JP2000320529A - Propeller shaft - Google Patents

Propeller shaft

Info

Publication number
JP2000320529A
JP2000320529A JP11133190A JP13319099A JP2000320529A JP 2000320529 A JP2000320529 A JP 2000320529A JP 11133190 A JP11133190 A JP 11133190A JP 13319099 A JP13319099 A JP 13319099A JP 2000320529 A JP2000320529 A JP 2000320529A
Authority
JP
Japan
Prior art keywords
rubber elastic
outer member
elastic body
propeller shaft
side member
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
JP11133190A
Other languages
Japanese (ja)
Inventor
Naohito Kuwayama
直仁 桑山
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.)
Sumitomo Riko Co Ltd
Original Assignee
Sumitomo Riko 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 Sumitomo Riko Co Ltd filed Critical Sumitomo Riko Co Ltd
Priority to JP11133190A priority Critical patent/JP2000320529A/en
Publication of JP2000320529A publication Critical patent/JP2000320529A/en
Pending legal-status Critical Current

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  • Motor Power Transmission Devices (AREA)
  • Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)

Abstract

PROBLEM TO BE SOLVED: To provide a propeller shaft which can increase sliding torque, without having an influence to torsional rigidity and characteristic of a rubber elastic unit. SOLUTION: This propeller shaft comprises a cylindrical outer side member 1, connected to a drive system, a cylindrical inner side member 2 arranged in a coaxial state with a distance in an inner side of the outer side member 1 to be connected to a driven system, and a plurality of ring-shaped rubber elastic units 3 interposed in a compressed condition in the diametric direction between an external peripheral surface of the inner side member 2 and an internal peripheral surface of the outer side member 1. A thermosetting bonding agent 4 in an unhardened condition, gradually hardened by heat in the atmosphere of use, is applied to a contact surface of the rubber elastic unit 3 and the outer side member 1.

Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【発明の属する技術分野】本発明は、車両等においてト
ルク伝達に使用される防振性のプロペラシャフトに関す
る。
The present invention relates to a vibration-proof propeller shaft used for transmitting torque in a vehicle or the like.

【0002】[0002]

【従来の技術】従来より、FR車においては、エンジン
の駆動力をリヤ側のデファレンシャルに伝達するトルク
伝達部材としてプロペラシャフトが使用されている。こ
のプロペラシャフトは、筒状の外側部材と、該外側部材
の内側に距離を隔てて同軸状に配置された筒状の内側部
材と、該内側部材の外周面と前記外側部材の内周面との
間に径方向に圧縮された状態で介在し軸方向に沿って配
列された複数のリング状のゴム弾性体とから構成されて
いる。
2. Description of the Related Art Conventionally, in a FR vehicle, a propeller shaft has been used as a torque transmitting member for transmitting a driving force of an engine to a rear differential. The propeller shaft has a cylindrical outer member, a cylindrical inner member disposed coaxially at a distance inside the outer member, an outer peripheral surface of the inner member, and an inner peripheral surface of the outer member. And a plurality of ring-shaped rubber elastic bodies interposed in the state of being compressed in the radial direction and arranged along the axial direction.

【0003】このプロペラシャフトは、通常、内側部材
の外周面に複数のゴム弾性体を加硫接着により固着し、
その内側部材を外側部材の内部に圧入することにより組
付けられる。そして、外側部材の一端をエンジン(駆動
系)側及びデファレンシャル(従動系)側のいずれか一
方に連結するとともに、内側部材の一端をエンジン側及
びデファレンシャル側のいずれか他方に連結することに
より実車に取付けられる。これにより、外側部材と内側
部材との間に設けられたゴム弾性体を介して、エンジン
からデファレンシャルへと回転トルクの伝達が行われ
る。なお、外側部材と内側部材との間に介装されたゴム
弾性体は、ノイズ振動を低減させるために捩じり剛性の
低減を目的として設けられている。
This propeller shaft usually has a plurality of rubber elastic bodies fixed to the outer peripheral surface of the inner member by vulcanization bonding.
It is assembled by press-fitting the inner member into the outer member. Then, one end of the outer member is connected to one of the engine (drive system) side and the differential (driven system) side, and one end of the inner member is connected to the other one of the engine side and the differential side. Mounted. Thus, the rotation torque is transmitted from the engine to the differential via the rubber elastic body provided between the outer member and the inner member. The rubber elastic body interposed between the outer member and the inner member is provided for the purpose of reducing torsional rigidity in order to reduce noise vibration.

