JPH05459A - Structure component using fiber reinforced resin composite material - Google Patents

Structure component using fiber reinforced resin composite material

Info

Publication number
JPH05459A
JPH05459A JP3007524A JP752491A JPH05459A JP H05459 A JPH05459 A JP H05459A JP 3007524 A JP3007524 A JP 3007524A JP 752491 A JP752491 A JP 752491A JP H05459 A JPH05459 A JP H05459A
Authority
JP
Japan
Prior art keywords
fiber
plate
frp
fibers
reinforced resin
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.)
Pending
Application number
JP3007524A
Other languages
Japanese (ja)
Inventor
Koichi Motonaga
光一 元永
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Hitachi Ltd
Hitachi Kasado Engineering Co Ltd
Original Assignee
Hitachi Ltd
Hitachi Kasado Engineering Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Hitachi Ltd, Hitachi Kasado Engineering Co Ltd filed Critical Hitachi Ltd
Priority to JP3007524A priority Critical patent/JPH05459A/en
Publication of JPH05459A publication Critical patent/JPH05459A/en
Pending legal-status Critical Current

Links

Classifications

    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T30/00Transportation of goods or passengers via railways, e.g. energy recovery or reducing air resistance

Landscapes

  • Rod-Shaped Construction Members (AREA)
  • Laminated Bodies (AREA)
  • Moulding By Coating Moulds (AREA)

Abstract

PURPOSE:To strengthen a plate end section by forming a curved face of large diameter on the plate end section of a component or forming a beading shape so that the fiber is not cut by the plate end section. CONSTITUTION:A side beam consist of a web 11a formed by FRP, a flange 11b and a plate-shaped core 12 with folded both ends forming a curved face. FRP is formed by rotating cloth-shaped prepregs. composed of fibers in one direction by 45 deg. and laminating the same in multi-folds in the four directions, and side beams, transverse beams and end beams are arranged as if integrated and wound in a manner of not cutting the fibers in the prepregs. As the core material 12 is put in so that the curvature radius of fibers is not getting smaller at the plate end section of the component, the fibers have not to be cut at the plate end section even if the prepregs in which fibers are arranged with resin are laminated in multi-folds in the four directions while being shifted by approximately 45 deg., and the strength at the plate section of FRP is not at all lowered.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【産業上の利用分野】本発明は、繊維強化樹脂複合材料
(以下「FRP」という)によって構成した構造部材に
係り、特に梁や枠の構造に関するものである。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a structural member made of a fiber reinforced resin composite material (hereinafter referred to as "FRP"), and more particularly to a beam or frame structure.

【0002】[0002]

【従来の技術】各種構造物の主要強度部材で軽量化が要
求される場合は高強度の繊維を使用したFRPが検討の
対象になり、特に交通機械の主要部材では軽量化が厳し
く要求されるのでFRPが多用されている。例えば、
(財)日本規格協会発行(1990.7.31刊)“次世代複
合材料技術ハンドブック”に詳細に述べられており、同
刊行物のP.61図2、1、24にアングル、P.255
図2、2、166に炭素繊維製三次元織物のI型材、
P.518表4、2、5に航空機の各種の構造材が記述
されている。FRPを強化する繊維の引張強さは金属の
引張強さに比べて大きいものがあり、この特徴を生かす
ためには連続した繊維を使用しなければならない。FR
Pを強化する繊維の伸びは金属に比べて非常に小さいの
で、繊維を金属なみに曲げるような加工を行うと繊維が
切れてしまう。梁や枠の板端部ではFRPの繊維を小さ
い曲線半径で曲げることができないために、最も強度を
必要とする板端部で繊維を切ってしまわざるを得ないと
いう場合がしばしばあった。本発明の対象となる従来の
FRPを使用した梁や枠の代表として鉄道車両の台車枠
を取り上げて説明する。
2. Description of the Related Art When weight reduction is required for main strength members of various structures, FRP using high-strength fiber is an object of consideration, and particularly for main members of traffic machines, weight reduction is strictly required. Therefore, FRP is frequently used. For example,
It is described in detail in “Next Generation Composite Material Technology Handbook” published by Japan Standards Association (published in 1990.31.31). Pg. 61, Figures 2, 1 and 24 of that publication, Angle, P. 255
2, 2, 166, I-shaped material of carbon fiber three-dimensional fabric,
Tables 4, 2 and 5 on page 518 describe various structural materials for aircraft. The tensile strength of the fiber that strengthens FRP is greater than that of metal, and continuous fibers must be used to take advantage of this feature. FR
The elongation of the fiber that strengthens P is much smaller than that of metal, so if the fiber is bent like a metal, the fiber will break. Since the FRP fiber cannot be bent with a small curve radius at the plate end of the beam or frame, it is often necessary to cut the fiber at the plate end that requires the most strength. A bogie frame of a railroad vehicle will be described as a representative of beams and frames using the conventional FRP which is the subject of the present invention.

