JP2003328498A - Strengthening member, trussed structure and manufacturing method therefor - Google Patents
Strengthening member, trussed structure and manufacturing method thereforInfo
- Publication number
- JP2003328498A JP2003328498A JP2002137521A JP2002137521A JP2003328498A JP 2003328498 A JP2003328498 A JP 2003328498A JP 2002137521 A JP2002137521 A JP 2002137521A JP 2002137521 A JP2002137521 A JP 2002137521A JP 2003328498 A JP2003328498 A JP 2003328498A
- Authority
- JP
- Japan
- Prior art keywords
- fiber
- manufacturing
- strength member
- resin
- strength
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 74
- 238000005728 strengthening Methods 0.000 title abstract 5
- 229920005989 resin Polymers 0.000 claims abstract description 58
- 239000011347 resin Substances 0.000 claims abstract description 58
- 238000000034 method Methods 0.000 claims abstract description 48
- 229920002430 Fibre-reinforced plastic Polymers 0.000 claims abstract description 46
- 239000011151 fibre-reinforced plastic Substances 0.000 claims abstract description 46
- 239000000463 material Substances 0.000 claims abstract description 41
- 238000005470 impregnation Methods 0.000 claims abstract description 14
- 239000000835 fiber Substances 0.000 claims description 37
- 238000002347 injection Methods 0.000 claims description 10
- 239000007924 injection Substances 0.000 claims description 10
- 230000008878 coupling Effects 0.000 claims description 9
- 238000010168 coupling process Methods 0.000 claims description 9
- 238000005859 coupling reaction Methods 0.000 claims description 9
- 238000005452 bending Methods 0.000 claims description 7
- 238000007789 sealing Methods 0.000 claims description 3
- 229920005992 thermoplastic resin Polymers 0.000 claims description 3
- 238000005304 joining Methods 0.000 claims 1
- 229910052751 metal Inorganic materials 0.000 description 19
- 239000002184 metal Substances 0.000 description 19
- 239000013585 weight reducing agent Substances 0.000 description 9
- 239000012783 reinforcing fiber Substances 0.000 description 8
- 239000003733 fiber-reinforced composite Substances 0.000 description 5
- 229910052782 aluminium Inorganic materials 0.000 description 4
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 4
- 230000003014 reinforcing effect Effects 0.000 description 4
- 229910001385 heavy metal Inorganic materials 0.000 description 3
- 238000009954 braiding Methods 0.000 description 2
- 239000004566 building material Substances 0.000 description 2
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 238000009730 filament winding Methods 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 238000003860 storage Methods 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000012141 concentrate Substances 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 239000002828 fuel tank Substances 0.000 description 1
- JHJNPOSPVGRIAN-SFHVURJKSA-N n-[3-[(1s)-1-[[6-(3,4-dimethoxyphenyl)pyrazin-2-yl]amino]ethyl]phenyl]-5-methylpyridine-3-carboxamide Chemical compound C1=C(OC)C(OC)=CC=C1C1=CN=CC(N[C@@H](C)C=2C=C(NC(=O)C=3C=C(C)C=NC=3)C=CC=2)=N1 JHJNPOSPVGRIAN-SFHVURJKSA-N 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
Landscapes
- Rod-Shaped Construction Members (AREA)
- Moulding By Coating Moulds (AREA)
Abstract
Description
【0001】[0001]
【発明の属する技術分野】本発明は、部材間に配され、
これら部材間の荷重伝達を行う強度部材と、この強度部
材の製造方法と、この強度部材を用いたトラス構造とに
関する。特には、軽くて低コストな強度部材、トラス構
造、及び強度部材の製造方法に関する。TECHNICAL FIELD The present invention is arranged between members,
The present invention relates to a strength member that transmits a load between these members, a method of manufacturing the strength member, and a truss structure using the strength member. In particular, it relates to a light and low-cost strength member, truss structure, and method for manufacturing a strength member.
【0002】[0002]
【従来の技術】例えば、宇宙ロケットにおける燃料タン
ク支持構造などの航空宇宙トラス構造や、一般建材など
の建築構造において、軽量でありながらも比較的高い強
度を発揮できるトラス構造が広く用いられている。この
種のトラス構造の構成要素に用いられる強度部材として
は、例えば一般建材では、金属製パイプの両端に端部金
具を溶接固定もしくはボルト固定したものが一般的であ
る。また、航空宇宙トラス構造では、軽量化が求められ
るため、金属製パイプの代わりにCFRP(繊維強化プ
ラスチック)製のチューブを採用し、その両端に金属製
(例えばアルミ材)の端部金具をファスナ結合したもの
が採用されている。2. Description of the Related Art For example, in an aerospace truss structure such as a fuel tank support structure for a space rocket or a construction structure such as general building materials, a truss structure which is lightweight but can exhibit relatively high strength is widely used. . As a strength member used for a component of this type of truss structure, for example, in a general building material, a metal pipe is generally welded or bolted with end fittings at both ends. In aerospace truss structures, weight reduction is required, so instead of metal pipes, CFRP (fiber reinforced plastic) tubes are used, and metal (for example, aluminum) end fittings are attached to both ends of the fasteners. The combined one is adopted.
【0003】このファスナ結合は、図示を省略するが、
両端が開口した円筒形状のCFRPチューブに対し、前
記各開口部分を他のCFRPリングで補強した後、この
補強部分に前記端部金具を嵌合させ、これら端部金具及
び補強部分の壁面を同時に貫く複数本のファスナによ
り、締結させた構造をなしている。そして、このように
して製作された強度部材の端部をなす前記端部金具に
は、予め雌ねじが切られているため、ここにロッドエン
ド(アイボルト)の雄ねじを螺着させることで、他の部
品間を、これらロッドエンドを介して接続可能な強度部
材となっている。Although not shown, this fastener connection is not shown.
For a cylindrical CFRP tube with both ends open, after reinforcing each of the openings with another CFRP ring, the end fittings are fitted to the reinforcing parts, and the end fittings and the wall surfaces of the reinforcing parts are simultaneously formed. It has a structure in which it is fastened with multiple fasteners that penetrate it. Since the end fittings forming the end of the strength member manufactured in this way are pre-threaded, the male thread of the rod end (eyebolt) is screwed onto the end fitting, thereby It is a strength member that can connect the parts via these rod ends.
【0004】[0004]
【発明が解決しようとする課題】ところで、この従来の
強度部材は、以下に説明する問題を有していた。すなわ
ち、従来の強度部材は、その端部を金属部品(端部金
具)で構成しているため、この金属部品を製作するため
の製造コストと、CFRPチューブに取り付けるための
取り付け加工費がかかるため、コストが高いという問題
を有していた。また、端部を金属部品(端部金具)で構
成することは、重量増加も招くことになるので、強度部
材そのものの軽量化の妨げになるという別の問題も有し
ている。特に、航空宇宙分野では、極力、部品を軽量化
させることが切望されている。By the way, this conventional strength member has the following problems. That is, since the end of the conventional strength member is composed of a metal part (end fitting), the manufacturing cost for manufacturing this metal part and the mounting processing cost for mounting the CFRP tube are required. However, it had a problem of high cost. In addition, forming the end portion with a metal component (end portion metal fitting) also causes an increase in weight, and thus has another problem that it hinders weight reduction of the strength member itself. In particular, in the aerospace field, it is strongly desired to reduce the weight of parts as much as possible.
