中，第二支撐部112b之支承面U2ib 包括至少一上凸出結構1122b，用以減少震動元件821 與第二支撐部112b之接觸面積。在本實施例_，上凸 出結構1122b係採用一環狀凸起結構，但上凸出結構 1122b亦可為凸點、凸塊或其他形式之上凸出結構，不 以本實施例為限》 請參考圖7係本創作之吸.震裝置lc之第四實施例 之結構立體圖。 本實施例係為前述第一實施例之變化形式。如圖 7所不，在本實施例中，為了避免採用單一氣囊結構於 軋囊破損時將會失去吸震效果，本創作之吸震裝置化 之環狀氣囊組件10C係設計為複數氣囊結構llc，相鄰 之二氣囊結構11C間係以實心之彈性材料或連接件彼此 9 連接’但彼此氣囊各自獨立，以構成環狀結構；而貫通 部20c係為複數氣囊結構Uc所圍繞而成之環狀結構之 中空部位，以近似一通道形式自環狀氣囊組件l〇c之一 端貫通另一端。 各氣囊結構11c包括第一支撐部111c及與其連接 之第二支撐部112c，而藉由複數氣囊結構Uc進而形成 複數第一支撐部111c及複數第二支撐部112c (並以複 數第二支撐部112形成複數支承面1121c)’以提供如同 前述圖2中第一實施例之第一支撐部ill及第二支撐部 之結構特徵與功能，在此不多加贅述。此外，氣囊 結構11c之設置數量可依設計不同而改變，在本創作之 一實施例中，可包括至少三個氣囊結構11c，以提供穩 定支撐之效果，而相鄰之氣囊結構11c可透過連接件彼 此連接’但氣囊結構11c之設置數量及連接方式不以此 實施例為限。 其中各氣嚢結構11c更包括内凸出部113c，係徑. 向地朝内凸設，用以減少殼體之固定座（圖未示）與環 狀氣囊組件l〇c之接觸面積。在本實施例中，各氣囊結 構11c係於朝内側處採用一半圓柱形式之外形以作為内 凸出部113c。因此，藉由複數氣囊結構11c所形成之複 數個内凸出部113c，使得環狀氣囊組件10c與固定座之 間僅形成複數線接觸，而減少環狀氣囊組件1〇與固定 座間之接觸面積。 各氣囊結構11c更包括外凸出部 114c，係自第一 支撐部111c徑向地朝外凸設，用以減少震動元件（圖 未不）與第一支撐部lllc之接觸面積。在本實施例中， 各氣囊結構lie係於第—支撐部1Ue朝外侧處採用一 半圓柱形式之外形以作為外凸出部n4e。因此，藉由複 數氣囊結構11c所形成之複數個外凸出部U4c，使得環 狀I囊組件l〇e與震動元件之間僅形成複數線接觸，而 減少锿狀.氣囊組件i 0c與固定座間之接觸面積。其中外 凸出部114c並可與前述内凸出部U3c搭配以形成類似 整體圓柱狀之結構’但本創作不以此為限。 請一併參考® 8及® 9。圖8係本創作之吸震裝置 Id之第五實〜例之結構立體圖。圖9係本創作之吸震 裝置Id之第五實施例之刮視圖。 本實施例係為前述第四實施例之變化形式。如圖 8及圖9所在本實施例中，本創作之吸震裝置id 之環狀氣囊組件1Gd係設計以複數氣囊結構nd所圍繞 而成之環狀t構，其中各氣囊結構Ud更包括内凸出部 U3d’係徑向地朝内凸設。而各氣囊結構Ud之第一支 撐部llld採用-支㈣臂之設計，其係連接於第二支 揮部md之支承面1121d，且第—支撐部iiid係與對 »«之内凸出。p 113d保持-間距B。其中第—支樓部lud 11 M435807 包括—凹槽mid，該凹槽自第一支撐部111(1延伸至第 二支撐部112d之支承面1121d ,以供卡合震動元件。 本創作之吸震裝置id藉由複數氣囊結構lld形成 複數第一支撐部llld及複數第二支撐部112d (並以複 數第二支撐部112形成複數支承面H21C1)。本創作之吸 震裝置id可藉由貫通部20d固定於殼體82之固定座 821上。於固定震動元件81時，由於各第一支撐部Uld 可自由擺動，使得震動元件81之固定部811可對應卡 入複數第一支撐部llld之複數凹槽11Ud内，並藉由 第二支撐部112d之支承面1121d支承震動元件81。 當震動元件81產生振動能量並傳遞至本創作之吸 震裝置Id時，藉由第一支撐部md如同彈簧一般之擺 動變形（如圖9中虛線所示可吸收並消耗多餘能量 之傳遞，已達到吸震效果，減少振動傳遞至殼體之可能 性。 又如圖1所示，本創作更包括應用於電子裝置80 之吸震模組，該吸震模組包括殼體82、震動元件81及 至少一如前所述之環狀氣囊組件1。殼體82包括至少 一固定座821 ;震動元件81係設置於殼體82 ,其包括 至少一固定孔811;各環狀氣囊組件丨係設置於震動元 件81與殼體82之間，其一端固定於殼體82之固定座 821上，另一端則連接震動元件81之固定孔811，以減 12 /震動自震動7〇件81傳遞至殼體.各環狀氣囊組件 1而各钱氣囊崎丨之結構設計已於前述各實施例中 敘明，在此不多加贅述。 應注忍的疋’上述諸多實施例僅係為了便於說明 而舉例而已，本創作所主張之制制自絲中請專利 範圍所述為準，而非僅限於上述實施例。 【圖式簡單說明】 圖1係本創作之吸震裝置之設置示意圖。 圖2係本創作之吸震裝置之第一實施例之立體結構圖。 圖3係本創作之吸震裝置之第一實施例於使用狀態下 之剖面圖。 圖4係本創作之吸震裝置之第一實施例於使用狀態下 之俯視圖。 圖5係本創作之吸震裝置之第二實施例之結構立體圖。 圖6係本創作之吸震裝置之第三實施例之剖視圖。 圖7係本創作之吸震裝置之第四實施例之結構立體圖。 圖8係本創作之吸震裝置之第五實施例之結構立體圖。 圖9係本創作之吸震裝置之第五實施例之剖視圖。 【主要元件符號說明】 吸震裝置 1、la、lb、1 c、Id M435807 環狀氣囊組件10、l〇a、10b、10 c、lOd 氣囊結構 1卜 11a、lib、11 c、lid 第一支撐部 m、111a、111b、111 c、llld 凹槽mid 第二支撐部 112、112a、112b、112 c、112d 支承面 1121、1121c、1121d 上凸出結構1122b 内凸出部 113、113a、113 c、113d 外凸出部 114、114a、114c 貫通部20 電子裝置80 震動元件81 固定部811 殼體82 固定座821 外徑 Dl、D2、D3M435807 V. New description: [New technical field] This creation is about a shock absorbing device, especially a shock absorbing device that uses a gas capsule structure to provide shock absorbing effects. [Prior Art] As the electronic device is portable and thin and light, the various electronic components used are more and more precise and have a smaller volume. Taking a portable computer as an example, since the inside thereof includes some necessary components that generate vibration under use, such as a residual fan, a cooling fan, etc., these vibrations may be transmitted through a computer case or other components. This in turn affects the accuracy or performance of some of the more sophisticated components, such as hard drives or optical drives used for data access, which may cause system instability or data access problems. Therefore, how to provide more effective vibration suppression design in the design of the portable computer device to avoid the vibration source directly transmitting vibration to the components such as the hard disk or the optical disk drive is a subject worthy of study. [New content] The main purpose of this creation is to provide a shock absorbing device that uses a balloon structure to provide shock absorbing effects. In order to achieve the