TW565502B - Composite structural with reinforcing ribs and method of making same - Google Patents

Composite structural with reinforcing ribs and method of making same Download PDF

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Publication number
TW565502B
TW565502B TW91118958A TW91118958A TW565502B TW 565502 B TW565502 B TW 565502B TW 91118958 A TW91118958 A TW 91118958A TW 91118958 A TW91118958 A TW 91118958A TW 565502 B TW565502 B TW 565502B
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Taiwan
Prior art keywords
fiber
reinforcing ribs
structural member
covered
composite
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TW91118958A
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Chinese (zh)
Inventor
Yu-De Chen
Ming-Ren Ding
Yung-Kuen Lin
Jeng-Jung Ke
Jin-Kuen Li
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Chung Shan Inst Of Science
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Priority to TW91118958A priority Critical patent/TW565502B/en
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Abstract

The objective of this invention is to provide a composite structural member with reinforcing ribs and method of making same. The method and the composite structural member made by the method is of a small sandwich structural member including appropriate number of layers of woven fiber tube and foamed materials coated by woven fabrics, hollow thermoplastic tubing, or honeycomb core, if desired. A structural member of large sandwich configuration is obtained by arranging the afore-mentioned structural members of small sandwich configuration in accordance with the cross-sections and appearance as desired in actual applications. The structural member is then coated with appropriate layers of woven fiber tube and woven fabrics, if needed, to form a fibril preform. A structural member of a composite material with ribs is then obtained by resin transfer molding.

Description

565502 _案號91118958 t年&amp;月日 修正_ 五、發明說明(1) 《發明概述》 本發明係關於一種具有加強肋之複材結構件及其製 程,特別是以樹脂轉注成形法,利用纖維編織管及視需要 加纖維布包覆蕊材形成小三明治結構,再以多個小三明治 結構結合成所需之結構件並包覆纖維編織管及視需要加纖 維布,並加以樹脂轉注成型之結構件及其製程。 《發明背景》 按,複材結構件所使用之樹脂轉注成型法,其所製作 之加強肋,大都另外成形,再配合整體之成形鋪設纖維 時,另外包覆並定位,或包覆後置入模穴中,單獨成形需 個別成形再結合成形,耗時又耗費模具成本及人力;且為 了結合結構,需多耗費纖維加以包覆,增加重量及成本之 諸多缺點;是故,針對上述樹脂轉注成型所產生之諸多缺 點與弊病,係有亟待改善之空間。 有鑑於此,本發明者即憑借著個人長期對於各種複材 結構之研究及融會貫通之構思,而發明一種具有加強肋之 複材結構件及其製程,其係以空心或實心之蕊材,利用編 織纖維管或纖維布加以包覆,形成一小型之三明治結構, 再配合結構件之整體套置編織纖維管結構或鋪設纖維布需 求,將小型三明治結構置於需求加強肋之位置,再置於模 具以樹脂轉注成形法一次成形完成;也可以利用多個小型 三明治結構,結合成一大型三明治結構,再與其他結構一 次鋪料結合並同時一次成形,其重量與結構強度均比二次565502 _Case No. 91118958 Year T &amp; Month and Day Amendment_ V. Description of the Invention (1) "Overview of the Invention" The present invention relates to a composite material structure with reinforcing ribs and its manufacturing process, especially the resin transfer molding method. The fiber braided tube and fiber cloth are used to cover the core material to form a small sandwich structure, and then multiple small sandwich structures are combined to form the required structural parts, and the fiber braided tube and fiber cloth are added as needed, and the resin is transferred into the molding. Structural parts and their processes. << Background of the Invention >> According to the resin injection molding method used for composite structural parts, most of the reinforcing ribs produced are formed separately. When the fiber is laid in conjunction with the overall forming, it is additionally covered and positioned, or placed after being covered. In the mold cavity, separate molding requires individual molding and combined molding, which is time-consuming and costly in terms of mold cost and manpower. In addition, in order to combine the structure, it requires more fiber to cover and increase the weight and cost. There are many shortcomings and disadvantages caused by molding, and there is room for urgent improvement. In view of this, the inventor has relied on his personal long-term research and integration of various composite materials, and invented a composite material structure with reinforcing ribs and its process, which is made of hollow or solid core materials. The woven fiber tube or fiber cloth is covered to form a small sandwich structure, and then the woven fiber tube structure or the fiber cloth needs are laid in accordance with the overall structure. The small sandwich structure is placed at the position where the reinforcing ribs are required, and then placed The mold is formed by resin injection molding at one time; it can also be combined into a large sandwich structure by using multiple small sandwich structures, and then combined with other structures at the same time and formed at the same time. Its weight and structural strength are both twice.