【0003】FRPを材料とした従来の梁によって構成
される台車枠について図9に平面図及び図10に正面図
を示し、図10のE−E断面拡大図を図11に示し、図
9のF−F断面拡大図を図12に、図9のG−G断面拡
大図を図13にそれぞれ示している。61はFRPを材
料とした側梁、62はFRPを材料とした横梁、63は
FRPを材料とした端梁であり、側梁61はウエブ61
aとフランジ61bによって構成されたI形断面の梁で
あり、横梁62はウエブ62aとフランジ62bによっ
て構成された溝形断面の梁であり、端梁63はウエブ6
3aとフランジ63bによって構成された溝形断面の梁
である。
FIG. 9 is a plan view and FIG. 10 is a front view of a bogie frame composed of a conventional beam made of FRP, and FIG. 11 is an enlarged cross-sectional view taken along line EE of FIG. An enlarged view of the FF section is shown in FIG. 12, and an enlarged view of the GG section of FIG. 9 is shown in FIG. 61 is a side beam made of FRP, 62 is a lateral beam made of FRP, 63 is an end beam made of FRP, and the side beam 61 is a web 61.
a beam having an I-shaped cross section composed of a and a flange 61b, a horizontal beam 62 being a beam having a groove-shaped cross section composed of a web 62a and a flange 62b, and an end beam 63 being a web 6.
It is a beam having a groove-shaped cross section constituted by 3a and a flange 63b.

【0004】FRPを材料としたI形断面や溝形断面の
梁によって構成された台車枠は軽量化を主目的としてお
り、側梁61、横梁62、端梁63の部材の板厚が非常
に薄いものによって構成するということが大前提とな
る。FRPによってこれらの部材を成形する方法として
は繊維を一方向に並べた布状のテ−プ(「プリプレグ」
と呼ばれている)を45°ずつ回転させて4方向に積層
するという方法(−45°、0°、45°、90°の4
方向に積層することを基本にして幾重にも積層し、擬似
等方性と呼ばれる特性を持たせた積層方法)が各種の交
通機関の部材で多用されている。FRPを強化する繊維
そのものは材料の伸びが非常に小さく、金属に比べて一
桁以上も異なる場合がある。FRPに使うこれらの繊維
は引張強さが非常に大きいのが特徴であり、該繊維が連
続したものを使用しなければ金属に比べて最も特長とさ
れている大きい引張強さを有効に使うということができ
なくなる。
A bogie frame made of a beam having an I-shaped section or a groove-shaped section made of FRP is intended mainly for weight reduction, and the plate thickness of the side beam 61, the lateral beam 62, and the end beam 63 is very large. The major premise is that it is composed of thin things. As a method of molding these members by FRP, a cloth-like tape in which fibers are arranged in one direction (“prepreg”)
It is called 45 degrees by 45 degrees and laminated in 4 directions (-45 degrees, 0 degrees, 45 degrees, 90 degrees 4
A stacking method in which multiple layers are stacked on the basis of stacking in the direction, and a property called pseudo-isotropic property) is widely used in various transportation members. The fiber itself that reinforces FRP has a very small elongation of the material and may differ by more than an order of magnitude compared with metal. The characteristic feature of these fibers used in FRP is that they have a very high tensile strength, and if they do not use continuous fibers, they will effectively use the large tensile strength that is most characterized compared to metals. Can't do it.

