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JPS6333452B2 - - Google Patents
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JPS6333452B2 - - Google Patents

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Publication number
JPS6333452B2
JPS6333452B2 JP54001235A JP123579A JPS6333452B2 JP S6333452 B2 JPS6333452 B2 JP S6333452B2 JP 54001235 A JP54001235 A JP 54001235A JP 123579 A JP123579 A JP 123579A JP S6333452 B2 JPS6333452 B2 JP S6333452B2
Authority
JP
Japan
Prior art keywords
hollow tube
composite material
fiber
reinforced composite
mandrel
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.)
Expired
Application number
JP54001235A
Other languages
Japanese (ja)
Other versions
JPS5595530A (en
Inventor
Kikuo Tanabe
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.)
Nissan Motor Co Ltd
Original Assignee
Nissan Motor 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 Nissan Motor Co Ltd filed Critical Nissan Motor Co Ltd
Priority to JP123579A priority Critical patent/JPS5595530A/en
Publication of JPS5595530A publication Critical patent/JPS5595530A/en
Publication of JPS6333452B2 publication Critical patent/JPS6333452B2/ja
Granted legal-status Critical Current

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  • Moulding By Coating Moulds (AREA)

Description

【発明の詳細な説明】 本発明は繊維強化複合材料製中空駆動軸の製造
方法に関するものである。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a method for manufacturing a hollow drive shaft made of fiber-reinforced composite material.

繊維強化複合材料(以下FRCMと略称する)
で造つた中空駆動軸は重量が軽く、例えば自動車
のプロペラシヤフトに有効なものとして用いられ
つつある。この場合第1図及び第2図に示すよう
に、FRCM製中空管1の両端内に金属製ジヨイ
ントヨーク2の対応端部を第2図に3で示す如く
嵌合、接着してプロペラシヤフトとなす。ところ
で、中空管1に対するジヨイントヨーク2の結着
強度は、接着面積、すなわち両者の嵌合部3の軸
方向長さにより決定され、この結着強度を伝達ト
ルクに耐えるものにするには嵌合部3の軸方向長
さを相当長くしなければならないのが実情であつ
た。しかし、嵌合部3の長さを長くすると、金属
製ジヨイントヨーク2自体が長大になり、プロペ
ラシヤフトの重量増を招き、その重量軽減のため
にFRCM製中空管1を用いた効果が半減する。
Fiber reinforced composite material (hereinafter abbreviated as FRCM)
Hollow drive shafts made from this material are light in weight and are being used effectively, for example, in automobile propeller shafts. In this case, as shown in Figures 1 and 2, the corresponding ends of the metal joint yoke 2 are fitted and glued into both ends of the FRCM hollow tube 1 as shown at 3 in Figure 2 to form the propeller shaft. Eggplant. By the way, the bonding strength of the joint yoke 2 to the hollow tube 1 is determined by the bonding area, that is, the axial length of the fitting portion 3 of both, and in order to make this bonding strength strong enough to withstand the transmitted torque, the fitting The actual situation is that the axial length of the portion 3 must be made considerably long. However, if the length of the fitting part 3 is increased, the metal joint yoke 2 itself becomes longer and larger, which increases the weight of the propeller shaft, and the effect of using the FRCM hollow tube 1 to reduce the weight is halved. .

そこで、嵌合部3の軸方向長さを長くすること
なしに、上記の結着強度を高める目的から、第3
図及び第4図の如くFRCM製中空管1の端面に
切欠き4を形成し、この切欠き内に侵入する突部
5をヨーク2に設けることが考えられる。これら
切欠き4及び突部5は嵌合部3の接着面と共に、
中空管1及びヨーク2間でトルク伝達機能を果た
し、嵌合部3における接着強度を左程大きくする
必要がなくなり、ヨーク2の長さを短かくでき
る。
Therefore, for the purpose of increasing the bonding strength described above without increasing the axial length of the fitting part 3, a third
It is conceivable to form a notch 4 in the end face of the FRCM hollow tube 1 as shown in FIGS. These notches 4 and protrusions 5 together with the adhesive surface of the fitting part 3,
A torque transmission function is achieved between the hollow tube 1 and the yoke 2, and there is no need to increase the adhesive strength at the fitting part 3, and the length of the yoke 2 can be shortened.