565502 五、發明說明條正 以上成形之具有加強 上整體製作技術實施容:、:;:;;減少成形之成本’加 確能符合產業利用性與實用性^本低,成效大,俾使整體 《發明目的》 Ί itb ’ 本發日月夕古α 結構件及a製程,其係—係在提供一種具有加強肋之複材 要加纖維布作為加強肋覆f材之編織纖維管及視需 起結合鋪料於模具 =與需加強肋之結構件- 型,透過此-製程所製=型製程製作-體成 強度,俾可藉以達到結構2,大幅提昇抗挫曲 構件之品質者。 件之…構強度需求,同時提昇結 本發明之次要目的係在提供一罝 及其製程,其結構件因為ς P,二有加強肋之複材結構件 之後續加工,可縮短工作“二二〉主膠成形,減少不必要 行製作加強肋再加以包覆纖‘與,4: 成形,不需先 纖維疊層及使用量’故可減輕結;仍效減少 件需求強度。 里 仍此確保結構 本發明之另一目的係在提供一種呈 及其製程’其中藉由纖維編織管;之=材結構件 織管具有伸縮性及連續性,緊=⑽材時’因為纖維編 易,裁切之廢料幾乎為零,得減小二^,使纖維之施工容 同時降低製作成本者。 ’夕並大巾s降低材料費用,565502 Fifth, the description of the invention has been strengthened to implement the overall production technology for the formation of the above articles:,:;: ;; reduce the cost of forming 'plus indeed can meet the industrial applicability and practicality ^ low cost, large effect, and make the whole "Objective of the Invention" Ί itb 'The ancient α structural parts and manufacturing process of the sun and the moon, which is to provide a woven fiber tube with reinforcing ribs to be added with fiber cloth as reinforcing ribs and f materials, as required The combination of material laying in the mold = and the structural parts that need to strengthen the ribs-through this-manufacturing process = molding process production-physical strength, can be used to achieve the structure 2 and significantly improve the quality of anti-buckling components. The secondary purpose of the present invention is to provide a stack and its manufacturing process. The structural parts of the composite part are reinforced because of the subsequent processing of the reinforced rib composite structural parts, which can shorten the work. 2> Forming of main rubber, reducing unnecessary production of reinforcing ribs and then covering the fibers 'and, 4: forming, without the need for fiber stacking and the amount of use', so the knot can be reduced; it still reduces the strength of the required parts. Ensuring structure Another object of the present invention is to provide a presentation and its process 'where fiber braided tube is used; where = the structure of the material is woven and the tube is stretchable and continuous, and tight = when the material is woven' because the fiber is easy to cut. The cut waste is almost zero, and it is necessary to reduce the two, so that the construction capacity of the fiber and the production cost are reduced at the same time.