【0005】本発明は、上記事情に鑑みてなされたもの
であり、低コスト化と軽量化を達成できる強度部材、ト
ラス構造と、その強度部材の製造方法の提供を目的とす
る。The present invention has been made in view of the above circumstances, and an object of the present invention is to provide a strength member, a truss structure, and a method of manufacturing the strength member, which can achieve cost reduction and weight reduction.
【0006】[0006]
【課題を解決するための手段】本発明は、上記課題を解
決するために以下の手段を採用した。すなわち、請求項
1に記載の強度部材は、部材間に配され、これら部材間
の荷重伝達を行う強度部材において、前記部材に取り付
けられる結合体と、該結合体が固定される端部に向かっ
て収束する繊維強化プラスチック中空構造体とを備え、
該繊維強化プラスチック中空構造体の前記端部に、前記
結合体が螺着する螺合部が設けられていることを特徴と
する。上記請求項1に記載の強度部材によれば、その端
部は、従来の金属部品に代わり、胴体と同じ繊維強化複
合材料で構成されている。しかも、この端部には螺合部
が設けられているため、従来通り、ロッドエンド等の結
合体を容易に取り付けることができるものとなってい
る。したがって、端部をなす金属部品を必要としないこ
とから、その金属部品の製造コストと取り付けコストと
を削減することができるようになる。The present invention adopts the following means in order to solve the above problems. That is, the strength member according to claim 1 is disposed between the members, and in the strength member that transmits the load between the members, faces the joint body attached to the member and the end portion to which the joint body is fixed. And a fiber-reinforced plastic hollow structure that converges,
The fiber-reinforced plastic hollow structure is characterized in that a threaded portion to which the combined body is screwed is provided at the end portion. According to the strength member of the first aspect, the end portion is made of the same fiber-reinforced composite material as the body, instead of the conventional metal part. Moreover, since the end portion is provided with the screwed portion, the coupling body such as the rod end can be easily attached as in the conventional case. Therefore, since the metal component forming the end portion is not required, the manufacturing cost and the mounting cost of the metal component can be reduced.
【0007】請求項2に記載の強度部材は、請求項1に
記載の強度部材において、前記繊維強化プラスチック中
空構造体の内部に、前記螺合部の少なくとも一部をなす
螺着体が一体に備えられていることを特徴とする。上記
請求項2に記載の強度部材によれば、螺着体がない場合
に比較して、螺合部の全長を長く取ることができるた
め、結合体と繊維構造体との間の螺着長さを十分に長く
確保することができる。According to a second aspect of the present invention, there is provided a strength member according to the first aspect, in which the threaded body forming at least a part of the threaded portion is integrally formed inside the fiber reinforced plastic hollow structure. It is characterized by being provided. According to the strength member of the second aspect, the total length of the screwed portion can be made longer than in the case where there is no screwed body, so the screwed length between the combined body and the fiber structure is large. The length can be secured long enough.
【0008】請求項3に記載の強度部材は、請求項1ま
たは請求項2に記載の強度部材において、前記繊維強化
プラスチック中空構造体の外部に、前記端部に螺着され
た前記結合体に対して面接触し、これら繊維強化プラス
チック中空構造体及び結合体間に作用する引張荷重や圧
縮荷重あるいは曲げ荷重等を受ける当接面を備えた当接
部材が固定されていることを特徴とする。上記請求項3
に記載の強度部材によれば、この構成によれば、繊維強
化プラスチック中空構造体及び結合体間に比較的大きな
引張荷重や圧縮荷重あるいは曲げ荷重等が作用しても、
これらの全てを螺合部で受けるのではなく、当接面によ
る面接触で受け、さらには、この当接部材を介して繊維
強化プラスチック中空構造体に逃がすことができるた
め、荷重が集中しないように分散させることができる。According to a third aspect of the present invention, there is provided the strength member according to the first or second aspect, in which the fiber-reinforced plastic hollow structure is externally attached to the joint body screwed to the end portion. It is characterized in that an abutting member having an abutting surface that is in surface contact with the fiber-reinforced plastic hollow structure and the joint and receives a tensile load, a compressive load, a bending load, or the like acting between them is fixed. . Claim 3
According to this structure, according to the strength member described in (1), even if a relatively large tensile load, compression load, bending load, or the like acts between the fiber-reinforced plastic hollow structure and the bonded body,
All of these are not received by the screwed part but by surface contact by the contact surface, and further, it can be released to the fiber reinforced plastic hollow structure through this contact member, so that the load is not concentrated. Can be dispersed in.
【0009】請求項4に記載のトラス構造は、請求項1
から請求項3のいずれか1項に記載の強度部材が用いら
れていることを特徴とする。上記請求項4に記載のトラ
ス構造によれば、その強度部材が、低コスト化と軽量化
を同時に達成できるため、低コストで軽量なトラス構造
を構成することができる。The truss structure according to claim 4 is the structure according to claim 1.
The strength member according to any one of claims 1 to 3 is used. According to the truss structure of the fourth aspect, since the strength member can simultaneously achieve cost reduction and weight reduction, it is possible to configure a low cost and lightweight truss structure.
【0010】請求項5に記載の強度部材の製造方法は、
結合部材を介して部材間に配され、これら部材間の荷重
伝達を行う強度部材の製造方法において、型材の周囲
に、前記結合部材が取り付けられる端部にかけて収束す
るように繊維組織を形成して繊維構造体を製造する母材
製造工程と、該母材製造工程後の前記繊維構造体の繊維
組織に、溶融した樹脂を含浸させて固める樹脂含浸工程
と、該樹脂含浸工程後の前記端部に、前記結合部材を取
り付ける取り付け工程とを有することを特徴とする。上
記請求項5に記載の強度部材の製造方法によれば、製造
された強度部材の端部が、従来の金属部品に代わり、胴
体と同じ繊維強化複合材料で構成できる。したがって、
端部をなす金属部品を必要としないことから、その金属
部品の製造コストと取り付けコストとを削減することが
できるようになる。A method for manufacturing a strength member according to claim 5 is
In a method for manufacturing a strength member that is arranged between members via a connecting member and transmits load between these members, a fiber structure is formed around a mold material so as to converge toward an end to which the connecting member is attached. A base material manufacturing step for manufacturing a fiber structure, a resin impregnation step of impregnating a molten resin into the fiber structure of the fiber structure after the base material manufacturing step to solidify, and the end portion after the resin impregnation step And a mounting step for mounting the coupling member. According to the method for manufacturing a strength member described in claim 5, the end portion of the manufactured strength member can be formed of the same fiber-reinforced composite material as the body instead of the conventional metal part. Therefore,
Since the metal component forming the end portion is not required, the manufacturing cost and the mounting cost of the metal component can be reduced.