above purpose, the shock absorbing device of the present invention is disposed between the vibration element and the housing in the 3 M435807 electronic device, and the housing includes a fixing base. The shock absorbing device includes an annular air bag assembly and a through portion. The annular air bag assembly includes at least one air bag structure, and each air bag structure includes a first support portion and a second support portion. The first supporting portion is for connecting the vibration component; the second supporting portion is connected to the first supporting portion, and the outer diameter of the second supporting portion and the outer diameter of the first supporting portion form a bearing surface for the second supporting portion to support The vibration component; the penetration portion is located at a central portion of the annular airbag module, the penetration portion has two open ends, and the penetration portion is connected to the annular airbag module to the fixed seat of the housing. In one embodiment of the present invention, at least one of the airbag structures is a single annular airbag structure; wherein the single annular airbag structure further includes at least one inner projection, each of the inner projections protruding radially inwardly. The single annular balloon structure further includes at least one outer projection, each of the outer projections projecting radially outward from the first support portion. In one embodiment of the present invention, at least one of the airbag structures is a plurality of airbag structures; wherein each of the airbag structures further includes an inner projection that projects radially inwardly. Each of the airbag structures further includes an outer protrusion that protrudes radially outward from the first support portion. In one embodiment of the present invention, the first support portion of each of the airbag structures is a support cantilever that is coupled to the support surface of the second support portion, and the first support portion is spaced from the corresponding inner projection. With this design, the shock absorbing device of the present invention can achieve the shock absorbing effect by the filling gas of 4 M435.807 in the airbag structure, and the structural design can reduce the contact area between the shock absorbing device and the vibration component and/or the shell to reduce the vibration transmission. The path and energy. Due to the novel structure of this creation, it can provide industrial use, and it has improved efficiency. Therefore, it applies for a new type of patent according to law. [Embodiment] The above and other objects, features and advantages of the present invention will become apparent from the following description. In the following embodiments, the shock absorbing device of the present invention is applied to an electronic device. The shock absorbing device of the present invention is disposed between the vibration element of the electronic device and the casing. The electronic device is a portable computer, a smart phone, a GPS, a PDA, etc., and can also be a desktop computer or other electronic device provided with a vibration component (material, wind material), and the creation is not limited thereto. . Please refer to Figure 1 for the setting of the shock absorbing device. As shown in FIG. 1, the shock absorbing device of the present invention is disposed between the vibration element 81 of the electronic device 80 and the housing 82. The housing 82 of the electronic device 8 can be provided with a corresponding number of fixing seats 821 (for example, a total of two sets of fixing bases 821 are provided), and the end of the shock absorbing device 1 of the present invention is fixed to the corresponding fixing seat 821, and The fixing of the vibrating member 81 is completed by