第6頁 565502Page 6 565502

《發明之詳細說明》 為使審查委貝對本於明台b、仓 較佳實施例,ϋ配:月;;—步的瞭解’以下兹舉- 1i + &amp; &amp; 〇 Η 圖旒,將本發明之構成内容及 具所達成的功效詳細說明如后: 《具體實施例說明》 晴參閱第一圖中太發日日 &gt; 舍』γ 產品形狀設計,製作=之ϊ程流程圖’第-步驟是依 11 &amp;盔π π f t 材 再於蕊材10包覆第一纖維層 基礎結構件A,如第二圖所 枓結構件之其他纖維一起έ奘 ^ 後,詈於f目m t、、且裝成所需之結構件預成形狀態 後置於杈具,利用樹脂轉注成型f θ 固化成型’拆模後,即可得—出σ I私於至 '飢或问狐下 步了解,·^失閽筮一 m ^ σσ,為了使審查委員進一 解巧參閱第二圖至第十圖,Α 實施例來說明本製程及其所製=:2明舉例多種不同 三圖可見-具有加強肋= 構^ ^ 構件A,再以第二纖維層12包覆,盆中、J有兩個基 構件…或取出蕊材1。,使結構:二:可以留i 口由第四圖所示’ “多個基 成為空心;再 么士椹姓/士 成為一平板型結構件8,复士+|枯 g構件Α亦可因應設計,而有不同之“ 2 ^基礎 =是由多個基礎結構件A # =由J五圖 12包覆,以兩個結構料結人 】一再將第二纖維層 成為—樑柱型結構件。 二示織維層13包覆’ U Μ不,疋由多個基礎"Detailed Description of the Invention" In order for the review committee to understand the preferred embodiment of the book in Mingtai b, Cang, equipped with: month ;;-Step by step understanding 'The following are given-1i + &amp; &amp; 〇Η Figure Η, will The details of the composition of the present invention and the effects achieved are as follows: "Explanation of Specific Embodiments" Please refer to Taifa Day in the first figure &gt; shed. Γ Product shape design, production = process flow chart. -The step is to cover the first fiber layer basic structural component A with the 11 &amp; helmet π π ft material and the core material 10. After the other fibers of the structural component shown in the second figure are hand-rolled ^, 詈 詈 f head mt , And put the required structural parts in the pre-formed state, put them on the fork, and use resin transfer injection molding f θ curing molding 'after demolding, you can get-σ I privately to' hungry or ask the next step to understand , ^ 失 阍 筮 一 m ^ σσ, in order to make the reviewers better understand the second to tenth drawings, Α embodiment to explain the process and its making =: 2 examples for a variety of different three figures can be seen-with Reinforcement ribs = structure ^ ^ member A, and then covered with the second fiber layer 12, there are two base members in the basin, J ... or take out the core材 1。 Material 1. Make the structure: two: you can leave the mouth as shown in the fourth picture, "" Multiple bases become hollow; then Shishi surname / Shi becomes a flat-shaped structural member 8, Fu Shi + | dry g member A can also respond Design, but there are different "2 ^ foundation = is composed of multiple basic structural parts A # = is covered by J five Figure 12 and tied with two structural materials] repeatedly the second fiber layer into a beam-column structure . The second display woven layer 13 is coated with U’M No.

IHI 第7頁 565502 9111895« 五、發明說明(4) 結構件A並列之接, 件B結合,再以第 將第二纖維層1 2包覆,以三個蛀 ,.^ 第二纖維層1 3包覆,点在史 似…構 構件;再請由第七圖所示,是 成為另一種樑柱型結 後,再將第二纖維層12 個基礎結構件A並列之 應用於船殼結構;再 ^ ^型或V型結構件,可以 結構件,成為一中空型鈇盖曰,匕覆並組成一個環狀 構或大型油槽·爯a = &quot;以應用於機身、車體处 Α ^ 曰’再清由第九圖所示,县i夕ν 干般、、、口 A並列之後,再將第二纖 12 疋由夕個基礎結構件 構件,成為一中空型处、、曰 是,並組成一個環狀結 礎結構件A,成為構件,再於其中加入-個以上之基 示,是由三個不同形狀之基 A:;:由:十圖所 二纖維層12包覆,成為一翼二:A並列組合’再將第 旋翼及葉片結構。 、籌件’可以應用於機翼、 兹由以上說明得知 1、 結構強度提古“ίΐ明係可達到下列諸多功效: 管及視需要加纖維布包I β ^係在於先以纖維編織 他纖維組成後,經力^小三明治結構,與其 2、 降低成本明;:抗挫曲強度。 少使用量,仍維持設計強产 纖維童層減少,相對減 使用纖維編織管具有伸縮:及連;:低=巧;^若 :ί作=料幾乎為零,大幅降低材==樣Γ降 Λ (&gt; 曰 _修正IHI Page 7 565502 9111895 «V. Description of the invention (4) Structural parts A are connected side by side, parts B are combined, and then the second fiber layer 12 is covered with the first, and the three fiber layers are covered by the second fiber layer 1 3 cladding, the point is similar to the historical structural member; please show the seventh figure, it is another beam-column knot, and then the second fiber layer 12 basic structural parts A are applied side by side to the hull structure ^ ^ Or V-shaped structural parts, can be structural parts, become a hollow 鈇 cover, said dagger cover and form a ring structure or large oil tank · 爯 a = &quot; for application to the fuselage, car body Α ^ "Qi Qing" is shown in the ninth figure, after the county i and ν are parallel to each other, the second fiber 12 疋 is formed from a basic structural member to become a hollow type. , And form a ring-shaped foundation structure A, and become a component, and then add one or more bases, which are covered by three bases A of different shapes :; Become a wing two: A side-by-side combination 'then the first rotor and blade structure. "The chip" can be applied to the wing. It is learned from the above description. 1. The strength of the structure can be improved. The "Li Mingming system can achieve the following many effects: The tube and the fiber cloth package I β ^ are required to weave other fibers first." After the fiber composition, the warp force ^ small sandwich structure, and its cost reduction is clear ;: anti-buckling strength. Use less, still maintain the design of high-yield fiber child layer reduction, the relative reduction of the use of fiber braided tube has expansion and contraction: and even; : Low = qiao; ^ If: ί Zuo = material is almost zero, greatly reducing the material == 样 Γ 降 Λ (&gt;

