TWM601683U - Composite reinforcing structure - Google Patents
Composite reinforcing structure Download PDFInfo
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- TWM601683U TWM601683U TW108217280U TW108217280U TWM601683U TW M601683 U TWM601683 U TW M601683U TW 108217280 U TW108217280 U TW 108217280U TW 108217280 U TW108217280 U TW 108217280U TW M601683 U TWM601683 U TW M601683U
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Abstract
本創作關於一種複合材料補強結構,包括:一基體及一加強結構。該基體包含有一第一纖維層及一第二纖維層,該第一纖維層與該第二纖維層沿一堆疊方向相互堆疊結合,該第一纖維層背向該第二纖維層之一面定義為一外表面,該第二纖維層背向該第一纖維層之一面定義為一內表面;該加強結構包含有複數補強肋,該複數補強肋沿該堆疊方向地一體凸伸於該內表面,該複數補強肋相互交錯連接進而形成複數凹格部。This creation is about a composite reinforcement structure, including: a matrix and a reinforcement structure. The matrix includes a first fiber layer and a second fiber layer. The first fiber layer and the second fiber layer are stacked and combined with each other along a stacking direction. A side of the first fiber layer facing away from the second fiber layer is defined as An outer surface, a surface of the second fiber layer facing away from the first fiber layer is defined as an inner surface; the reinforcing structure includes a plurality of reinforcing ribs, and the plurality of reinforcing ribs integrally protrude from the inner surface along the stacking direction, The plurality of reinforcing ribs are alternately connected to each other to form a plurality of concave lattice parts.
Description
本創作係與複合材料之應用有關,特別是有關於一種複合材料補強結構。This creation is related to the application of composite materials, especially a composite reinforcement structure.
複合材料係至少由兩種材料經過複合技藝所製成,以期可兼容各種材料的優點,達到取長補短滿足不同使用需求,舉例但不顯於碳纖維複合材,其高硬度、輕量、耐高溫之優點,廣受各行業喜愛,尤其航空、車業或運動設備相關行業皆相繼推出相關產品。The composite material is made of at least two materials through composite technology, in order to be compatible with the advantages of various materials, to learn from each other to meet different needs of use, for example, but not obvious to carbon fiber composite materials, its advantages of high hardness, light weight, and high temperature resistance , Widely loved by various industries, especially aviation, automobile industry or sports equipment related industries have launched related products.
在上述所提及之碳纖維複合材中,其製品大都透過交錯編織的方式,或是以各種不同排列角度進行層層堆疊,來加強整體結構。然而,此種層層堆疊之強化方式將導致複合材料整體重量過重、層數過多而厚度過厚等缺點。Among the carbon fiber composite materials mentioned above, most of the products are interlaced weaving, or stacked layer by layer with various arrangement angles to strengthen the overall structure. However, this layer-by-layer strengthening method will result in the disadvantages of excessive weight, too many layers, and thick thickness of the composite material.
因此,有必要提供一種新穎且具有進步性之複合材料補強結構,以解決上述之問題。Therefore, it is necessary to provide a novel and progressive composite material reinforcement structure to solve the above-mentioned problems.
本創作之主要目的在於提供一種複合材料補強結構,可以對至少局部位置進行結構強化,以減少整體材料之消耗,進而達到兼顧輕量、堅固之優點。The main purpose of this creation is to provide a composite material reinforcement structure, which can strengthen the structure at least partially in order to reduce the consumption of the overall material, thereby achieving the advantages of light weight and sturdiness.
為達成上述目的,本創作提供一種複合材料補強結構,包括:一基體及一加強結構。該基體包含有一第一纖維層及一第二纖維層,該第一纖維層與該第二纖維層沿一堆疊方向相互堆疊結合,該第一纖維層背向該第二纖維層之一面定義為一外表面,該第二纖維層背向該第一纖維層之一面定義為一內表面;該加強結構包含有複數補強肋,該複數補強肋沿該堆疊方向地一體凸伸於該內表面,該複數補強肋相互交錯連接進而形成複數凹格部。In order to achieve the above-mentioned purpose, this creation provides a composite reinforcement structure, including: a matrix and a reinforcement structure. The matrix includes a first fiber layer and a second fiber layer. The first fiber layer and the second fiber layer are stacked and combined with each other along a stacking direction. A side of the first fiber layer facing away from the second fiber layer is defined as An outer surface, a surface of the second fiber layer facing away from the first fiber layer is defined as an inner surface; the reinforcing structure includes a plurality of reinforcing ribs, and the plurality of reinforcing ribs integrally protrude from the inner surface along the stacking direction, The plurality of reinforcing ribs are alternately connected to each other to form a plurality of concave lattice parts.