【0004】[0004]

【発明が解決しようとする課題】ところで、近年におい
ては、エンジントルクの上昇や駆動系全体の雰囲気温度
の上昇が進んでおり、これに伴い、プロペラシャフトの
滑りトルクの向上も必要となっている。この場合、初期
の滑りトルクのみではなく、使用時の雰囲気温度の上昇
に起因するゴム弾性体の老化へたり後の滑りトルクの向
上も要求されるため、より厳しい条件となる。
In recent years, however, the engine torque and the ambient temperature of the entire drive system have been increasing, and accordingly, it is necessary to improve the sliding torque of the propeller shaft. . In this case, not only the initial sliding torque but also the improvement of the aging of the rubber elastic body due to the rise of the ambient temperature during use or the improvement of the sliding torque after the use are required, so that more severe conditions are required.

【0005】この要求に対して、従来では、軸方向に配
列されるゴム弾性体の個数を増やし、ゴム弾性体と内側
部材及び外側部材との接触面積を増大させることにより
滑りトルクの向上に対処していた。例えば、エンジント
ルクが20%上昇した場合には、5個であったゴム弾性
体を6個に増やすことにより対処するものである。しか
し、この場合には、重量やコストの上昇を伴うという不
具合が生じるばかりでなく、捩じり剛性も高くなってし
まうため、ノイズ振動の低減を図るように構成されるプ
ロペラシャフトにとって問題となる場合が多い。
In response to this demand, conventionally, the number of rubber elastic bodies arranged in the axial direction has been increased, and the contact area between the rubber elastic bodies and the inner and outer members has been increased to cope with the improvement of the sliding torque. Was. For example, when the engine torque increases by 20%, the number of rubber elastic bodies is increased from five to six. However, in this case, not only the problem of increasing the weight and cost is caused but also the torsional rigidity is increased, which is a problem for a propeller shaft configured to reduce noise vibration. Often.

【0006】また、ゴム弾性体と内側部材或いは外側部
材との接触面を後加温接着剤により接着することによっ
て、滑りトルクの向上を図ることも可能である。しか
し、この場合には、捩じり剛性の上昇はないものの、後
加温接着処理を施すために大掛かりな設備等が必要とな
るためコスト上昇を招くこととなり、しかも、加硫済み
ゴム弾性体に熱負荷が加えられるためゴム弾性体の物性
が変化しやすいという問題もある。
[0006] Further, it is possible to improve the sliding torque by bonding the contact surface between the rubber elastic body and the inner member or the outer member with a post-heating adhesive. However, in this case, although there is no increase in torsional rigidity, a large-scale facility or the like is required for performing the post-heating bonding treatment, which leads to an increase in cost, and furthermore, a vulcanized rubber elastic body. There is also a problem that the physical properties of the rubber elastic body are liable to change because a thermal load is applied to the rubber.

【0007】本発明は上記問題に鑑み案出されたもので
あり、捩じり剛性やゴム弾性体の特性に影響を与えるこ
となく、滑りトルクの向上を図ることができるプロペラ
シャフトを提供することを解決すべき課題とするもので
ある。
The present invention has been devised in view of the above problems, and provides a propeller shaft capable of improving a sliding torque without affecting the torsional rigidity and the characteristics of a rubber elastic body. Should be solved.

【0008】[0008]

【課題を解決するための手段】上記課題を解決する請求
項1記載の発明に係るプロペラシャフトは、駆動系及び
従動系のいずれか一方に連結される筒状の外側部材と、
該外側部材の内側に距離を隔てて同軸状に配置され前記
駆動系及び前記従動系のいずれか他方に連結される筒状
の内側部材と、該内側部材の外周面と前記外側部材の内
周面との間に径方向に圧縮された状態で介在するリング
状のゴム弾性体と、を備え、該ゴム弾性体と前記外側部
材との接触面に、使用雰囲気中の熱により硬化が徐々に
進行する未硬化状態の熱硬化性接着剤が塗布されている
という手段を採用している。
According to a first aspect of the present invention, there is provided a propeller shaft having a tubular outer member connected to one of a driving system and a driven system;
A cylindrical inner member disposed coaxially at a distance inside the outer member and connected to one of the drive system and the driven system; an outer peripheral surface of the inner member and an inner periphery of the outer member; And a ring-shaped rubber elastic body interposed in a state of being compressed in the radial direction between the rubber member and the outer member.The contact surface between the rubber elastic body and the outer member is gradually cured by heat in a use atmosphere. Means is employed in which a thermosetting adhesive in an uncured state is applied.