U 第8頁 565502 案號 91118958 &gt; 曰 修正 五、發明說明(5) 3、 縮短工時 形,可增加結 需求,減少不 4、 形狀變化 計,包括蕊材 構件之設計變. 綜上所述 其結構件,係 程,其利用蕊 明治結構,再 需之大三明治 層,以樹脂轉 較佳之結構強 成本低,成效 者,且其構成 發明專利申請 為感禱。 需陳明者 用之技術原理 之功能作用仍 在本發明之範 :由於 構件整 必要之 :蕊材 之斷面 化,有 ,本發 提供一 材編織 依實際 結構件 注成形 度及品 大,俾 結構又 要件, ,以上 ,若依 未超出 圍内, 本發明係採一次注膠之樹脂 體之含浸效果’提而結構強 後續加工,縮短工作時程。 之形狀可以依實際結構件加 形狀,蕊材之整體造型,皆 不同之設定。 明具有流道系統之複合材料 種具有加強肋之複材結構件 纖維管及視需要加纖維布, 使用之結構件斷面及外型, 預成形物,最後,再包覆纖 成化之製程製作結構件,使 質,加上整體製作技術實施 使整體符合產業實用性及成 未曾見於諸書刊或公開使用 懇請 鈞局明鑑,早日准予 所述乃是本發明之具體實施 本發明之構想所作之改變, 說明書及圖式所涵蓋之精神 合予陳明。 轉注成 度設計之 以預先設 可因應結 之製程及 及其製 形成小三 排列成所 維結構 結構件具 容易,且 本效益 ,誠符合 專利,至 例及所運 其所產生 時,均應U Page 8 565502 Case No. 91118958 &gt; Revision V. Description of the Invention (5) 3. Shorten the working hours, which can increase the knot requirements, reduce the number of shapes 4, including the design changes of the core material components. The structural parts and processes are described. It utilizes the Ruimeiji structure and requires a large sandwich layer. It is a structure with a better resin and a lower cost. It is effective and its constitutional patent application is a prayer. The function of the technical principles that need to be used is still within the scope of the present invention: due to the need for structural integrity: the cross-section of the core material.俾 The structure also requires, if the above does not exceed the range, the invention adopts the impregnation effect of the resin body once injected to improve the structure for subsequent processing and shorten the working time. The shape can be added according to the actual structure, and the overall shape of the core material is different. The composite material structure with reinforced ribs and fiber tubes with reinforced ribs and fiber fabrics as needed, the cross-section and appearance of the structural components used, preforms, and finally the fiberization process The production of structural parts, quality, and the implementation of the overall production technology make the overall conformity with industrial practicality and achievements have not been seen in books or public use. I kindly ask Jun Bureau to make a clear reference, and the early approval is the implementation of the present invention. Changes, the spirit covered by the description and drawings are shared by Chen Ming. The design of the transfer rate is based on the pre-designed process and its formation. It is easy to arrange the three-dimensional structure into a dimensional structure. The structure is easy, and the benefit is in line with the patent. When it comes to the example and when it is generated, it should be