以下僅以實施例說明本創作可能之實施態樣,然並非用以限制本創作所欲保護之範疇,合先敘明。The following examples are only used to illustrate the possible implementation of this creation, but it is not intended to limit the scope of the creation to be protected, and it is first stated.
請參考圖1至圖4,其顯示本創作之一較佳實施例,本創作之複合材料補強結構包括一基體1及一加強結構2。Please refer to FIGS. 1 to 4, which show a preferred embodiment of the present invention. The composite reinforcement structure of the present invention includes a
該基體1包含有一第一纖維層11及一第二纖維層12,該第一纖維層11與該第二纖維層12沿一堆疊方向4相互堆疊結合,該第一纖維層11背向該第二纖維層12之一面定義為一外表面13,該第二纖維層12背向該第一纖維層11之一面定義為一內表面14。該基體1可用於包覆於球桿、電腦外殼、手機殼、車體等各種物體之外部,以強化物體耐衝擊之能力,應用層面極為廣泛。而可以理解的是,該基體1可以是板狀、弧形、波浪狀等各式各樣造型。The
該加強結構2包含有複數補強肋21,該複數補強肋21沿該堆疊方向4地一體凸伸於該內表面14,即該加強結構2屬於該第二纖維層12之部分,該複數補強肋21相互交錯連接進而形成複數凹格部22,以進一步補強該基體1耐衝擊能力,給予包覆物更加完善之保護。詳細地說,該加強結構2僅設於該內表面14之部分,可以針對包覆物之部分再進行局部強化,相較於整體強化,局部強化可以有效減少整體材料之使用量,降低複合材料的整體重量,兼顧結構強化及維持整體輕量之目的。The
各該凹格部22可提供該基體1受到外力衝擊時,緩衝形變之裕度空間,各該凹格部22之形狀為多邊形,以期能以較少之材料即可獲得高承載力之結構;其中,該複數凹格部22包含有至少一第一格部221,該第一格部221之輪廓形狀為六邊形,其中,以正六邊形為優選。Each of the
於本實施例中,該複數凹格部22包含有複數該第一格部221以形成類蜂窩式結構,以建構出能承受較大受力之結構;並且,該複數凹格部22另包含有複數第二格部222與複數第三格部223,該第二格部222之輪廓形狀為四邊形,該第三格部223之輪廓形狀為五邊形,該第二格部222與該第三格部223以對應所欲包覆物之輪廓變化而分布於不同位置,以承受分散不同程度之作用力。In this embodiment, the plurality of
較佳地,該複數凹格部22之輪廓形狀大小不盡相同,以期可以透過疏密分布來對包覆物進行客製化之補強配置,複數該凹格部22進行較密集之配置,能有效大幅提升保護部位之結構剛性,使其能有極佳抵抗外力之能力。此外,較大的該凹格部22處,該基體1相對較容易彎曲,而可對應包覆物輪廓彎曲變化較大之部分,讓該基體1能夠緊密地地貼附於包覆物。Preferably, the contour shapes and sizes of the plurality of
該加強結構2另包含有一邊界肋23,該邊界肋23界定出一補強空間24,該複數補強肋21於該補強空間24內相互連接,進行將該補強空間24劃分出該複數凹格部22;其中,部分該複數補強肋21連接於該邊界肋23,以有更連續完整之結構。The
更具體來說,該複數補強肋21包含有一第一補強部211及一第二補強部212,沿該堆疊方向4觀之,該第二補強部212之寬度大於該第一補強部211之寬度,該邊界肋23之寬度介於該第一補強部211之寬度與該第二補強部212之寬度之間,透過寬度之變化可以控制該補強肋21之補強強度,以進行更細膩之補強程度調整,可以理解的是,該第一補強部211、該第二補強部212及該邊界肋23之寬度並不以上述為限,上述僅為實施例之一種,實際應用乃以使用者之需求為主進行調整。而要再次強調的是,強化程度補強之調控可進一步配合該複數凹格部22之大小變化形成疏密分布來調整控制,越密集處強化效果越佳、結構剛性越高。More specifically, the plurality of reinforcing
於該堆疊方向4之方向上,該第一纖維層11之厚度大於該第二纖維層12之厚度,從較微觀之角度觀之,於本實施例中,該第一纖維層11係為連續纖維層,該第二纖維層12係為不連續纖維層,即該強化結構2為不連續纖維所構成。明確地說,該第一纖維層11包含有複數長纖維111,該複數長纖維111沿同向排列,或進一步以不同角度層疊來作為連續結構之強度基準,並配合該複數補強肋21來更進一步強化結構強度,而該第二纖維層12包含有複數短纖維121,相鄰之複數該短纖維121組構成複數短纖維群122,該複數短纖維群122沿任意方向排列並於該內表面14形成一花紋結構3,如此一來,使用者可透過目視觀看之方式即可辨認出該內表面14,且該花紋結構3有利增加與包覆物之接觸面積,使得該基體1能緊密地貼覆於包覆物。重要的是,沿任意方向的該複數短纖維群122有助於強化該第二纖維層12(包含該強化結構)承受來自不同方向之受力;同時,隨機排列配置的該複數短纖維群122能夠產生較高之密度,以補強結構硬度。另外,該複數短纖維群122可選自餘料,以充分利用原料。In the direction of the