【0009】この手段によれば、プロペラシャフトが実
車に取付けられ、高温となる使用雰囲気中に晒される
と、ゴム弾性体と外側部材との接触面に塗布された未硬
化状態の熱硬化性接着剤は、使用雰囲気中の熱に加熱さ
れることにより長期にわたって硬化が徐々に進行し、そ
の接着力が徐々に増強される。これにより、使用雰囲気
での熱負荷によるゴム弾性体の老化へたりに伴う滑りト
ルクの低下が補われ、初期段階の高レベルの滑りトルク
が長期にわたって維持される。
According to this means, when the propeller shaft is mounted on an actual vehicle and exposed to a high-temperature use atmosphere, the uncured thermosetting adhesive applied to the contact surface between the rubber elastic body and the outer member. When the agent is heated by the heat in the use atmosphere, the curing gradually progresses over a long period of time, and the adhesive force is gradually enhanced. This compensates for the decrease in the sliding torque due to the aging of the rubber elastic body due to the thermal load in the use atmosphere, and maintains the high level of the initial stage sliding torque for a long time.

【0010】また、本発明の熱硬化性接着剤は、使用雰
囲気中の熱を利用して硬化が徐々に進行するようにして
いるため、塗布された後の少なくとも車両等に組付けら
れて使用されるまでは未硬化状態のままとされ、加熱処
理等を施す必要がない。そのため、ゴム弾性体の特性に
影響を与えることはない。したがって、本発明のプロペ
ラシャフトによれば、捩じり剛性やゴム弾性体の特性に
影響を与えることなく、滑りトルクの向上を図ることが
できる。
Further, the thermosetting adhesive of the present invention uses the heat in the use atmosphere so that the curing progresses gradually. Therefore, the thermosetting adhesive is used after being applied to at least a vehicle or the like after being applied. Until the heat treatment is completed, it is not necessary to perform a heat treatment or the like. Therefore, it does not affect the characteristics of the rubber elastic body. Therefore, according to the propeller shaft of the present invention, the sliding torque can be improved without affecting the torsional rigidity and the characteristics of the rubber elastic body.

【0011】なお、本発明における熱硬化性接着剤は、
ゴム弾性体と外側部材との接触面に塗布され、加熱処理
等が施されずに未硬化状態のままにされる。この熱硬化
性接着剤は、そのプロペラシャフトが実車で使用される
際に、ゴム弾性体の老化へたりの進行に応じて、使用雰
囲気中の熱により硬化が徐々に進行し、その接着力が長
期にわたって徐々に増強されるものが選択される。ま
た、硬化速度がより遅い熱硬化性接着剤を用いることも
有効となる。このような熱硬化性接着剤としては、その
熱硬化性接着剤が塗布されるべきゴム弾性体や外側部材
との相性等をも考慮すれば、例えば、塩化ゴム系接着剤
を好適に採用することができる。
The thermosetting adhesive according to the present invention comprises:
It is applied to the contact surface between the rubber elastic body and the outer member, and is left uncured without being subjected to heat treatment or the like. When the propeller shaft is used in an actual vehicle, the thermosetting adhesive gradually cures due to the heat in the use atmosphere as the rubber elastic body progresses to aging, and the adhesive force is reduced. Those that gradually increase over time are selected. It is also effective to use a thermosetting adhesive having a lower curing speed. As such a thermosetting adhesive, for example, in consideration of compatibility with a rubber elastic body or an outer member to which the thermosetting adhesive is to be applied, for example, a chlorinated rubber-based adhesive is preferably used. be able to.

【0012】また、本発明において、内側部材と外側部
材との間に介在するゴム弾性体は、径方向に圧縮された
状態にされている。このゴム弾性体の圧縮は、例えば、
ゴム弾性体が固着された内側部材を外側部材の内部に圧
入して組付けたり、或いは、ゴム弾性体が固着された内
側部材2を外側部材1の内周面との間に空隙が形成され
るように嵌挿し、外側部材1を求心方向に絞るか又は内
側部材2を遠心方向に膨出させて組付けたりする方法を
採用することができる。
In the present invention, the rubber elastic body interposed between the inner member and the outer member is in a state of being compressed in the radial direction. The compression of this rubber elastic body is, for example,
The inner member to which the rubber elastic body is fixed is press-fitted into the outer member and assembled, or a gap is formed between the inner member 2 to which the rubber elastic member is fixed and the inner peripheral surface of the outer member 1. And the outer member 1 is squeezed in the centripetal direction, or the inner member 2 is bulged in the centrifugal direction and assembled.