【0011】請求項6に記載の強度部材の製造方法は、
請求項5に記載の強度部材の製造方法において、前記樹
脂含浸工程で、前記繊維構造体を収容する凹部が形成さ
れた金型内に、前記繊維構造体を密閉した後、前記凹部
内に前記樹脂を注入することで前記繊維組織に含浸させ
ることを特徴とする。上記請求項6に記載の強度部材の
製造方法によれば、金型の凹部内を満たす樹脂が、隙間
なく繊維組織に含浸されていく。The method for manufacturing a strength member according to claim 6 is
The method for manufacturing a strength member according to claim 5, wherein, in the resin impregnating step, the fiber structure is hermetically sealed in a mold in which a recess for accommodating the fiber structure is formed, It is characterized in that the fiber structure is impregnated by injecting a resin. According to the method for manufacturing a strength member described in claim 6, the resin filling the concave portion of the mold is impregnated into the fibrous structure without any gap.
【0012】請求項7に記載の強度部材の製造方法は、
請求項6に記載の強度部材の製造方法において、前記型
材として熱可塑性樹脂等の伸縮可能な材料からなる中空
部材を用い、前記樹脂含浸工程では、前記樹脂注入中の
前記型材に内圧を加えることで、前記繊維組織の形状を
保持することを特徴とする。上記請求項7に記載の強度
部材の製造方法によれば、製造後に強度部材の一部とな
る型材に、中空部材を採用することにより、強度部材を
軽量化できるようになる。しかも、この型材は、樹脂注
入中は内圧を受けた状態に保たれるため、注入樹脂によ
る外圧(圧縮)を受けても、その形状を適切に維持する
ことができ、繊維組織に形状を付与するための型として
の機能も十分に発揮することができる。A method for manufacturing a strength member according to claim 7 is
The method for manufacturing a strength member according to claim 6, wherein a hollow member made of a stretchable material such as a thermoplastic resin is used as the mold member, and in the resin impregnating step, an internal pressure is applied to the mold member during the resin injection. Thus, the shape of the fiber structure is maintained. According to the method for manufacturing a strength member according to the seventh aspect, the strength member can be reduced in weight by employing the hollow member as the mold material that becomes a part of the strength member after manufacturing. Moreover, since this mold material is kept under internal pressure during resin injection, its shape can be properly maintained even when external pressure (compression) is applied by the injected resin, and the fiber structure is given a shape. The function as a mold for working can be fully exerted.
【0013】請求項8に記載の強度部材の製造方法は、
請求項7に記載の強度部材の製造方法において、前記型
材の内部加圧を、前記結合部材が取り付けられる貫通孔
より行うことを特徴とする。上記請求項8に記載の強度
部材の製造方法によれば、内部加圧を行うためだけの専
用の孔を強度部材壁面に形成する必要がないThe method for manufacturing a strength member according to claim 8 is
The method for manufacturing a strength member according to claim 7, wherein the internal pressure of the mold member is applied through a through hole to which the coupling member is attached. According to the method of manufacturing a strength member described in claim 8, it is not necessary to form a dedicated hole in the strength member wall surface only for performing internal pressurization.
【0014】請求項9に記載の強度部材の製造方法は、
請求項5から請求項8のいずれか1項に記載の強度部材
の製造方法において、前記母材製造工程では、前記型材
の端部に、前記結合部材と結合する被結合部材を取り付
けて一体とした上で、これら型材及び被結合部材の周囲
に前記繊維組織を形成することを特徴とする。上記請求
項9に記載の強度部材の製造方法によれば、繊維組織形
成後の強度部材内に、被結合部材を一体に固定すること
ができる。これにより、被結合部材がない場合に比較し
て、結合体の取り付け強度をより高くすることができ
る。The method for manufacturing a strength member according to claim 9 is
The method for manufacturing a strength member according to any one of claims 5 to 8, wherein in the base material manufacturing step, a coupled member that is coupled to the coupling member is attached to an end portion of the mold material to be integrated. In addition, the fiber structure is formed around these mold members and members to be bonded. According to the method for manufacturing a strength member described in claim 9, the member to be coupled can be integrally fixed in the strength member after the formation of the fibrous structure. As a result, the attachment strength of the combined body can be increased as compared with the case where there is no member to be connected.
【0015】[0015]
【発明の実施の形態】本発明の強度部材は、例えば部材
間に配され、これら部材間の荷重伝達を行うものであ
り、その一実施形態を、図面を参照しながら以下に説明
するが、本発明がこれのみに限定解釈されるものでない
ことは勿論である。なお、図1は、本実施形態の強度部
材を示す図であって、その軸線を含む断面で見た場合の
断面図である。また、図2は、同強度部材の端部を示す
部分拡大図である。BEST MODE FOR CARRYING OUT THE INVENTION The strength member of the present invention is arranged, for example, between members to perform load transmission between these members, and one embodiment thereof will be described below with reference to the drawings. Of course, the present invention is not limited to this. Note that FIG. 1 is a view showing the strength member of the present embodiment, and is a cross-sectional view when seen in a cross-section including the axis thereof. Further, FIG. 2 is a partially enlarged view showing an end portion of the same strength member.
【0016】図1に示すように、本実施形態の強度部材
は、一対(2個)のアイボルトであるロッドエンド1
(結合体)と、これらロッドエンド1が固定される固定
部分に向かって収束する両端2aを有するチューブ状の
繊維強化プラスチック中空構造体2とを備えて概略構成
されている。同図では、説明のために、各ロッドエンド
1を繊維強化プラスチック中空構造体2から取り外した
状態を示しているが、実際には、図2に示すように、繊
維強化プラスチック中空構造体2に対して各ロッドエン
ド1を取り付けた状態で、1部品として用いられる。As shown in FIG. 1, the strength member of this embodiment is a rod end 1 which is a pair (two) of eyebolts.
It is roughly configured by including a (combined body) and a tubular fiber-reinforced plastic hollow structure 2 having both ends 2a that converge toward a fixed portion to which these rod ends 1 are fixed. In the figure, for the sake of explanation, the state where each rod end 1 is removed from the fiber reinforced plastic hollow structure 2 is shown, but in reality, as shown in FIG. In contrast, each rod end 1 is attached and used as one component.
【0017】各ロッドエンド1は、例えばアルミなどの
金属部品であり、図1に示すように、前記部材や他の強
度部材のロッドエンド(図示せず)に接続される接続部
1aと、前記端部2aに螺着される雄ねじ部1bとを備
えている。なお、各ロッドエンド1としては、金属に限
らず、樹脂材をその材質として採用しても良いEach rod end 1 is, for example, a metal component such as aluminum, and as shown in FIG. 1, a connecting portion 1a connected to a rod end (not shown) of the member or another strength member, and A male screw portion 1b screwed to the end portion 2a is provided. The rod end 1 is not limited to metal, and a resin material may be used as the material.
【0018】繊維強化プラスチック中空構造体2は、主
にCFRP(繊維強化プラスチック)製のチューブから
なり、図2に示すように、両端2aで絞られた長尺の中
空円筒形状をなしている。この繊維強化プラスチック中
空構造体2は、両端が絞られた、熱可塑性樹脂等の伸縮
可能な材料からなる中空円筒形状のライナー4(型材)
の周囲に、強化繊維3をブレイディングやフィラメント
ワインディングなどの手法を用いて隙間なく巻き付けた
組み物を作成し、強化繊維3中に溶融した樹脂を含浸さ
せ、さらには硬化させたものである。樹脂の含浸/硬化
については、後述する。The fiber reinforced plastic hollow structure 2 is mainly composed of a CFRP (fiber reinforced plastic) tube, and has a long hollow cylindrical shape squeezed at both ends 2a as shown in FIG. This fiber-reinforced plastic hollow structure 2 is a hollow cylindrical liner 4 (mold material) whose both ends are squeezed and which is made of a stretchable material such as a thermoplastic resin.