當然,並不侷限於此,依據需求之不同,亦可如圖5及圖6之另一實施例所示,第一纖維層11A係為連續纖維層,第二纖維層12A為連續纖維層,加強結構2A亦為連續纖維所構成,以便於快速生產。Of course, it is not limited to this. According to different requirements, as shown in another embodiment of FIG. 5 and FIG. 6, the
綜上,本創作之複合材料補強結構可以針對局部範圍進行強化,並可隨欲包覆物品之輪廓,客製化編列強化肋所建構出凹格部的疏密度、大小範圍,進而可再對欲強化部分做更全面、更細膩的補強;此外,第二纖維層採用不連續纖維可以於各種方向上進行受力補強、提升密度,而可有較堅韌的結構承受、分散來自外界之衝擊力。In summary, the composite reinforcement structure of this creation can be strengthened for a local area, and the outline of the object can be covered at will, and the density and size range of the concave grid constructed by the reinforcement ribs can be customized. The part to be strengthened can be strengthened more comprehensively and delicately; in addition, the discontinuous fiber used in the second fiber layer can strengthen the force and increase the density in various directions, and it can have a tougher structure to withstand and disperse the impact from the outside. .
1:基體
11,11A:第一纖維層
111:長纖維
12,12A:第二纖維層
121:短纖維
122:短纖維群
13:外表面
14:內表面
2,2A:加強結構
21:補強肋
211:第一補強部
212:第二補強部
22:凹格部
221:第一格部
222:第二格部
223:第三格部
23:邊界肋
24:補強空間
3:花紋結構
4:堆疊方向1:
圖1為本創作一實施例之立體圖。 圖2為圖1之正視圖。 圖3為圖2之剖面圖。 圖4為圖3之局部放大圖。 圖5為本創作另一實施例之正視圖。 圖6為圖5之局部剖面放大圖。 Figure 1 is a perspective view of an embodiment of the creation. Figure 2 is a front view of Figure 1; Figure 3 is a cross-sectional view of Figure 2. Figure 4 is a partial enlarged view of Figure 3. Figure 5 is a front view of another embodiment of the creation. Figure 6 is an enlarged partial cross-sectional view of Figure 5;
1:基體 1: matrix
11:第一纖維層 11: The first fiber layer
12:第二纖維層 12: The second fiber layer
2:加強結構 2: Strengthen the structure
21:補強肋 21: reinforcement ribs
22:凹格部 22: concave grid
23:邊界肋 23: boundary rib
3:花紋結構 3: pattern structure
4:堆疊方向 4: Stacking direction
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TW108217280U TWM601683U (en) | 2019-12-26 | 2019-12-26 | Composite reinforcing structure |
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TW108217280U TWM601683U (en) | 2019-12-26 | 2019-12-26 | Composite reinforcing structure |
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TWM601683U true TWM601683U (en) | 2020-09-21 |
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