【0005】繊維を一方向に並べた布状のプリプレグを
45°ずつ回転させて4方向に積層する場合に板端部、
すなわち、フランジ端部で板の表と裏の間で繊維が連続
していることが強度的に不可欠である。しかし、部材の
板厚を薄くすると繊維の伸びが小さいためにフランジ端
部で繊維を曲げることができない場合があり、フランジ
端部に繊維の端部がくることになってフランジ端部が強
化されないという問題があった。したがって、フランジ
端部を強化するためには繊維を連続させることができる
構造にする必要がある。
When a cloth-like prepreg in which fibers are arranged in one direction is rotated by 45 ° and laminated in four directions, a plate end portion,
That is, it is essential in terms of strength that the fibers are continuous between the front and back of the plate at the flange end. However, if the plate thickness of the member is made thin, the fiber may not be able to bend at the flange end due to the small elongation of the fiber, and the fiber end will come to the flange end and the flange end will not be strengthened. There was a problem. Therefore, in order to strengthen the flange end, it is necessary to have a structure in which the fibers can be continuous.

【0006】[0006]

【発明が解決しようとする課題】上記従来技術はFRP
によって構成した梁や枠では部材の板端部で強度上大切
な繊維を切ることになり、FRPの強度が低下するとい
う問題があった。
DISCLOSURE OF THE INVENTION Problems to be Solved by the Invention
In the beam and the frame constituted by, the fiber important for strength is cut at the plate end of the member, and there is a problem that the strength of the FRP is reduced.

【0007】本発明の目的はFRPを主体とした梁や枠
の部材の板端部を強化することであり、これによって部
材を軽量化すると同時に強度的にバランスのとれた梁や
枠を提供することを目的としている。
An object of the present invention is to reinforce the plate ends of the members of the beam or frame mainly composed of FRP, thereby reducing the weight of the member and at the same time providing the beam or frame in which the strength is balanced. Is intended.

【0008】[0008]

【課題を解決するための手段】上記目的を達成するため
に、部材の板端部に大きい半径の曲面を設けたり、玉縁
状にして繊維が板端部で切られることがないようにした
ものである。
In order to achieve the above object, a curved surface having a large radius is provided at the plate end of the member, or a bead shape is used so that the fiber is not cut at the plate end. It is a thing.

【0009】また、板端部に曲面を持たせるために、板
端部に芯材を設けてその外周に繊維を一方向に並べた布
状のプリプレグを積層する構造にしたものである。
Further, in order to have a curved surface at the plate end portion, a core material is provided at the plate end portion and a cloth-like prepreg in which fibers are arranged in one direction is laminated on the outer periphery thereof.

【0010】さらに、板端部に曲面を形成し、かつ、軽
量化するために、中空の芯材を使用してその外周にプリ
プレグを積層したものである。
Furthermore, in order to form a curved surface at the plate end and to reduce the weight, a hollow core material is used and a prepreg is laminated on the outer periphery thereof.

【0011】そして、板端部で繊維を切らないようにす
ると同時にフランジの内面側を平面にするために、フラ
ンジの中に板状の芯材を入れてその外周にプリプレグを
積層したものである。
Then, in order to prevent the fibers from being cut at the plate ends and at the same time to make the inner surface side of the flange flat, a plate-shaped core material is put in the flange and a prepreg is laminated on the outer periphery thereof. .

【0012】[0012]

【作用】部材の板端部で繊維の曲げ半径が小さくならな
いように芯材を入れているので、繊維を樹脂で並べたプ
リプレグを約45°ずつずらしながら4方向に幾重にも
積層しても板端部で繊維を切らざるを得ないというよう
なことはなく、FRPの板端部で強度が低下することは
なくなる。
[Function] Since the core material is inserted so that the bending radius of the fiber does not become small at the plate end of the member, even if the prepregs in which the fibers are lined with the resin are shifted by about 45 ° and laminated in four directions There is no need to cut the fiber at the plate end, and the strength does not decrease at the plate end of the FRP.