A structure in which the reinforcing fibers 3 are tightly wound around the periphery of the resin using a technique such as braiding or filament winding is created, and the reinforcing fibers 3 are impregnated with the molten resin and further cured. The resin impregnation / curing will be described later.
【0019】図2に示すように、繊維強化プラスチック
中空構造体2の両端部2aには、前記各ロッドエンド1
の雄ねじ部1bが螺着する雌ねじ部2b(螺合部)が形
成されている。これら雌ねじ部2bは、繊維強化プラス
チック中空構造体2の内部に一体に固定された螺着体5
(螺着体、被結合部材)と、繊維強化プラスチック中空
構造体2の外部に一体に固定された当接部材6と、これ
ら螺着体5及び当接部材6間に挟み込まれる両端部2a
の壁部とを同時に貫く雌ねじ孔である。As shown in FIG. 2, each of the rod ends 1 is attached to both ends 2a of the fiber reinforced plastic hollow structure 2.
The female screw portion 2b (screw portion) to which the male screw portion 1b is screwed is formed. These internal threaded portions 2b are screwed members 5 integrally fixed to the inside of the fiber-reinforced plastic hollow structure 2.
(Screw body, member to be coupled), contact member 6 integrally fixed to the outside of the fiber-reinforced plastic hollow structure 2, and both end portions 2a sandwiched between the screw body 5 and the contact member 6.
Is a female screw hole that simultaneously penetrates the wall of the.
【0020】各螺着体5は、例えばアルミ材などの金属
部品からなり、中空の球体を半分に割った概略形状を有
している。これら螺着体5は、その内側に形成された球
面において、繊維強化プラスチック中空構造体2の外部
両端の外壁面に密着固定されている。なお、各螺着体5
としては、金属に限らず、樹脂材をその材質として採用
しても良い。各当接部材6は、例えばアルミ材などの金
属部品からなり、繊維強化プラスチック中空構造体2の
各端部2aに対して密着する内壁面を有している。そし
て、これら当接部材6は、その内壁面において、各端部
2aの外壁面に接着固定されている。また、これら当接
部材6の外壁面には、螺着された前記ロッドエンド1の
ナット部1cに対して面接触し、これらロッドエンド1
及び繊維強化プラスチック中空構造体2間に作用する引
張荷重や圧縮荷重あるいは曲げ荷重等を受ける、当接面
6aがそれぞれ形成されている。なお、各当接部材6と
しては、金属に限らず、樹脂材をその材質として採用し
ても良い。Each screw body 5 is made of a metal part such as an aluminum material, and has a general shape obtained by dividing a hollow sphere in half. These screwed bodies 5 are closely fixed to the outer wall surfaces of the fiber reinforced plastic hollow structure 2 at both outer ends on the spherical surface formed inside thereof. In addition, each screw 5
As the material, not only metal but also resin material may be adopted as the material. Each contact member 6 is made of, for example, a metal component such as an aluminum material, and has an inner wall surface that is in close contact with each end 2a of the fiber-reinforced plastic hollow structure 2. Then, these abutting members 6 are adhesively fixed to the outer wall surface of each end 2a on the inner wall surface thereof. Further, the outer wall surfaces of these abutting members 6 are in surface contact with the nut portion 1c of the rod end 1 that is screwed, and these rod end 1
Also, contact surfaces 6a that receive a tensile load, a compressive load, a bending load, or the like acting between the fiber-reinforced plastic hollow structures 2 are formed. Note that each contact member 6 is not limited to metal, and a resin material may be used as the material.
【0021】以上説明の構成を有する強度部材は、軽量
でありながらも、圧縮荷重、引張荷重、さらには曲げ荷
重に対して極めて高い強度を発揮できるため、この強度
部材を複数本、互いに組み合わせることにより、軽くて
強度的に優れ、しかも低コストなトラス構造を構成する
ことが可能である。このトラス構造の適した用途として
は、例えば、航空宇宙分野等の輸送構造物、建築構造
物、などが例示されるが、これに限らず、その他の幅広
い用途にも適用可能である。The strength member having the above-described structure is lightweight, but can exhibit extremely high strength against a compressive load, a tensile load, and a bending load. Therefore, a plurality of such strength members should be combined with each other. Thus, it is possible to construct a truss structure that is light and has excellent strength and is low in cost. Suitable applications of this truss structure are, for example, transportation structures in the aerospace field, building structures, etc., but are not limited to this, and are applicable to a wide range of other applications.
【0022】次に、図3及び図4を用いて、本実施形態
の強度部材の製造方法の一実施形態について以下に説明
する。なお、図3は、同強度部材の製造方法を説明する
ための図であって、金型内に挿入された強度部材を示す
断面図である。また、図4は、同金型内における同強度
部材の端部を示す部分拡大図である。また、図5は、同
強度部材の変形例を示す図であって、端部の部分拡大断
面図である。Next, one embodiment of the method for manufacturing the strength member of this embodiment will be described below with reference to FIGS. 3 and 4. 3 is a view for explaining the method for manufacturing the same strength member, and is a cross-sectional view showing the strength member inserted into the mold. Further, FIG. 4 is a partially enlarged view showing an end portion of the same strength member in the mold. FIG. 5 is a view showing a modified example of the same strength member, and is a partially enlarged cross-sectional view of the end portion.
【0023】本実施形態の製造方法は、以下に説明する
母材製造工程と、樹脂含浸工程と、当接部材取り付け工
程と、ロッドエンド取り付け工程とを経て製造される。
すなわち、図示を省略するが、母材製造工程では、各螺
着体5が予め外部に固定されているライナー4の周囲
に、強化繊維3を、各両端部2aにかけて収束するよう
に、ブレイディングやフィラメントワインディングなど
の手法を用いて繊維組織を形成し、繊維構造体を製造す
る。この時点では、まだ強化繊維3に樹脂が含浸されて
いない。The manufacturing method of this embodiment is manufactured through a base material manufacturing step, a resin impregnating step, a contact member attaching step, and a rod end attaching step, which will be described below.
That is, although not shown in the drawing, in the base material manufacturing process, braiding is performed so that the reinforcing fibers 3 are converged around both ends 2a around the liner 4 in which each screw 5 is fixed to the outside in advance. A fiber structure is manufactured by forming a fiber structure using a method such as a filament winding method. At this point, the reinforcing fibers 3 have not yet been impregnated with the resin.
【0024】続く樹脂含浸工程では、まず、前記母材製
造工程後の前記繊維構造体の繊維組織(強化繊維3)
に、溶融した樹脂を含浸させる。すなわち、図3に示す
ように、前記繊維構造体を、該繊維構造体を収容する凹
部10aが形成された雌金型10(金型)内に密閉した
後、この凹部10a内に樹脂Lを注入することで前記繊
維組織に含浸させる。In the subsequent resin impregnation step, first, the fiber structure (reinforcing fiber 3) of the fiber structure after the base material manufacturing step.