【0013】[0013]

【発明の実施の形態】以下、本発明の実施形態を図面に
基づき説明する。図1は本実施形態に係るプロペラシャ
フトの一部を断面で示す正面図である。本実施形態のプ
ロペラシャフトは、図1に示すように、筒状の外側部材
1と、外側部材1の内側に距離を隔てて同軸状に配置さ
れた内側部材2と、内側部材2の外周面と外側部材1の
内周面との間に径方向に圧縮された状態で介在するリン
グ状の5個のゴム弾性体3と、ゴム弾性体3と外側部材
1との接触面に塗布された未硬化状態の熱硬化性接着剤
4と、から構成されている。
Embodiments of the present invention will be described below with reference to the drawings. FIG. 1 is a front view showing a cross section of a part of the propeller shaft according to the present embodiment. As shown in FIG. 1, the propeller shaft according to the present embodiment includes a cylindrical outer member 1, an inner member 2 coaxially arranged inside the outer member 1 at a distance, and an outer peripheral surface of the inner member 2. The ring-shaped five rubber elastic bodies 3 interposed in a radially compressed state between the rubber elastic body 3 and the inner peripheral surface of the outer member 1, and are applied to a contact surface between the rubber elastic body 3 and the outer member 1. And an uncured thermosetting adhesive 4.

【0014】外側部材1は、金属により一端が開口する
円筒状に形成されている。この外側部材1の閉口側に
は、軸方向外方に二股状に延出する連結部11が設けら
れており、この連結部11が駆動系及び従動系のいずれ
か一方に固定される連結部材13に連結されている。内
側部材2は、金属により一端が開口する円筒チューブ状
に形成されている。この内側部材2は、外側部材1の内
径よりも所定寸法小さい外径を有し、外側部材1の内側
に距離を隔てて同軸状に配置されている。この内側部材
2の閉口側には、軸方向外方に二股状に延出する連結部
21が設けられており、この連結部21が駆動系及び従
動系のいずれか他方に固定される連結部材23に連結さ
れている。
The outer member 1 is formed in a cylindrical shape having one end opened by metal. On the closing side of the outer member 1, there is provided a connecting portion 11 extending bifurcated outward in the axial direction, and the connecting portion 11 is fixed to one of a driving system and a driven system. 13. The inner member 2 is formed of a metal into a cylindrical tube shape having one end opened. The inner member 2 has an outer diameter smaller than the inner diameter of the outer member 1 by a predetermined dimension, and is coaxially arranged inside the outer member 1 at a distance. On the closing side of the inner member 2, there is provided a connecting portion 21 extending bifurcated outward in the axial direction, and the connecting portion 21 is fixed to one of the driving system and the driven system. 23.

【0015】ゴム弾性体3は、ゴム材料を加硫成形する
ことによりリング状に形成されている。このゴム弾性体
3は、その内周面が内側部材2の外周面に加硫接着さ
れ、5個のゴム弾性体3が軸方向に沿って所定の間隔で
配置されている。これらゴム弾性体3が加硫接着された
内側部材2を外側部材1の内部に圧入して組付けること
により、内側部材2の外周面と外側部材1の内周面との
間に径方向に圧縮された状態で介在されている。これら
ゴム弾性体3が所定量圧縮されていることにより、適度
な捩じり剛性及び滑りトルクが付与されている。
The rubber elastic body 3 is formed in a ring shape by vulcanizing a rubber material. The rubber elastic body 3 has its inner peripheral surface vulcanized and bonded to the outer peripheral surface of the inner member 2, and five rubber elastic bodies 3 are arranged at predetermined intervals along the axial direction. By press-fitting and assembling the inner member 2 to which the rubber elastic body 3 is vulcanized and bonded into the inside of the outer member 1, a radial direction is formed between the outer peripheral surface of the inner member 2 and the inner peripheral surface of the outer member 1. It is interposed in a compressed state. By compressing the rubber elastic body 3 by a predetermined amount, an appropriate torsional stiffness and sliding torque are given.