combining the fixed 5 M435807 fixed holes 811 on both sides of the vibrating member 81 to the other end of the shock absorbing device 1 to provide the shock absorbing effect by the shock absorbing device 1 of the present invention. In the present embodiment, the vibrating element 81 is a device, and the present invention is not limited thereto. Please refer to Figure 2 and Figure 3 together. Fig. 2 is a perspective structural view showing a first embodiment of the shock absorbing device 1 of the present invention. Fig. 3 is a cross-sectional view showing the first embodiment of the shock absorbing device 1 of the present invention in use. As shown in Figs. 2 and 3, the shock absorbing device of the present invention includes a ring-shaped airbag module 10 and a through portion 2A. The annular airbag module ι includes at least an airbag structure 1. In the present embodiment, at least the airbag structure is a body-formed single-annular airbag structure, and the through portion is located at a central portion of the annular airbag module 10. The through portion 2G has two open ends such that the through portion 20 penetrates the other end from the end of the annular airbag module in the form of a channel. The hollow portion of the airbag structure u can be filled with a gas such as an inert gas, and the annular airbag module 10 can be made of a flexible polymeric or plastic material. The airbag structure U includes a first support portion U1 and a second 112° first branch portion 111 for connecting the fixing of the vibration element 81. The 81-fixed portion 811 is directly sleeved on the first branch portion (1). The branch portion 112 is connected to the first support portion 111, and the outer diameter Μ of the second support portion is larger than the first support portion lu, and the outer diameter D2 of the portion 112 is equal to the outer diameter M435807 of the first cut portion (1). Support surface 1121. When the vibrating member 81 is fixed, the supporting surface 1121 can support the second supporting portion 112 to support the vibrating member 81. The through portion 20 is configured to connect the annular airbag module 10 to the fixing base 821 of the housing 82, and the inner diameter D3 of the annular airbag module 10 is smaller than the outer diameter D1 of the first supporting portion 111 by the arrangement of the through portion 20. And an outer diameter D2 of the second support portion 112. Please refer to Figure 2 and Figure 4 together. Fig. 4 is a plan view showing the first embodiment of the shock absorbing device 1 of the present invention in use. As shown in FIG. 2 and FIG. 4 , in the embodiment, the airbag structure _ 11 further includes a plurality of inner protrusions 113 , and the inner protrusions 113 are radially inwardly convex, that is, protruded from the airbag structure. 11 forms an inner wall of the through portion 20 for reducing the contact area of the fixed seat 821 with the annular airbag module 10. When the annular airbag module 10 is sleeved on the fixing base 821, only a plurality of inner protruding portions 113 are protruded, so that only a plurality of line contacts are formed between the annular airbag module 10 and the fixing base 821, which can be greatly reduced. The contact area between the annular airbag module 10 and the fixing base 821. Further, it is designed such that the diameter of the fixing base 821 is not less than the distance from the center of the through portion 20 to the inner protruding portion 113, so that the annular airbag module 10 can be tightly fitted on the fixing base 821. Here, each of the inner projections 113 is of a semi-cylindrical shape and extends to the ports at both ends of the penetration portion 20, but the present invention is not limited thereto. The number of the inner protrusions 113 can be changed according to the