しかるに、中空管1の端面に切欠き4を形成す
るに当り、中空管1の端面を切欠き4の形状に切
除するのでは、中空管1の主構成要素たる繊維6
が第3図及び第5図の如く切欠き4の箇所で切断
されてしまい、中空管1の端面に及ばない。すな
わち、繊維6は、中空管1の端面に点在するに過
ぎない。この場合、中空管1の端部が強度不足を
免れず、この中空管端部とヨーク2との間で切欠
き4及び突部5を介し大きなトルク伝達が行なわ
れることもあつて、中空管1の端部が破壊され易
い。
However, when forming the notch 4 on the end surface of the hollow tube 1, cutting the end surface of the hollow tube 1 into the shape of the notch 4 results in the fibers 6, which are the main components of the hollow tube 1.
is cut off at the notch 4 as shown in FIGS. 3 and 5, and does not reach the end surface of the hollow tube 1. That is, the fibers 6 are only scattered on the end face of the hollow tube 1. In this case, the strength of the end of the hollow tube 1 is inevitably insufficient, and a large torque is transmitted between the end of the hollow tube and the yoke 2 through the notch 4 and the protrusion 5. The end of the hollow tube 1 is easily destroyed.

本発明はかかる観点から、上記端面切欠きにジ
ヨイントヨークの突部を侵入させたFRCM製中
空駆動軸を、中空管の繊維が切欠き部分で切断さ
れることなく、全て中空管端面に緻密に及ぶよう
に製造できる方法を開発したものである。
From this point of view, the present invention provides a hollow drive shaft made of FRCM in which the protrusion of the joint yoke is inserted into the end face notch, so that the fibers of the hollow tube are not cut at the notch, and all of the fibers of the hollow tube are densely attached to the end face of the hollow tube. We have developed a manufacturing method that can cover up to 100%.

以下、図面に基づき本発明の方法を詳細に説明
する。
Hereinafter, the method of the present invention will be explained in detail based on the drawings.

本発明方法の実施に当つては、第6図及び第7
図に示すようにピン7を着脱自在に有するマンド
レル8を用いる。ピン7の数及び位置は、
FRCM製中空管1の端面に形成すべき切欠き4
の数及び位置に対応させ、各ピン7をその取付状
態でマンドレル8から半径方向に突出させる。そ
して、マンドレル8をピン7が取付けられた状態
で、軸線周りに回転させ、この間にマンドレル8
上に、液状の複合材料を通過してこの複合材料を
含浸された繊維6を、マンドレル8の軸方向に往
復動させつつ巻付ける。かかる往復動の幅は第6
図に明示するように、マンドレル8の軸方向に離
間したピン7の間隔を越える幅とする。かように
して繊維6をマンドレル8上に巻付けると、繊維
6は各ピン7を避けて巻付けられ、その分ここで
の巻付繊維が緻密になる。
In carrying out the method of the present invention, FIGS.
As shown in the figure, a mandrel 8 having a detachable pin 7 is used. The number and position of pins 7 are
Notch 4 to be formed on the end face of FRCM hollow tube 1
Each pin 7 projects radially from the mandrel 8 in its attached state, corresponding to the number and position of the pins 7 . Then, the mandrel 8 is rotated around the axis with the pin 7 attached, and during this time the mandrel 8
On the mandrel 8, the fiber 6, which has been passed through the liquid composite material and impregnated with this composite material, is wound while reciprocating in the axial direction of the mandrel 8. The width of this reciprocating motion is the sixth
As clearly shown in the figure, the width is greater than the distance between the axially spaced pins 7 of the mandrel 8. When the fibers 6 are wound on the mandrel 8 in this manner, the fibers 6 are wound avoiding each pin 7, and the wound fibers here become denser accordingly.