【0016】熱硬化性接着剤4は、ゴム弾性体3と外側
部材1との接触面に塗布されており未硬化状態のもので
ある。この熱硬化性接着剤4は、各ゴム弾性体3が加硫
接着された内側部材2を外側部材1の内部に圧入して組
付ける前に、各ゴム弾性体3の外周面に塗布されてい
る。本実施形態では、熱硬化性接着剤4として、塩化ゴ
ム系接着剤(商品名「ケムロック220」「ケムロック
252」(ロードコーポレーション社製))が用いられ
ている。なお、熱硬化性接着剤4が塗布された各ゴム弾
性体3の外周面には、外側部材1への内側部材2の圧入
が円滑になるように、必要に応じて圧入液(例えば、石
鹸水やオイル等)が塗布される。
The thermosetting adhesive 4 is applied to the contact surface between the rubber elastic body 3 and the outer member 1 and is in an uncured state. This thermosetting adhesive 4 is applied to the outer peripheral surface of each rubber elastic body 3 before the inner member 2 to which each rubber elastic body 3 is vulcanized and bonded is pressed into the inside of the outer member 1 and assembled. I have. In the present embodiment, a chlorinated rubber-based adhesive (trade names “Chemlock 220” and “Chemlock 252” (manufactured by Road Corporation)) is used as the thermosetting adhesive 4. A press-fitting liquid (for example, a soap) is provided on the outer peripheral surface of each rubber elastic body 3 coated with the thermosetting adhesive 4 so that the inner member 2 can be pressed into the outer member 1 smoothly. Water or oil) is applied.

【0017】以上のように構成された本実施形態のプロ
ペラシャフトは、外側部材1の連結部11が連結部材1
3を介してエンジン側に連結されるとともに、内側部材
2の連結部21が連結部材23を介してデファレンシャ
ル側に連結されることにより実車に取付けられる。これ
により、外側部材1と内側部材2との間に設けられたゴ
ム弾性体3を介して、エンジンからデファレンシャルへ
と回転トルクの伝達が行われる。
In the propeller shaft of this embodiment configured as described above, the connecting portion 11 of the outer member 1
3 and connected to the engine side, and the connecting portion 21 of the inner member 2 is connected to the differential side via a connecting member 23 to be mounted on the actual vehicle. As a result, the rotation torque is transmitted from the engine to the differential via the rubber elastic body 3 provided between the outer member 1 and the inner member 2.

【0018】そして、このプロペラシャフトが高温とな
る使用雰囲気中に晒されると、熱負荷によるゴム弾性体
3の老化へたりによって滑りトルクが徐々に低下する。
しかし、ゴム弾性体3と外側部材1との接触面に塗布さ
れた未硬化状態の熱硬化性接着剤4は、使用雰囲気中の
熱に繰り返し加熱されることにより、硬化が急激に進行
することなく長期にわたって徐々に進行し、その接着力
が徐々に増強される。これにより、ゴム弾性体3の老化
へたりに伴う滑りトルクの低下が補われ、初期段階の高
レベルの滑りトルクが長期にわたって維持される。
When the propeller shaft is exposed to a high-temperature use atmosphere, the sliding torque gradually decreases due to the aging of the rubber elastic body 3 due to a thermal load.
However, the thermosetting adhesive 4 in the uncured state applied to the contact surface between the rubber elastic body 3 and the outer member 1 rapidly cures due to repeated heating by the heat in the use atmosphere. Progresses gradually over a long period of time, and the adhesive strength gradually increases. As a result, a decrease in the sliding torque due to the aging of the rubber elastic body 3 is compensated, and a high level of the initial stage sliding torque is maintained for a long time.

【0019】以上のように、本実施形態のプロペラシャ
フトによれば、ゴム弾性体3と外側部材1との接触面
に、使用雰囲気中の熱により硬化が徐々に進行する未硬
化状態の熱硬化性接着剤4が塗布されているため、滑り
トルクの向上を図ることができる。また、この熱硬化性
接着剤4は、塗布された後には未硬化状態のままとさ
れ、加熱処理等を施す必要がないため、ゴム弾性体3の
特性に影響を与えることがなく、プロペラシャフトの機
能品質の安定化を図ることができる。
As described above, according to the propeller shaft of the present embodiment, the uncured thermosetting in which the curing gradually progresses due to the heat in the use atmosphere is applied to the contact surface between the rubber elastic body 3 and the outer member 1. Since the adhesive 4 is applied, the slip torque can be improved. Further, since the thermosetting adhesive 4 is left in an uncured state after being applied and does not need to be subjected to heat treatment or the like, the properties of the rubber elastic body 3 are not affected, and the propeller shaft is not affected. Function quality can be stabilized.