【0013】芯材としては板端部に丸棒状のものを使用
したり、中空筒状のものを使用する場合もある。また、
フランジの表裏両面を平面にするために、フランジの中
に板状の芯材を使用したり、中空板状の芯材を使用する
ものもある。さらに、各芯材を薄板や小さな針状芯棒で
結合させて芯材間の寸法を保持する場合もある。
As the core material, a round bar-shaped material may be used at the end of the plate, or a hollow cylindrical material may be used. Also,
In some cases, a plate-shaped core material is used in the flange or a hollow plate-shaped core material is used in order to make both front and back surfaces of the flange flat. Further, the core members may be joined together by thin plates or small needle-shaped core rods to maintain the dimension between the core members.

【0014】[0014]

【実施例】本発明の梁や枠は全ての構造物の強度部材と
して使用が可能であるが、最も適用の対象になりやすい
のは交通機械の主要部材である。なかでも、航空機や鉄
道車両等の主要な強度部材では軽量化が厳しく追及され
るので、これらの強度部材としてFRP等による軽量化
が検討されて各種採用されている。本発明では鉄道車両
用の台車枠を念頭に置きながら台車枠の実施例を図1〜
図8にしたがって説明する。なお、本発明は必ずしも鉄
道車両に限定したものではない。
The beam and frame of the present invention can be used as a strength member for all structures, but the most applicable object is a main member of a traffic machine. In particular, since weight reduction is rigorously pursued in major strength members such as aircraft and railway vehicles, weight reduction by FRP or the like has been studied and variously adopted as these strength members. In the present invention, an example of a bogie frame is shown in FIG.
It will be described with reference to FIG. It should be noted that the present invention is not necessarily limited to railway vehicles.

【0015】FRPによって形成された本発明の台車枠
について図1に平面図及び図2に正面図を示し、図2の
A−A断面拡大図を図3に、図1のB−B断面拡大図を
図4に、図1のC−C断面拡大図を図5に、図1のD−
D断面拡大図を図6に示し、芯材を中空板状にした断面
図を図7に、芯材を中空筒状にした断面図を図8にそれ
ぞれ示している。
FIG. 1 is a plan view of the bogie frame of the present invention formed by FRP and FIG. 2 is a front view thereof. FIG. 3 is an enlarged sectional view taken along line AA of FIG. 2 and enlarged sectional view taken along line BB of FIG. FIG. 4 is a diagram, FIG. 5 is an enlarged cross-sectional view taken along line CC of FIG.
FIG. 6 shows an enlarged view of the D cross section, FIG. 7 shows a hollow plate-shaped cross section of the core member, and FIG. 8 shows a hollow cylindrical cross section of the core member.

【0016】11は台車枠の長手方向に配する側梁であ
り、側梁11はFRPによって形成されたウエブ11a
とフランジ11b及び両端を丸めて曲面を持たせた板状
の芯材12によって成り立っている。21は側梁11を
左右に結合する横梁であり、横梁21はFRPによって
形成されたウエブ21aとフランジ21b及び丸棒状の
芯材22によって成り立っている。31は側梁11を左
右に結合する端梁であり、端梁31はFRPによって形
成されたウエブ31aとフランジ31b及び両端を丸め
て曲面を持たせた板状の芯材32によって成り立ってい
る。
Reference numeral 11 is a side beam arranged in the longitudinal direction of the bogie frame, and the side beam 11 is a web 11a formed by FRP.
And a flange 11b and a plate-shaped core member 12 having both ends rounded to have a curved surface. Reference numeral 21 is a horizontal beam that connects the side beams 11 to the left and right, and the horizontal beam 21 is composed of a web 21a formed by FRP, a flange 21b, and a round bar-shaped core material 22. Reference numeral 31 is an end beam that connects the side beams 11 to the left and right, and the end beam 31 is made up of a web 31a formed by FRP, a flange 31b, and a plate-shaped core member 32 having both ends rounded to have a curved surface.