その後、この状態で繊維6に含浸された複合材
料の硬化を加熱により促進させて、中空管基材9
を造形する。かように複合材料の硬化で中空管基
材9が造形された後に、ピン7を全てマンドレル
8から引抜き、このマンドレルを中空管基材9か
ら抜取る。中空管基材9からマンドレル8を抜取
る作業を行ない易くするためには、マンドレル8
上に前述の如く繊維6を巻付ける前に、マンドレ
ル8の表面に離型材を塗布しておくのが良い。
Thereafter, in this state, the curing of the composite material impregnated into the fibers 6 is accelerated by heating, and the hollow tube base material 9 is heated.
Model. After the hollow tube base material 9 is shaped by curing the composite material in this manner, all the pins 7 are pulled out from the mandrel 8, and this mandrel is pulled out from the hollow tube base material 9. In order to make it easier to remove the mandrel 8 from the hollow tube base material 9, it is necessary to
It is preferable to apply a release agent to the surface of the mandrel 8 before wrapping the fiber 6 thereon as described above.

マンドレル8を抜取られた中空管基材9はピン
7に対応する箇所にその断面形状と同じ形の孔1
0を有し、この孔10を通る面11内で中空管基
材9を横方向に切断することにより、第8図に示
す如き中空管1を所定長に且つ端面に切欠き4を
持つように製造することができる。
The hollow tube base material 9 from which the mandrel 8 has been removed has a hole 1 having the same cross-sectional shape as the pin 7 at a location corresponding to the pin 7.
0, and by cutting the hollow tube base material 9 in the transverse direction within the plane 11 passing through the hole 10, the hollow tube 1 as shown in FIG. It can be manufactured to have.

かようにして造つた中空管1の端面開口にジヨ
イントヨーク2を、その突部5が第3図及び第4
図の如く切欠き4間に侵入するよう嵌着すること
で、繊維強化複合材料製中空駆動軸を得ることが
できる。
A joint yoke 2 is attached to the end opening of the hollow tube 1 thus manufactured, and its protrusion 5 is shown in FIGS. 3 and 4.
A hollow drive shaft made of fiber-reinforced composite material can be obtained by fitting it into the notches 4 as shown in the figure.

上述の本発明方法により製造した駆動軸によれ
ば、その主構成要素たる中空管1の繊維6が第8
図に示すように、切欠き4の箇所で切断されるこ
となく、全て切欠き4の箇所を迂回して緻密に中
空管1の端面に沿い延在し、端面に切欠き4を有
する中空管1を用いた駆動軸と雖も、中空管1の
端面強度が低下するようなことがなく、駆動軸の
許容伝達トルクを高く保つことができる。
According to the drive shaft manufactured by the method of the present invention described above, the fibers 6 of the hollow tube 1, which is the main component,
As shown in the figure, the hollow tube 1 is not cut at the notch 4, but extends closely along the end surface of the hollow tube 1, bypassing the notch 4, and has the notch 4 on the end surface. Even with the drive shaft using the hollow tube 1, the strength of the end face of the hollow tube 1 does not decrease, and the allowable transmission torque of the drive shaft can be maintained high.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図は繊維強化複合材料製中空管を用いたプ
ロペラシヤフトの側面図、第2図は第1図のA−
A断面図、第3図は第1図に示すプロペラシヤフ
トのジヨイントヨーク結着部に関する改良構造の
側面図、第4図は第3図のB−B断面図、第5図
は第3図及び第4図のプロペラシヤフトに用いる
繊維強化複合材料製中空管の端部を示す斜視図、
第6図は本発明方法による繊維強化複合材料製中
空管の製造途中における状態を示す側面図、第7
図は第6図のC−C断面図、第8図は本発明方法
により製造した繊維強化複合材料製中空管の端部
を示す斜視図である。 1……繊維強化複合材料製中空管、2……ジヨ
イントヨーク、3……ジヨイントヨーク嵌合接着
部、4……切欠き、5……突部、6……繊維、7
……ピン、8……マンドレル、9……繊維強化複
合材料製中空管基材、10……孔、11……切断
面。
Figure 1 is a side view of a propeller shaft using a hollow tube made of fiber-reinforced composite material, and Figure 2 is a side view of the propeller shaft shown in Figure 1.
A sectional view, FIG. 3 is a side view of the improved structure related to the joint yoke connection part of the propeller shaft shown in FIG. 1, FIG. 4 is a BB sectional view of FIG. 3, and FIG. A perspective view showing the end of the fiber-reinforced composite hollow tube used in the propeller shaft shown in FIG. 4;
FIG. 6 is a side view showing the state in the process of manufacturing a hollow tube made of fiber-reinforced composite material by the method of the present invention;
The figure is a sectional view taken along the line CC in FIG. 6, and FIG. 8 is a perspective view showing the end of a hollow tube made of a fiber-reinforced composite material manufactured by the method of the present invention. DESCRIPTION OF SYMBOLS 1...Hollow tube made of fiber reinforced composite material, 2...Joint yoke, 3...Joint yoke fitting adhesive part, 4...Notch, 5...Protrusion, 6...Fiber, 7
... Pin, 8 ... Mandrel, 9 ... Hollow tube base material made of fiber-reinforced composite material, 10 ... Hole, 11 ... Cut surface.