Is impregnated with the molten resin. That is, as shown in FIG. 3, after sealing the fiber structure in a female mold 10 (mold) in which a recess 10a for accommodating the fiber structure is formed, the resin L is placed in the recess 10a. The fibrous tissue is impregnated by injection.
【0025】この雌金型10は、樹脂注入ポート10b
を介して、樹脂Lの収容タンク11に接続されており、
収容タンク11から凹所10a内への樹脂注入が可能と
なっている。また、雌金型10には、凹所10a内に連
通する排気口10cを介して、図示されない真空ポンプ
に接続されている。したがって、この真空ポンプで凹所
10a内を真空引きすると同時に、樹脂Lの注入を行う
ことにより、凹所10aの内壁面とライナー4の外周面
との間に気泡を生じることなく樹脂Lが充填されるもの
となっている。これにより、強化繊維3に隙間なく樹脂
Lが含浸されていく。This female mold 10 is provided with a resin injection port 10b.
Is connected to the storage tank 11 for the resin L via
Resin can be injected into the recess 10a from the storage tank 11. Further, the female die 10 is connected to a vacuum pump (not shown) via an exhaust port 10c communicating with the inside of the recess 10a. Therefore, by vacuuming the inside of the recess 10a with this vacuum pump and at the same time injecting the resin L, the resin L is filled without generating bubbles between the inner wall surface of the recess 10a and the outer peripheral surface of the liner 4. It is supposed to be done. As a result, the reinforcing fiber 3 is impregnated with the resin L without any gap.
【0026】なお、この樹脂含浸工程における樹脂注入
中のライナー4は、凹所10a内に充填される樹脂Lに
よって周囲からの圧縮荷重を受けるが、このライナー4
が、図示されない加圧ポンプからの圧縮空気Aによって
一定内圧に保たれているので、へこむことなくその形状
を適切に維持することができ、繊維組織に形状を付与す
るための雄型としての機能を十分に発揮できるようにな
っている。この時のライナー4の内部加圧は、ロッドエ
ンド1が取り付けられる端部の貫通孔を利用して行われ
る。これにより、内部加圧を行うためだけの専用の孔を
強度部材壁面に形成する必要がないものとなっている。The liner 4 during resin injection in the resin impregnation step receives a compressive load from the surroundings by the resin L filled in the recess 10a.
However, since it is kept at a constant internal pressure by compressed air A from a pressurizing pump (not shown), its shape can be appropriately maintained without being dented, and the function as a male mold for imparting a shape to the fibrous tissue. It is designed to be able to fully demonstrate. Internal pressurization of the liner 4 at this time is performed by using a through hole at an end to which the rod end 1 is attached. As a result, it is not necessary to form a dedicated hole on the wall surface of the strength member only for performing internal pressurization.
【0027】なお、図4に示すように、加圧のための前
記貫通孔を有する端部は、雌金型10の外部に露出して
いるが、雌金型10内に備えられているOリング12で
シールされているため、ここから外部に樹脂Lが漏れな
いようになっている。排気口10cから樹脂Lが雌金型
10外に出てくることで、凹所10a内への樹脂注入が
完了したと判断されるので、樹脂注入を停止させる。そ
して、雌金型10を所定時間加熱した後、加熱を停止さ
せて常温まで雌金型10の冷却を行う。すると、強化繊
維3に含浸されている樹脂Lが硬化するので、雌金型1
0を開いて中身を取り出し、内部加圧のための両端の突
起部分を切り取る。As shown in FIG. 4, the end portion having the through hole for pressurizing is exposed to the outside of the female die 10, but is provided inside the female die 10. Since it is sealed by the ring 12, the resin L does not leak to the outside from here. When the resin L comes out of the female die 10 through the exhaust port 10c, it is determined that the resin injection into the recess 10a is completed, and therefore the resin injection is stopped. After heating the female die 10 for a predetermined time, the heating is stopped and the female die 10 is cooled to room temperature. Then, the resin L impregnated in the reinforcing fiber 3 is cured, so that the female mold 1
Open 0, take out the contents, and cut off the protruding parts at both ends for internal pressurization.
【0028】続く当接部材取り付け工程では、各当接部
材6を、繊維強化プラスチック中空構造体2の両端2a
それぞれに接着固定する。そして、前記各雌ねじ部2b
の雌ねじを切ることにより、図1に示す状態となり、繊
維強化プラスチック中空構造体2が完成する。続くロッ
ドエンド取り付け工程(取り付け工程)では、上記樹脂
含浸工程後の両端2aに、ロッドエンド1を完全に螺着
させることで、図2に示す固定状態となり、強度部材の
完成となる。In the subsequent contact member attaching step, each contact member 6 is attached to both ends 2a of the fiber reinforced plastic hollow structure 2.
Adhesively fixed to each. Then, each female screw portion 2b
By cutting the female screw of, the state shown in FIG. 1 is obtained, and the fiber-reinforced plastic hollow structure 2 is completed. In the subsequent rod end attaching step (attaching step), the rod ends 1 are completely screwed to both ends 2a after the resin impregnation step, whereby the fixed state shown in FIG. 2 is obtained, and the strength member is completed.
【0029】以上説明の本実施形態の強度部材は、各ロ
ッドエンド1と、両端部2aに向かって収束する繊維強
化プラスチック中空構造体2とを備え、該繊維強化プラ
スチック中空構造体2の両端部2aに雌ねじ部2bを形
成する構成を採用した。また、その製造方法において
は、母材製造工程と、樹脂含浸工程と、当接部材取り付
け工程と、ロッドエンド取り付け工程とを経て製造する
方法を採用した。この強度部材の構成及び製造方法によ
れば、強度部材の両端部2aが、胴体と同じ繊維強化複
合材料で構成されており、別部品でかつ重量のある金属
部品を必要としないため、低コスト化と軽量化を同時に
達成することが可能となっている。The strength member of the present embodiment described above includes each rod end 1 and the fiber reinforced plastic hollow structure 2 that converges toward both ends 2a, and both end parts of the fiber reinforced plastic hollow structure 2 are provided. The structure in which the female screw portion 2b is formed on 2a is adopted. Further, in the manufacturing method, a method of manufacturing through a base material manufacturing step, a resin impregnation step, a contact member attaching step, and a rod end attaching step is adopted. According to the structure and the manufacturing method of the strength member, both ends 2a of the strength member are made of the same fiber reinforced composite material as the body, and a separate and heavy metal part is not required, so that the cost is low. It is possible to achieve both weight reduction and weight reduction at the same time.
【0030】また、本実施形態の強度部材は、繊維強化
プラスチック中空構造体2の内部に各螺着体5を一体に
備える構成を採用した。この構成によれば、各ロッドエ
ンド1と繊維構造体2との間の螺着部分の長さを十分に
長く確保できるため、繊維構造体2に対する各ロッドエ
ンド1の固定強度を強固にすることが可能となってい
る。Further, the strength member of the present embodiment employs a structure in which the respective threaded members 5 are integrally provided inside the fiber reinforced plastic hollow structure 2. According to this configuration, the length of the threaded portion between each rod end 1 and the fibrous structure 2 can be ensured to be sufficiently long, so that the fixing strength of each rod end 1 to the fibrous structure 2 is strengthened. Is possible.