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

【図1】本発明の実施形態に係るプロペラシャフトの一
部を断面で示す正面図である。
FIG. 1 is a front view showing a cross section of a part of a propeller shaft according to an embodiment of the present invention.

【符号の説明】 1…外側部材 2…内側部材 3…ゴム弾性体 4…熱硬化性接着剤 11、21…連結部 13、23…連結部材[Description of Signs] 1 ... outer member 2 ... inner member 3 ... rubber elastic member 4 ... thermosetting adhesive 11,21 ... connecting portion 13,23 ... connecting member

Claims (2)

【特許請求の範囲】[Claims] 【請求項1】 駆動系及び従動系のいずれか一方に連結
される筒状の外側部材と、 該外側部材の内側に距離を隔てて同軸状に配置され前記
駆動系及び前記従動系のいずれか他方に連結される筒状
の内側部材と、 該内側部材の外周面と前記外側部材の内周面との間に径
方向に圧縮された状態で介在するリング状のゴム弾性体
と、を備え、 該ゴム弾性体と前記外側部材との接触面に、使用雰囲気
中の熱により硬化が徐々に進行する未硬化状態の熱硬化
性接着剤が塗布されていることを特徴とするプロペラシ
ャフト。
1. A cylindrical outer member connected to one of a driving system and a driven system, and one of the driving system and the driven system disposed coaxially at a distance inside the outer member. A cylindrical inner member connected to the other, and a ring-shaped rubber elastic body interposed in a radially compressed state between an outer peripheral surface of the inner member and an inner peripheral surface of the outer member. A propeller shaft, wherein an uncured thermosetting adhesive whose curing gradually progresses due to heat in a use atmosphere is applied to a contact surface between the rubber elastic body and the outer member.
【請求項2】 前記熱硬化性接着剤は、塩化ゴム系接着
剤であることを特徴とする請求項1記載のプロペラシャ
フト。
2. The propeller shaft according to claim 1, wherein the thermosetting adhesive is a chlorinated rubber-based adhesive.
JP11133190A 1999-05-13 1999-05-13 Propeller shaft Pending JP2000320529A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP11133190A JP2000320529A (en) 1999-05-13 1999-05-13 Propeller shaft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP11133190A JP2000320529A (en) 1999-05-13 1999-05-13 Propeller shaft

Publications (1)

Publication Number Publication Date
JP2000320529A true JP2000320529A (en) 2000-11-24

Family

ID=15098816

Family Applications (1)

Application Number Title Priority Date Filing Date
JP11133190A Pending JP2000320529A (en) 1999-05-13 1999-05-13 Propeller shaft

Country Status (1)

Country Link
JP (1) JP2000320529A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6883653B2 (en) 2002-05-27 2005-04-26 Tokai Rubber Industries, Ltd. Dynamic damper
JP2011073525A (en) * 2009-09-29 2011-04-14 Yamada Seisakusho Co Ltd Unbalance correction device of propeller shaft
CN106402179A (en) * 2015-07-28 2017-02-15 长城汽车股份有限公司 Transmission shaft and vehicle with same
WO2018043248A1 (en) * 2016-09-05 2018-03-08 日本発條株式会社 Stabilizer manufacturing method, and joint structure for stabilizer link
WO2022105363A1 (en) * 2020-11-20 2022-05-27 上海纳铁福传动系统有限公司 Shaft tube joint structure of drive shaft

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6883653B2 (en) 2002-05-27 2005-04-26 Tokai Rubber Industries, Ltd. Dynamic damper
JP2011073525A (en) * 2009-09-29 2011-04-14 Yamada Seisakusho Co Ltd Unbalance correction device of propeller shaft
CN106402179A (en) * 2015-07-28 2017-02-15 长城汽车股份有限公司 Transmission shaft and vehicle with same
WO2018043248A1 (en) * 2016-09-05 2018-03-08 日本発條株式会社 Stabilizer manufacturing method, and joint structure for stabilizer link
JPWO2018043248A1 (en) * 2016-09-05 2019-06-24 日本発條株式会社 Method of manufacturing stabilizer, and joint structure of stabilizer link
WO2022105363A1 (en) * 2020-11-20 2022-05-27 上海纳铁福传动系统有限公司 Shaft tube joint structure of drive shaft
US11940019B2 (en) 2020-11-20 2024-03-26 Shanghai Gkn Huayu Driveline Systems Company Limited Shaft tube joint structure of drive shaft

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