【0017】ウエブ11a、フランジ11b、ウエブ2
1a、フランジ21b、ウエブ31a、フランジ31b
はFRPであり、これらは繊維を一方向に並べた布状の
プリプレグを45°ずつ回転させて4方向に幾重にも積
層したものであって、側梁11、横梁21、端梁31が
あたかも一体のようにできるので前記のプリプレグ内の
繊維を切断することのないように巻き付けられている。
前記のプリプレグは両端を丸めて曲面を持たせた板状の
芯材12、丸棒状の芯材22、両端を丸めて曲面を持た
せた板状の芯材32の外周に巻き付けられている。芯材
12、22、32は相互に結合され、各芯材の位置関係
を保持している場合もあり、また、各芯材間は薄板や小
さな針状芯棒で結合して各芯材の位置関係を保持してい
る場合もある。側梁11、横梁21、端梁31の板端部
では曲面になるように前記の芯材12、22、32はい
ずれも曲面になっているので、芯材12、22、32の
外周に巻き付ける繊維はいずれも大きい半径で曲げるこ
とになり、繊維を切断せざるを得ないようなことはな
い。
Web 11a, Flange 11b, Web 2
1a, flange 21b, web 31a, flange 31b
Is an FRP, and these are cloth-like prepregs in which fibers are arranged in one direction rotated by 45 ° and laminated in multiple layers in four directions. Side beams 11, lateral beams 21, end beams 31 The fibers in the prepreg are wound so as not to be cut because they can be made as one piece.
The prepreg is wound around the outer circumference of a plate-shaped core material 12 having rounded ends and a curved surface, a round bar-shaped core material 22, and a plate-shaped core material 32 having rounded ends and a curved surface. The core members 12, 22, 32 may be connected to each other to maintain the positional relationship between the core members, and the core members may be connected by thin plates or small needle-shaped core rods. In some cases, the positional relationship is retained. Since all the core members 12, 22, 32 are curved so that the plate ends of the side beams 11, the lateral beams 21, and the end beams 31 are curved, the core members 12, 22, 32 are wound around the outer periphery of the core members 12, 22, 32. All the fibers are bent with a large radius, and there is no choice but to cut the fibers.

【0018】芯材を中空板状にした図7に示すI形断面
のフランジ部の断面図では両端を丸めて曲面を持たせた
板状の芯材41を中空板状としている。芯材を中空筒状
にした図8に示す板端部の断面図では芯材51を中空筒
状としている。芯材41、51はいずれも中空にして軽
量化をねらったものである。図7では繊維を一方向に並
べた布状のプリプレグを45°ずつ回転させて4方向に
幾重にも積層したFRP部材42が配置されており、芯
材41にはFRP部材42の繊維の曲げ半径を大きくす
るような凸部41aが設けられている。図8では繊維を
一方向に並べた布状のプリプレグを45°ずつ回転させ
て4方向に幾重にも積層したFRP部材52が配置され
ており、芯材51にはFRP部材52の繊維の曲げ半径
を大きくするような凸部51aが設けられている。そし
て、凸部41a、51aにはいずれも繊維が大きな曲線
半径で曲げられるように大きな凹曲面が設けられてい
る。
In the cross-sectional view of the flange portion of the I-shaped cross section shown in FIG. 7 in which the core material is a hollow plate shape, the plate-shaped core material 41 having both ends rounded to have a curved surface is a hollow plate shape. In the cross-sectional view of the end portion of the plate shown in FIG. 8 in which the core material has a hollow cylindrical shape, the core material 51 has a hollow cylindrical shape. The core materials 41 and 51 are both hollow to reduce the weight. In FIG. 7, the FRP member 42 in which cloth-like prepregs in which fibers are arranged in one direction are rotated by 45 ° and stacked in multiple layers in four directions is arranged, and the core material 41 bends the fibers of the FRP member 42. A convex portion 41a having a large radius is provided. In FIG. 8, a cloth-like prepreg in which fibers are arranged in one direction is rotated by 45 °, and an FRP member 52 in which multiple layers are laminated in four directions is arranged, and the core material 51 bends the fibers of the FRP member 52. A convex portion 51a having a large radius is provided. A large concave curved surface is provided on each of the convex portions 41a and 51a so that the fiber can be bent with a large curve radius.

【0019】本実施例では、繊維を小さな半径で曲げた
り、繊維そのものを切ることがないようにしており、F
RPの中に使用した繊維の強度を十分に発揮させること
ができる。したがって、本実施例によればFRPに期待
したい強度がそのまま保持されるので部材の軽量化も遺
憾なく行うことが可能となり、FRPによって強度部材
を軽量化することができる。
In this embodiment, the fiber is not bent at a small radius and the fiber itself is not cut.
The strength of the fibers used in the RP can be fully exerted. Therefore, according to the present embodiment, the strength desired for the FRP is maintained as it is, so that the weight of the member can be reduced without hesitation, and the strength member can be reduced by the FRP.