design. In the preferred embodiment of the present invention, the airbag structure 11 can include 7 M435807 at least two inner protrusions 113 to form a positive relationship with the fixing base 821. At least two contact positions of the apex of the triangle (four contact positions of the rectangle as shown) 'but not limited to this embodiment. The airbag structure 11 further includes a plurality of outer protrusions 114. The outer protrusions 114 are radially outwardly protruded from the first support portion U1, that is, protruded from the outer surface of the first support portion 111 to reduce The contact area between the fixing portion 811 of the vibrating element and the first connecting portion U1. When the fixing portion 811 of the vibrating member 81 is sleeved on the first supporting portion lu, only a plurality of outer protruding portions 114 are protruded, so that only a plurality of line contacts are formed between the fixing portion 8U and the first supporting portion 1? Further, the contact area between the fixed portion 811 and the first support portion 111 can be greatly reduced. In addition, the length of the aperture of the fixing portion 811 is not greater than the outer diameter of the first supporting portion 111 plus the thickness of the outer protruding portion U4, so that the fixing portion 811 of the vibrating member 81 can be tightly sleeved on the first portion. - on the selection part U1. Here, each of the outer projections 114 is semi-cylindrical 'extending from the bearing surface of the second supporting portion 112 to the top end of the first branch portion 111' and can be matched with the aforementioned inner protruding portion 113 to form a similar overall cylindrical shape. The structure, but this creation is not limited to this. In addition, the number of the outer projections 113 may be changed depending on the design, and is not limited to the embodiment. Please refer to Fig. 5 is a perspective view showing the structure of the second embodiment of the shock absorbing device la of the present invention. This embodiment is a variation of the foregoing __ embodiment. As shown in Fig. M435807, in the present embodiment, the airbag The plurality of inner projections 113a of the structure Ua are radially inwardly convex and the inner projections 113a are in the form of an annular form, whereby the annular airbag module 1 〇a and the fixed seat are not shown. Only a plurality of annular line contacts are formed between them, and the contact area between the annular airbag module 10a and the fixed seat can be greatly reduced. However, the present invention is not limited thereto. Please refer to FIG. 6 for the shock absorbing device of the present invention. A cross-sectional view of the third embodiment of the first embodiment. The embodiment is also a variation of the first embodiment. As shown in Fig. 6, in the embodiment, the support surface U2ib of the second support portion 112b includes at least one upper projection. The structure 1122b is configured to reduce the contact area between the vibrating element 821 and the second supporting portion 112b. In the embodiment, the upper protruding structure 1122b adopts an annular convex structure, but the upper protruding structure 1122b may also be a bump. , bumps or other forms of convex structures, Please refer to FIG. 7 for a perspective view of the structure of the fourth embodiment of the shock absorbing device 1c. The present embodiment is a variation of the foregoing first embodiment. In this embodiment, in order to avoid the use of a single airbag structure, the shock absorbing effect will be lost when the rolled cap is damaged. The shock absorbing device of the present invention is designed as a plurality of airbag structures 11c, and the adjacent two airbag structures 11C. The inter-series are connected to each other by