第9頁 565502 案號 91118958 圖式簡單說明 年厶月ί &gt; 曰 修正 《圖 第一 第二 第三 第四 第五 第六 第七 第八 第九 第十 面之 圖係 圖係 圖係 圖係 圖係 圖係 圖係 圖係 圖係 圖係 簡單說明 為本發明 為本發明 為本發明 為本發明 為本發明 為本發明 為本發明 為本發明 為本發明 為本發明 》 之製程流程圖。 之基礎結構之剖面圖。 第一實施例之剖面圖。 第二實施例之剖面圖。 第三實施例之剖面圖。 第四實施例之剖面圖。 第五實施例之剖面圖。 第六實施例之剖面圖。 第七實施例之剖面圖。 第八實施例之剖面圖。 《圖號說明 (Α)··· (10)···(12) · · 基礎結構件(Β) · 蕊材 (11)· 第二纖維層 (13) 結構件 第一纖維層 •第三纖維層Page 9 565502 Case No. 91118958 Schematic description of the year and month & &gt; Revision "The first, second, third, fourth, fifth, sixth, seventh, eighth, ninth, and tenth faces of the drawings" Schematic Schematic Schematic Schematic Schematic Schematic Schematic Schematic Schematic Schematic of the process of the invention The invention is the invention The invention is the invention The invention is the invention The invention is the invention The invention is the invention . Sectional view of the basic structure. A sectional view of the first embodiment. Sectional view of the second embodiment. Sectional view of the third embodiment. A sectional view of the fourth embodiment. Sectional view of the fifth embodiment. Sectional view of the sixth embodiment. Sectional view of the seventh embodiment. A sectional view of the eighth embodiment. "Illustration of drawing number (Α) ·· (10) ·· (12) · · Basic structural parts (B) · Core material (11) · Second fiber layer (13) Structural member first fiber layer • third Fibrous layer

第10頁Page 10

Claims (1)

565502 _案號91118958 年厶月ί丄日 修正_ 六、申請專利範圍 1 、一種具有加強肋之複材結構件,其係由一蕊材包覆纖 維編織管及視需要加纖維布,成為一基礎結構預型件,依 設計之結構組合預型件,以纖維結構結合並包覆,以樹脂 轉注成型製程成化之複材結構件,藉由蕊材置於複材結構 中而提昇結構件之強度並減少重量者。 2、 一種製造如專利範圍第1項所述之具有加強肋之複材 結構件之製程,其製程為:將一蕊材包覆纖維編織管及視 需要加纖維布,成為一基礎結構預型件,依設計之結構組 合預型件,以纖維結構結合並包覆,置入模具中並利用樹 脂轉注成型製程,將之成化,藉以提昇結構件之強度並減 少重量,降低成本及減少工時者。 3、 依據申請專利範圍第1項所述之具有加強肋之複材結 構件,其結構件含有一個以上之基礎結構件,包覆第二層 以上之纖維而經樹脂轉注成形者。 4、 依據申請專利範圍第1項所述之具有加強肋之複材結 構件,其中,包覆之蕊材可為空心或實心之發泡材或蜂巢 件、熱塑性或熱固性塑膠、金屬者。565502 _ Case No. 91118958 Amendment on the following day_ 6. Application for patent scope 1 A composite material structure with reinforcing ribs, which is covered by a core material with a fiber braided tube and fiber cloth if necessary, becoming a Basic structure preforms, according to the structure of the design, the preforms are combined and covered with fiber structure, and the composite structure is formed by the resin injection molding process. The strength and weight reduction. 2. A process for manufacturing a composite material structure with reinforcing ribs as described in item 1 of the patent scope. The process is as follows: a core material is coated with a fiber braided tube and a fiber cloth is added as necessary to become a basic structure preform. Prefabricated parts are assembled according to the designed structure, combined and covered with fiber structure, placed in a mold and converted into resin using a resin injection molding process to increase the strength of the structural part and reduce weight, cost and labor Time. 3. According to the composite material structure with reinforcing ribs described in item 1 of the scope of the patent application, the structural component contains more than one basic structural component, which is covered by the second layer or more of the fiber and then transferred to the resin. 4. According to the composite material with reinforcing ribs described in item 1 of the scope of the patent application, the core material can be hollow or solid foam material or honeycomb, thermoplastic or thermosetting plastic, metal. 第11頁Page 11
TW91118958A 2002-08-20 2002-08-20 Composite structural with reinforcing ribs and method of making same TW565502B (en)

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN117680672A (en) * 2024-02-02 2024-03-12 北京理工大学 Nickel-chromium-aluminum dynamic sealing material with sandwich structure and preparation method thereof

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN117680672A (en) * 2024-02-02 2024-03-12 北京理工大学 Nickel-chromium-aluminum dynamic sealing material with sandwich structure and preparation method thereof
CN117680672B (en) * 2024-02-02 2024-04-30 北京理工大学 Nickel-chromium-aluminum dynamic sealing material with sandwich structure and preparation method thereof

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