【0020】尚、本発明の梁や枠は軽量化を要するもの
であれば如何なるものにでも適用可能である。
The beam or frame of the present invention can be applied to any beam as long as it requires weight reduction.

【0021】[0021]

【発明の効果】本発明は、以上説明したように構成され
ているので以下に記載されるような効果を有する。
Since the present invention is constructed as described above, it has the following effects.

【0022】板端部の内部に芯材として曲面を有するも
のを設置しているので板端部で繊維を切る必要がなく、
板端部が強化される。さらに、板端部に玉縁を設けるこ
とになり、板端部が玉縁自身によっても強化される。
Since the core having a curved surface is installed inside the plate end, it is not necessary to cut the fiber at the plate end.
The plate edge is strengthened. Furthermore, since the bead is provided at the plate end, the plate end is also strengthened by the bead itself.

【0023】また、板端部や板部に中空の芯材を入れて
いるので芯材自体の質量も小さく抑えることができ、さ
らに、FRP自体に板端部で強度的な欠陥部を生じさせ
るようなことがなく、FRP内の繊維が有効に配置され
て部材全体の軽量化が可能である。
Further, since the hollow core material is put in the plate end portion or the plate portion, the mass of the core material itself can be kept small, and further, the FRP itself causes a strong defect portion at the plate end portion. Without such a situation, the fibers in the FRP are effectively arranged, and the weight of the entire member can be reduced.

【0024】したがって、本発明のFRPを使用した梁
や枠は強度上のばらつきをなくすることになり、ひいて
は軽量化を行うことができるという効果がある。
Therefore, the beam or frame using the FRP of the present invention eliminates variations in strength, which in turn has the effect of reducing the weight.

【図面の簡単な説明】[Brief description of drawings]

【図1】FRPを材料とした本発明の梁によって構成さ
れた台車枠の平面図である。
FIG. 1 is a plan view of a bogie frame constituted by a beam of the present invention made of FRP.

【図2】図1の正面図である。FIG. 2 is a front view of FIG.

【図3】図2のA−A断面拡大図である。3 is an enlarged cross-sectional view taken along the line AA of FIG.

【図4】図1のB−B断面拡大図である。4 is an enlarged cross-sectional view taken along the line BB of FIG.

【図5】図1のC−C断面拡大図である。5 is an enlarged cross-sectional view taken along line CC of FIG.

【図6】図1のD−D断面拡大図である。FIG. 6 is a magnified view taken along the line DD of FIG.

【図7】本発明の芯材を中空板状にした断面図である。FIG. 7 is a cross-sectional view of the core material of the present invention in the shape of a hollow plate.

【図8】本発明の芯材を中空筒状にした断面図である。FIG. 8 is a cross-sectional view in which the core material of the present invention has a hollow cylindrical shape.

【図9】FRPを材料とした従来の梁によって構成され
る台車枠の平面図である。
FIG. 9 is a plan view of a bogie frame composed of conventional beams made of FRP.

【図10】図9の正面図である。FIG. 10 is a front view of FIG. 9.

【図11】図10のE−E断面拡大図である。11 is an enlarged cross-sectional view taken along line EE of FIG.

【図12】図9のF−F断面拡大図である。12 is an enlarged view taken along line FF of FIG.

【図13】図9のG−G断面拡大図である。FIG. 13 is an enlarged view taken along line GG of FIG.

【符号の説明】[Explanation of symbols]

11,61…側梁、11a,21a,31a…ウエブ、
11b,21b,31b…フランジ、12,22,3
2,41,51…芯材、21,62…横梁、31,63
…端梁、41a,51a…凸部、42,52…FRP部
材。
11, 61 ... Side beams, 11a, 21a, 31a ... Web,
11b, 21b, 31b ... Flange, 12, 22, 3
2, 41, 51 ... Core material 21, 62 ... Horizontal beam, 31, 63
... end beams, 41a, 51a ... convex portions, 42, 52 ... FRP members.