a solid elastic material or a connecting member, but the airbags are independent of each other to constitute a ring-shaped structure, and the penetrating portion 20c is a hollow portion of the annular structure surrounded by the plurality of airbag structures Uc to approximate One channel forms from one end of the annular airbag module 10c through the other end. Each of the airbag structures 11c includes a first support portion 111c and a second support portion 112c connected thereto, and a plurality of first supports are formed by the plurality of airbag structures Uc. a portion 111c and a plurality of second support portions 112c (and a plurality of second support portions 112 form a plurality of support surfaces 1121c) to provide a first support portion ill as in the first embodiment of FIG. 2 and The structural features and functions of the second support portion are not described here. In addition, the number of the airbag structures 11c may vary depending on the design. In one embodiment of the present invention, at least three airbag structures 11c may be included. The effect of the stable support is provided, and the adjacent airbag structures 11c can be connected to each other through the connecting member. However, the number and connection manner of the airbag structure 11c are not limited to this embodiment. The air venting structure 11c further includes an inner protruding portion. 113c, the diameter of the ground is convex toward the ground to reduce the contact area between the fixing seat (not shown) of the casing and the annular airbag module 10c. In this embodiment, each airbag structure 11c is attached to A half cylindrical outer shape is used as the inner convex portion 113c at the inner side. Therefore, by the plurality of inner protrusions 113c formed by the plurality of airbag structures 11c, only a plurality of line contacts are formed between the annular airbag module 10c and the fixing seat, and the contact area between the annular airbag module 1 and the fixed seat is reduced. . Each of the airbag structures 11c further includes an outer protruding portion 114c protruding radially outward from the first supporting portion 111c for reducing the contact area of the vibrating member (not shown) with the first supporting portion 111c. In the present embodiment, each of the airbag structures lie is formed in a semi-cylindrical shape as the outer projection n4e at the outer side of the first support portion 1Ue. Therefore, by the plurality of outer protrusions U4c formed by the plurality of airbag structures 11c, only the plurality of line contacts are formed between the annular I capsule assembly 10e and the vibration element, thereby reducing the shape of the bellows. The airbag module i0c and the fixing The contact area between the seats. The outer protruding portion 114c may be combined with the inner protruding portion U3c to form a structure similar to a whole cylindrical shape, but the present invention is not limited thereto. Please refer to ® 8 and ® 9 together. Fig. 8 is a perspective view showing the structure of the fifth embodiment of the shock absorbing device Id of the present invention. Figure 9 is a plan view of a fifth embodiment of the shock absorbing device Id of the present invention. This embodiment is a variation of the aforementioned fourth embodiment. As shown in FIG. 8 and FIG. 9 , the annular airbag module 1Gd of the shock absorbing device id of the present invention is designed as an annular t-shaped structure surrounded by a plurality of airbag structures nd, wherein each airbag structure Ud further includes a convex inner body. The outlet U3d' is projecting radially inwardly. The first support portion llld of each of the airbag structures Ud is designed to be a branch (four) arm, which is connected to the support surface 1121d of the second support portion