【0031】また、本実施形態の強度部材は、繊維強化
プラスチック中空構造体2の両端2aの外部に、引張荷
重や圧縮荷重あるいは曲げ荷重等を受ける当接面6aを
備えた当接部材を接着固定する構成を採用した。この構
成によれば、当接部材6を介して繊維強化プラスチック
中空構造体2に荷重を均等に逃がすことにより、荷重が
集中しないように分散させることができるので、機械的
強度のさらなる向上が達成可能であり、強度部材として
の高い信頼性を確保することが可能となっている。In the strength member of this embodiment, an abutting member having an abutting surface 6a for receiving a tensile load, a compressive load, a bending load or the like is adhered to the outside of both ends 2a of the fiber reinforced plastic hollow structure 2. The fixed structure is adopted. According to this configuration, the load can be dispersed so as not to be concentrated by uniformly escaping the load to the fiber-reinforced plastic hollow structure 2 through the contact member 6, and thus the mechanical strength is further improved. It is possible, and it is possible to secure high reliability as a strength member.
【0032】また、本実施形態の強度部材の製造方法で
は、前記樹脂含浸工程で、前記繊維構造体を雌金型10
内に密閉した後、真空引きしながら樹脂Lを注入するこ
とで繊維組織に含浸させる方法を採用した。この方法に
よれば、樹脂Lが、確実に隙間なく繊維組織に含浸され
ていくので、欠陥のない強度部材を確実に製造すること
が可能となっている。Further, in the method for manufacturing a strength member of this embodiment, the fiber structure is made into the female mold 10 in the resin impregnation step.
After sealing the inside, a method of impregnating the fiber structure by injecting the resin L while drawing a vacuum was adopted. According to this method, the resin L is surely impregnated into the fibrous structure without any gaps, so that it is possible to reliably manufacture a defect-free strength member.
【0033】なお、上記実施形態では、繊維強化プラス
チック中空構造体2の両端2aそれぞれに形成した各雌
ねじ部2bに、各ロッドエンド1を直接、螺着させるも
のとしたが、これに限らず、例えば図5に示すように、
雌ねじ孔13aが同軸に形成されたボルト13を繊維強
化プラスチック中空構造体2の両端2aに螺着させ、そ
の雌ねじ孔13aに、各ロッドエンド1を螺着させて取
り付ける構成も採用可能である。In the above embodiment, the rod ends 1 are directly screwed to the female screw portions 2b formed at both ends 2a of the fiber reinforced plastic hollow structure 2, but the present invention is not limited to this. For example, as shown in FIG.
It is also possible to adopt a configuration in which the bolts 13 in which the female screw holes 13a are formed coaxially are screwed to both ends 2a of the fiber reinforced plastic hollow structure 2, and the rod ends 1 are screwed and attached to the female screw holes 13a.
【0034】[0034]
【発明の効果】本発明の請求項1に記載の強度部材は、
結合体と、端部に向かって収束する繊維強化プラスチッ
ク中空構造体とを備え、該繊維強化プラスチック中空構
造体の端部に螺合部を設ける構成を採用した。この構成
によれば、強度部材の端部が、胴体と同じ繊維強化複合
材料で構成されており、別部品でかつ重量のある金属部
品を必要としないため、低コスト化と軽量化を同時に達
成することが可能となる。The strength member according to claim 1 of the present invention is
A structure is provided in which a combined body and a fiber-reinforced plastic hollow structure that converges toward the end are provided, and a screw portion is provided at the end of the fiber-reinforced plastic hollow structure. According to this configuration, since the end portion of the strength member is made of the same fiber reinforced composite material as the body, there is no need for a separate and heavy metal part, so that cost reduction and weight reduction can be achieved at the same time. It becomes possible to do.
【0035】また、請求項2に記載の強度部材は、請求
項1に記載の強度部材において、前記繊維強化プラスチ
ック中空構造体の内部に螺着体を一体に備える構成を採
用した。この構成によれば、結合体と繊維構造体との間
の螺着長さを十分に長く確保できるため、繊維構造体に
対する結合体の固定強度を強固にすることが可能とな
る。The strength member according to a second aspect of the invention is the strength member according to the first aspect of the invention, in which the threaded body is integrally provided inside the fiber-reinforced plastic hollow structure. According to this configuration, the screwing length between the combined body and the fiber structure can be sufficiently long, so that the fixing strength of the combined body with respect to the fiber structure can be strengthened.
【0036】また、請求項3に記載の強度部材は、請求
項1または請求項2に記載の強度部材において、前記繊
維強化プラスチック中空構造体の外部に、引張荷重や圧
縮荷重あるいは曲げ荷重等を受ける当接面を備えた当接
部材を固定する構成を採用した。この構成によれば、当
接部材を介して繊維強化プラスチック中空構造体に荷重
を逃がすことにより、荷重が集中しないように分散させ
ることができるので、機械的強度のさらなる向上が達成
可能であり、強度部材としての高い信頼性を確保するこ
とが可能となる。The strength member according to a third aspect is the strength member according to the first or second aspect, in which a tensile load, a compressive load, a bending load, or the like is applied to the outside of the fiber-reinforced plastic hollow structure. A structure for fixing an abutting member having an abutting surface for receiving is adopted. According to this configuration, by releasing the load to the fiber-reinforced plastic hollow structure via the contact member, it is possible to disperse the load so as not to concentrate, it is possible to further improve the mechanical strength, It becomes possible to secure high reliability as a strength member.
【0037】また、請求項4に記載のトラス構造は、請
求項1から請求項3のいずれか1項に記載の強度部材を
用いる構成を採用した。この構成によれば、その強度部
材が、低コスト化と軽量化を同時に達成できるため、低
コストで軽量なトラス構造を構成することが可能とな
る。Further, the truss structure described in claim 4 adopts a structure using the strength member described in any one of claims 1 to 3. According to this configuration, the strength member can simultaneously achieve cost reduction and weight reduction, so that it is possible to configure a low cost and lightweight truss structure.
【0038】また、請求項5に記載の強度部材の製造方
法は、型材の周囲に、その端部にかけて収束するように
繊維組織を形成して繊維構造体を製造する母材製造工程
と、繊維組織に溶融した樹脂を含浸させて固める樹脂含
浸工程と、結合部材を取り付ける取り付け工程とを有す
る方法を採用した。この方法によれば、製造された強度
部材の端部が、胴体と同じ繊維強化複合材料で構成され
ており、別部品でかつ重量のある金属部品を必要としな
いため、低コスト化と軽量化を同時に達成することが可
能となる。In the method for manufacturing a strength member according to a fifth aspect of the present invention, there is provided a base material manufacturing step of manufacturing a fiber structure by forming a fiber structure around the mold material so that the fiber structure is converged toward the ends thereof. A method having a resin impregnation step of impregnating the tissue with molten resin to solidify it and an attaching step of attaching a coupling member was adopted. According to this method, the end portion of the manufactured strength member is made of the same fiber reinforced composite material as the body, and since a separate and heavy metal part is not required, cost reduction and weight reduction can be achieved. Can be achieved at the same time.