Claims (9)

【特許請求の範囲】[Claims] 【請求項1】板端部の内部に曲面を有する芯材を設け、
該芯材の外表面に繊維が巻き付けられるように構成した
ことを特徴とする繊維強化樹脂複合材料を用いた構造部
材。
1. A core material having a curved surface is provided inside a plate end,
A structural member using a fiber-reinforced resin composite material, characterized in that fibers are wound around the outer surface of the core material.
【請求項2】前記芯材を丸棒状とした請求項1記載の繊
維強化樹脂複合材料を用いた構造部材。
2. A structural member using the fiber reinforced resin composite material according to claim 1, wherein the core material is formed into a round bar shape.
【請求項3】前記芯材を板状とした請求項1記載の繊維
強化樹脂複合材料を用いた構造部材。
3. A structural member using the fiber-reinforced resin composite material according to claim 1, wherein the core material is plate-shaped.
【請求項4】前記芯材を中空筒状とした請求項1記載の
繊維強化樹脂複合材料を用いた構造部材。
4. A structural member using the fiber reinforced resin composite material according to claim 1, wherein the core material is a hollow cylinder.
【請求項5】前記芯材を中空板状とした請求項1記載の
繊維強化樹脂複合材料を用いた構造部材。
5. A structural member using the fiber-reinforced resin composite material according to claim 1, wherein the core material is a hollow plate.
【請求項6】前記各芯材の間を結合させた請求項1から
請求項5までに記載の繊維強化樹脂複合材料を用いた構
造部材。
6. A structural member using the fiber-reinforced resin composite material according to claim 1, wherein the core materials are bonded together.
【請求項7】前記各芯材の間を薄板で結合させた請求項
6記載の繊維強化樹脂複合材料を用いた構造部材。
7. A structural member using a fiber reinforced resin composite material according to claim 6, wherein the core members are joined together by a thin plate.
【請求項8】前記各芯材の間を針状芯棒で結合させた請
求項6記載の繊維強化樹脂複合材料を用いた構造部材。
8. A structural member using a fiber-reinforced resin composite material according to claim 6, wherein the core members are connected by a needle-shaped core rod.
【請求項9】大きな凹曲面を有する凸部を芯材に設けた
請求項1から請求項8までに記載の繊維強化樹脂複合材
料を用いた構造部材。
9. A structural member using the fiber-reinforced resin composite material according to claim 1, wherein a convex portion having a large concave curved surface is provided on the core material.
JP3007524A 1991-01-25 1991-01-25 Structure component using fiber reinforced resin composite material Pending JPH05459A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP3007524A JPH05459A (en) 1991-01-25 1991-01-25 Structure component using fiber reinforced resin composite material

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP3007524A JPH05459A (en) 1991-01-25 1991-01-25 Structure component using fiber reinforced resin composite material

Publications (1)

Publication Number Publication Date
JPH05459A true JPH05459A (en) 1993-01-08

Family

ID=11668166

Family Applications (1)

Application Number Title Priority Date Filing Date
JP3007524A Pending JPH05459A (en) 1991-01-25 1991-01-25 Structure component using fiber reinforced resin composite material

Country Status (1)

Country Link
JP (1) JPH05459A (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4962744A (en) * 1988-08-29 1990-10-16 Toyota Jidosha Kabushiki Kaisha Device for detecting malfunction of fuel evaporative purge system
WO2006068089A1 (en) * 2004-12-21 2006-06-29 Thk Co., Ltd. Movement guiding device
JP2010163789A (en) * 2009-01-15 2010-07-29 Miyaji Iron Works Co Ltd Inspection passage
JP2010168780A (en) * 2009-01-21 2010-08-05 Miyaji Iron Works Co Ltd Inspection path
JP2011520690A (en) * 2008-05-16 2011-07-21 ザ・ボーイング・カンパニー REINFORCED REINFORCEMENT AND METHOD FOR PRODUCING REINFORCED REINFORCEMENT
KR101242267B1 (en) * 2006-12-06 2013-03-12 (주)엘지하우시스 Constructing member by composite material
RU2623054C1 (en) * 2016-07-15 2017-06-21 Акционерное общество Центральный научно-исследовательский институт специального машиностроения Supporting bend for thin-wall shells from composite materials and method of its manufacture
WO2019159443A1 (en) * 2018-02-13 2019-08-22 三菱重工業株式会社 Method for producing composite material and composite material
US10823494B2 (en) 2016-11-30 2020-11-03 Liebherr-Hausgeräte Ochsenhausen GmbH Refrigerating and/or freezing device