Claims (1)

【特許請求の範囲】 1 繊維強化複合材料製中空管の端面開口にジヨ
イントヨークを嵌着し、該ジヨイントヨークの軸
線方向突部を繊維強化複合材料製中空管の端面に
形成した切欠き内に侵入させた繊維強化複合材料
製中空駆動軸を製造するに際し、 マンドレルにその半径方向へ突出するピンを挿
入した状態でマンドレル上に、複合材料中を通過
した繊維を巻付け、複合材料の硬化による中空管
基材の造形を待つて、前記ピンをマンドレルから
抜き取ると共に、このマンドレルを前記中空管基
材から引抜き、その後この中空管基材を、前記ピ
ンにより形成された孔を通る軸直角面内で横方向
に切断して前記切欠きを端面に有する繊維強化複
合材料製中空管を形成し、該切欠きに前記突部が
侵入するよう前記ジヨイントヨークを繊維強化複
合材料製中空管の端面開口に嵌着することを特徴
とする繊維強化複合材料製中空駆動軸の製造方
法。
[Claims] 1. A joint yoke is fitted into an opening at the end of a hollow tube made of fiber-reinforced composite material, and the axial protrusion of the joint yoke is inserted into a notch formed in the end surface of the hollow tube made of fiber-reinforced composite material. When manufacturing a hollow drive shaft made of a fiber-reinforced composite material, the fibers that have passed through the composite material are wound around the mandrel with pins that protrude in the radial direction inserted into the mandrel, and the fibers that have passed through the composite material are then hardened. Waiting for the formation of the hollow tube base material, the pin is pulled out from the mandrel, the mandrel is pulled out from the hollow tube base material, and then this hollow tube base material is inserted into the shaft passing through the hole formed by the pin. A hollow tube made of fiber-reinforced composite material is formed by cutting transversely within a right-angled plane to form a hollow tube made of fiber-reinforced composite material having the notch on the end surface, and the joint yoke is cut into a hollow tube made of fiber-reinforced composite material such that the protrusion enters the notch. A method for manufacturing a hollow drive shaft made of fiber-reinforced composite material, characterized in that it is fitted into an opening at the end of a pipe.
JP123579A 1979-01-12 1979-01-12 Manufacture for hollow pipe of fiber reinforced composite material with notch at end face Granted JPS5595530A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP123579A JPS5595530A (en) 1979-01-12 1979-01-12 Manufacture for hollow pipe of fiber reinforced composite material with notch at end face

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP123579A JPS5595530A (en) 1979-01-12 1979-01-12 Manufacture for hollow pipe of fiber reinforced composite material with notch at end face

Publications (2)

Publication Number Publication Date
JPS5595530A JPS5595530A (en) 1980-07-19
JPS6333452B2 true JPS6333452B2 (en) 1988-07-05

Family

ID=11495795

Family Applications (1)

Application Number Title Priority Date Filing Date
JP123579A Granted JPS5595530A (en) 1979-01-12 1979-01-12 Manufacture for hollow pipe of fiber reinforced composite material with notch at end face

Country Status (1)

Country Link
JP (1) JPS5595530A (en)

Also Published As

Publication number Publication date
JPS5595530A (en) 1980-07-19

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