【0039】また、請求項6に記載の強度部材の製造方
法は、請求項5に記載の強度部材の製造方法において、
前記樹脂含浸工程で、前記繊維構造体を金型内に密閉し
た後、樹脂を注入することで繊維組織に含浸させる方法
を採用した。この方法によれば、樹脂が、確実に隙間な
く繊維組織に含浸されていくので、欠陥のない強度部材
を確実に製造することが可能となる。The method for manufacturing a strength member according to claim 6 is the same as the method for manufacturing a strength member according to claim 5,
In the resin impregnation step, after the fiber structure was sealed in a mold, a resin was injected to impregnate the fiber structure. According to this method, the resin is surely impregnated into the fibrous structure without any gaps, so that it is possible to reliably manufacture a defect-free strength member.
【0040】また、請求項7に記載の強度部材の製造方
法は、請求項6に記載の強度部材の製造方法において、
前記型材として中空部材を用い、前記樹脂含浸工程で、
樹脂注入中の型材に内圧を加えることで繊維組織の形状
を保持する方法を採用した。この方法によれば、中空の
型材を用いることにより、強化部材を軽量化することが
可能となる。さらに、この型材は、中空でありながら
も、樹脂注入中には、内圧を受けて型としての強度を確
保できるようになっているため、製品の歩留まりを良く
することも可能となっている。The method for manufacturing a strength member according to claim 7 is the same as the method for manufacturing a strength member according to claim 6,
Using a hollow member as the mold material, in the resin impregnation step,
A method of retaining the shape of the fiber structure by applying internal pressure to the mold material during resin injection was adopted. According to this method, it is possible to reduce the weight of the reinforcing member by using the hollow mold member. Further, although this mold material is hollow, it is possible to secure the strength as a mold by receiving internal pressure during resin injection, so that it is possible to improve the product yield.
【0041】また、請求項8に記載の強度部材の製造方
法は、請求項7に記載の強度部材の製造方法において、
前記型材の内部加圧を、結合部材が取り付けられる貫通
孔より行う方法を採用した。この方法によれば、内部加
圧を行うためだけの孔を強度部材壁面に形成する必要が
ないので、製造後の強度部材に、余計な孔が残ることが
ない。したがって、強度部材の強度低下が防止可能とな
っている。The method of manufacturing a strength member according to claim 8 is the same as the method of manufacturing a strength member according to claim 7,
A method of applying internal pressure to the mold through a through hole to which a coupling member is attached is adopted. According to this method, it is not necessary to form a hole in the wall of the strength member only for performing internal pressurization, so that no extra hole is left in the strength member after manufacturing. Therefore, it is possible to prevent the strength of the strength member from decreasing.
【0042】また、請求項9に記載の強度部材の製造方
法は、請求項5から請求項8のいずれか1項に記載の強
度部材の製造方法において、前記母材製造工程で、前記
型材の端部に被結合部材を取り付けて一体とした上で、
繊維組織を形成する方法を採用した。この方法によれ
ば、被結合部材がない場合に比較して、繊維構造体に対
する結合体の固定強度を強固にすることが可能となる。A method for manufacturing a strength member according to a ninth aspect is the method for manufacturing a strength member according to any one of the fifth to eighth aspects, in which the base material manufacturing step is performed to produce the mold material. After attaching the member to be joined to the end to make it integral,
The method of forming fibrous tissue was adopted. According to this method, as compared with the case where there is no member to be bonded, it becomes possible to strengthen the fixing strength of the bonded body to the fiber structure.
【図1】 本発明の強度部材の一実施形態を示す図であ
って、その軸線を含む断面で見た場合の断面図である。FIG. 1 is a view showing an embodiment of a strength member of the present invention and is a cross-sectional view when seen in a cross section including an axis thereof.
【図2】 同強度部材の端部を示す部分拡大図であるFIG. 2 is a partially enlarged view showing an end portion of the same strength member.
【図3】 同強度部材の製造方法を説明するための図で
あって、金型内に挿入された強度部材を示す断面図であ
る。FIG. 3 is a view for explaining the method of manufacturing the same strength member, and is a cross-sectional view showing the strength member inserted into the mold.
【図4】 同金型内における同強度部材の端部を示す部
分拡大図である。FIG. 4 is a partial enlarged view showing an end portion of the same strength member in the mold.
【図5】 同強度部材の変形例を示す図であって、端部
の部分拡大断面図である。FIG. 5 is a diagram showing a modified example of the same strength member, and is a partially enlarged cross-sectional view of an end portion.
1・・・ロッドエンド(結合体) 2・・・繊維強化プラスチック中空構造体 2a・・・端部 2b・・・雌ねじ孔(螺合部) 3・・・強化繊維(繊維組織) 4・・・ライナー(型材) 5・・・螺着体(螺着体、被結合部材) 6・・・当接部材 6a・・・当接面 10・・・雌金型(金型) 10a・・・凹部 L・・・樹脂 1 ... Rod end (combined body) 2 ... Fiber reinforced plastic hollow structure 2a ... end 2b: Female screw hole (threaded portion) 3 ... Reinforcing fiber (fiber structure) 4 ... Liner (mold material) 5 ... Threaded body (threaded body, member to be coupled) 6 ... Contact member 6a ... Abutting surface 10 ... Female mold (mold) 10a ... recess L: Resin
フロントページの続き (72)発明者 浅田 正一郎 愛知県名古屋市港区大江町10番地 三菱重 工業株式会社名古屋航空宇宙システム製作 所内 (72)発明者 中込 良之 愛知県名古屋市港区大江町10番地 三菱重 工業株式会社名古屋航空宇宙システム製作 所内 (72)発明者 新屋 雅弘 愛知県名古屋市港区大江町10番地 三菱重 工業株式会社名古屋航空宇宙システム製作 所内 Fターム(参考) 2E163 DA02 DA04 FE03 FF73 4F205 AB11 AD16 AG07 AG21 AH47 AM28 HA06 HA25 HA35 HA47 HB01 HC07 HF30 HK17 HK32 HM06 HW02 HW21 Continued front page (72) Inventor Shoichiro Asada Mitsubishi Heavy, 10 Oemachi, Minato-ku, Nagoya-shi, Aichi Industrial Co., Ltd. Nagoya Aerospace System Production In-house (72) Inventor Yoshiyuki Nakagome Mitsubishi Heavy, 10 Oemachi, Minato-ku, Nagoya-shi, Aichi Industrial Co., Ltd. Nagoya Aerospace System Production In-house (72) Inventor Masahiro Shinya Mitsubishi Heavy, 10 Oemachi, Minato-ku, Nagoya-shi, Aichi Industrial Co., Ltd. Nagoya Aerospace System Production In-house F term (reference) 2E163 DA02 DA04 FE03 FF73 4F205 AB11 AD16 AG07 AG21 AH47 AM28 HA06 HA25 HA35 HA47 HB01 HC07 HF30 HK17 HK32 HM06 HW02 HW21
Claims (9)
達を行う強度部材において、 前記部材に取り付けられる結合体と、該結合体が固定さ
れる端部に向かって収束する繊維強化プラスチック中空
構造体とを備え、 該繊維強化プラスチック中空構造体の前記端部には、前
記結合体が螺着する螺合部が設けられていることを特徴
とする強度部材。1. A strength member arranged between members for transmitting a load between the members, wherein a joined body attached to the member and a fiber reinforced plastic hollow converging toward an end to which the joined body is fixed. And a structure, wherein the end portion of the fiber-reinforced plastic hollow structure is provided with a screwing portion to which the coupling body is screwed.