md, and the first support portion iiid is protruded from the inside of the pair. p 113d hold - pitch B. The first branch portion lud 11 M435807 includes a groove mid, and the groove extends from the first support portion 111 (1) to the support surface 1121d of the second support portion 112d for engaging the vibration element. The shock absorbing device of the present invention The id is formed by the plurality of first airbag structures 11d and the plurality of second support portions 112d (and the plurality of second support portions 112 form a plurality of support surfaces H21C1). The shock absorbing device id of the present invention can be fixed by the through portion 20d. The fixing portion 811 of the vibration element 81 can be correspondingly engaged with the plurality of grooves of the plurality of first supporting portions 111d. In the 11Ud, the vibrating member 81 is supported by the supporting surface 1121d of the second supporting portion 112d. When the vibrating member 81 generates vibration energy and transmits it to the shock absorbing device Id of the present invention, the first supporting portion md swings like a spring. Deformation (as shown by the dashed line in Figure 9 can absorb and consume excess energy, has achieved shock absorption effect, reducing the possibility of vibration transmission to the shell. As shown in Figure 1, this creation also includes application to electronics The shock absorbing module comprises a housing 82, a vibration element 81 and at least one annular airbag assembly 1 as described above. The housing 82 includes at least one fixing seat 821; the vibration element 81 is disposed on the housing The body 82 includes at least one fixing hole 811. The annular air bag assembly is disposed between the vibration element 81 and the housing 82, and one end thereof is fixed to the fixing base 821 of the housing 82, and the other end is connected with the vibration element 81. The fixing hole 811 is transmitted to the casing by the 12/shock vibration self-vibration 7〇81. The structural design of each of the annular airbag modules 1 and the rugged airbags has been described in the foregoing embodiments, and is not added here. The above-mentioned embodiments are merely examples for convenience of explanation, and the manufacturing claimed in the present invention is based on the scope of the patent application, and is not limited to the above embodiments. BRIEF DESCRIPTION OF THE DRAWINGS Fig. 1 is a schematic view showing the arrangement of the shock absorbing device of the present invention. Fig. 2 is a perspective structural view of the first embodiment of the shock absorbing device of the present invention. Fig. 3 is a first embodiment of the shock absorbing device of the present invention in use. Sectional view. Figure 4 is the original Fig. 5 is a perspective view showing the structure of the second embodiment of the shock absorbing device of the present invention. Fig. 6 is a cross-sectional view showing a third embodiment of the shock absorbing device of the present invention. Fig. 8 is a perspective view showing the structure of a fifth embodiment of the shock absorbing device of the present invention. Fig. 9 is a cross-sectional view showing a fifth embodiment of the shock absorbing device of the present invention. Explanation of component symbols] Shock absorbing device 1, la, lb, 1 c, Id M435807 Annular airbag module 10, l〇a, 10b, 10 c, lOd Airbag structure 1 11a, lib, 11 c, lid First support m , 111a, 111b, 111 c, llld groove mid second support portion 112, 112a, 112b, 112 c, 112d support surface 1121, 1121c, 1121d convex portion 1122b inner projection 113, 113a, 113 c, 113d Outer protrusions 114, 114a, 114c Penetration section 20 Electronic device 80 Vibration element 81 Fixing part 811 Housing 82 Mounting seat 821 Outer diameter Dl, D2, D3
間距B 14Spacing B 14