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4962744A (en) * 1988-08-29 1990-10-16 Toyota Jidosha Kabushiki Kaisha Device for detecting malfunction of fuel evaporative purge system
JP4813373B2 (en) * 2004-12-21 2011-11-09 Thk株式会社 Exercise guidance device
WO2006068089A1 (en) * 2004-12-21 2006-06-29 Thk Co., Ltd. Movement guiding device
JPWO2006068089A1 (en) * 2004-12-21 2008-06-12 Thk株式会社 Exercise guidance device
US7845854B2 (en) 2004-12-21 2010-12-07 Thk Co., Ltd. Motion guide device
KR101242267B1 (en) * 2006-12-06 2013-03-12 (주)엘지하우시스 Constructing member by composite material
JP2011520690A (en) * 2008-05-16 2011-07-21 ザ・ボーイング・カンパニー REINFORCED REINFORCEMENT AND METHOD FOR PRODUCING REINFORCED REINFORCEMENT
JP2010163789A (en) * 2009-01-15 2010-07-29 Miyaji Iron Works Co Ltd Inspection passage
JP2010168780A (en) * 2009-01-21 2010-08-05 Miyaji Iron Works Co Ltd Inspection path
RU2623054C1 (en) * 2016-07-15 2017-06-21 Акционерное общество Центральный научно-исследовательский институт специального машиностроения Supporting bend for thin-wall shells from composite materials and method of its manufacture
US10823494B2 (en) 2016-11-30 2020-11-03 Liebherr-Hausgeräte Ochsenhausen GmbH Refrigerating and/or freezing device
WO2019159443A1 (en) * 2018-02-13 2019-08-22 三菱重工業株式会社 Method for producing composite material and composite material
JP2019136970A (en) * 2018-02-13 2019-08-22 三菱重工業株式会社 Method for manufacturing composite material and composite material
US11383460B2 (en) 2018-02-13 2022-07-12 Mitsubishi Heavy Industries, Ltd. Method for producing composite material

Similar Documents

Publication Publication Date Title
JP2017013489A (en) Systems and methods for forming composite materials
JP4977696B2 (en) Reinforcing beam, method for manufacturing the reinforcing beam, and fiber laminate
CN103874629B (en) The compound longeron of bending and the corresponding panel of height convergent
JP5722045B2 (en) Composite parts with curved outer shape
TWI531695B (en) Woven preform, composite, and method of making thereof
JPH05459A (en) Structure component using fiber reinforced resin composite material
TWI526587B (en) Woven preform, composite, and method of making thereof
EP3626603B1 (en) Composite fabric wing spar with interleaved tape cap plies
US20090081400A1 (en) Sandwich Component Assembly with An L-Shaped Or T-Shaped Element, And Method For Production Of Such Assemblies
JPS58118401A (en) Production method of rim made of continuous fiber reinforced plastic
US3780969A (en) Wing case for air foils
JP5875147B2 (en) Composite structure and aircraft fuselage
US10919260B2 (en) Composite structure having a variable gage and methods for forming a composite structure having a variable gage
US11325689B2 (en) Composite stringer and methods for forming a composite stringer
JPS58502048A (en) filament roll container
JP2020001269A (en) Composite material, method for manufacturing composite material, and method for curing composite material
US10913215B2 (en) Composite structure having a variable gage and methods for forming a composite structure having a variable gage
JPH1016072A (en) Manufacture of composite material
JP3413357B2 (en) Golf club shaft
JPH0842060A (en) Concrete reinforcing bar made of frp
US11465655B2 (en) Railcar side wall fabrication and offset overlap welding of sheets
JP2002028944A (en) Method for molding composite material beam
JP3989124B2 (en) Fiber-reinforced composite cross beam with cross-section rib and method of manufacturing the same
JPS63258297A (en) Reinforcing structure of box-shaped structure by composite material
CN216546669U (en) Composite material wing rib and forming die thereof