螺合部の少なくとも一部をなす螺着体が一体に備えられ
ていることを特徴とする強度部材。2. The strength member according to claim 1, wherein the fiber-reinforced plastic hollow structure is integrally provided with a threaded body that forms at least a part of the threaded portion. And strength members.
材において、 前記繊維強化プラスチック中空構造体の外部には、前記
端部に螺着された前記結合体に対して面接触し、これら
繊維強化プラスチック中空構造体及び結合体間に作用す
る引張荷重や圧縮荷重あるいは曲げ荷重等を受ける当接
面を備えた当接部材が固定されていることを特徴とする
強度部材。3. The strength member according to claim 1 or 2, wherein the fiber-reinforced plastic hollow structure is in surface contact with the outside of the fiber-reinforced plastic hollow structure, and the combined structure is screwed to the end. A strength member, characterized in that an abutting member having an abutting surface that receives a tensile load, a compressive load, a bending load, or the like acting between the fiber-reinforced plastic hollow structure and the bonded body is fixed.
記載の強度部材が用いられていることを特徴とするトラ
ス構造。4. A truss structure, wherein the strength member according to any one of claims 1 to 3 is used.
ら部材間の荷重伝達を行う強度部材の製造方法におい
て、 型材の周囲に、前記結合部材が取り付けられる端部にか
けて収束するように繊維組織を形成して繊維構造体を製
造する母材製造工程と、 該母材製造工程後の前記繊維構造体の繊維組織に、溶融
した樹脂を含浸させて固める樹脂含浸工程と、 該樹脂含浸工程後の前記端部に、前記結合部材を取り付
ける取り付け工程とを有することを特徴とする強度部材
の製造方法。5. A method of manufacturing a strength member, which is arranged between members via a connecting member and transmits a load between these members, wherein the fiber is converged around a mold member toward an end to which the connecting member is attached. A base material manufacturing step of forming a structure to manufacture a fiber structure; a resin impregnation step of impregnating a molten resin into the fiber structure of the fiber structure after the base material manufacturing step to solidify the resin; and the resin impregnating step. And a step of attaching the coupling member to the end portion afterward.
おいて、 前記樹脂含浸工程では、前記繊維構造体を収容する凹部
が形成された金型内に、前記繊維構造体を密閉した後、
前記凹部内に前記樹脂を注入することで前記繊維組織に
含浸させることを特徴とする強度部材の製造方法。6. The method for manufacturing a strength member according to claim 5, wherein, in the resin impregnating step, after sealing the fiber structure in a mold in which a recess for accommodating the fiber structure is formed,
A method for manufacturing a strength member, characterized in that the fiber structure is impregnated by injecting the resin into the recess.
おいて、 前記型材として熱可塑性樹脂等の伸縮可能な材料からな
る中空部材を用い、前記樹脂含浸工程では、前記樹脂注
入中の前記型材に内圧を加えることで、前記繊維組織の
形状を保持することを特徴とする強度部材の製造方法。7. The method for manufacturing a strength member according to claim 6, wherein a hollow member made of a stretchable material such as a thermoplastic resin is used as the mold member, and the mold member during the resin injection is used in the resin impregnation step. A method for manufacturing a strength member, characterized in that the shape of the fiber structure is maintained by applying internal pressure to the.
おいて、 前記型材の内部加圧を、前記結合部材が取り付けられる
貫通孔より行うことを特徴とする強度部材の製造方法。8. The method of manufacturing a strength member according to claim 7, wherein the internal pressure of the mold member is applied through a through hole to which the coupling member is attached.
記載の強度部材の製造方法において、 前記母材製造工程では、前記型材の端部に、前記結合部
材と結合する被結合部材を取り付けて一体とした上で、
これら型材及び被結合部材の周囲に前記繊維組織を形成
することを特徴とする強度部材の製造方法。9. The method for manufacturing a strength member according to claim 5, wherein in the base material manufacturing step, a joined member that joins the joining member to an end portion of the mold member. After attaching and integrating
A method for manufacturing a strength member, characterized in that the fibrous structure is formed around these mold members and members to be bonded.
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| JP2002137521A JP3692329B2 (en) | 2002-05-13 | 2002-05-13 | Strength member, truss structure, and method of manufacturing strength member |
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|---|---|---|---|
| JP2002137521A JP3692329B2 (en) | 2002-05-13 | 2002-05-13 | Strength member, truss structure, and method of manufacturing strength member |
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| Publication Number | Publication Date |
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| JP3692329B2 JP3692329B2 (en) | 2005-09-07 |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2006194860A (en) * | 2004-12-16 | 2006-07-27 | Konica Minolta Medical & Graphic Inc | Radiological image conversion panel and method of manufacturing radiological image conversion panel |
| WO2009017217A1 (en) | 2007-08-01 | 2009-02-05 | Toyota Jidosha Kabushiki Kaisha | Fiber-reinforced resin hollow part with flange and method of forming the same |
| WO2009078419A1 (en) | 2007-12-17 | 2009-06-25 | Toyota Jidosha Kabushiki Kaisha | Method of molding fiber-reinforced-resin hollow part |
| KR20190131008A (en) | 2017-03-29 | 2019-11-25 | 후쿠이 켄 | Connection structure of fiber-reinforced plastic structural member and processing method of connection part |
| CN112727636A (en) * | 2020-12-18 | 2021-04-30 | 内蒙古航天红峡化工有限公司 | Forming die for combustion-limiting layer of small-diameter engine combustion chamber |
-
2002
- 2002-05-13 JP JP2002137521A patent/JP3692329B2/en not_active Expired - Fee Related
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2006194860A (en) * | 2004-12-16 | 2006-07-27 | Konica Minolta Medical & Graphic Inc | Radiological image conversion panel and method of manufacturing radiological image conversion panel |
| WO2009017217A1 (en) | 2007-08-01 | 2009-02-05 | Toyota Jidosha Kabushiki Kaisha | Fiber-reinforced resin hollow part with flange and method of forming the same |
| US8808480B2 (en) | 2007-08-01 | 2014-08-19 | Toyota Jidosha Kabushiki Kaisha | Flanged fiber-reinforced resin hollow part and method of molding the same |
| WO2009078419A1 (en) | 2007-12-17 | 2009-06-25 | Toyota Jidosha Kabushiki Kaisha | Method of molding fiber-reinforced-resin hollow part |
| US8932421B2 (en) | 2007-12-17 | 2015-01-13 | Toyota Jidosha Kabushiki Kaisha | Method of molding fiber-reinforced plastic hollow part |
| KR20190131008A (en) | 2017-03-29 | 2019-11-25 | 후쿠이 켄 | Connection structure of fiber-reinforced plastic structural member and processing method of connection part |
| CN112727636A (en) * | 2020-12-18 | 2021-04-30 | 内蒙古航天红峡化工有限公司 | Forming die for combustion-limiting layer of small-diameter engine combustion chamber |
Also Published As
| Publication number | Publication date |
|---|---|
| JP3692329B2 (en) | 2005-09-07 |
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