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JPH06227274A - Propeller shaft - Google Patents

Propeller shaft

Info

Publication number
JPH06227274A
JPH06227274A JP3460693A JP3460693A JPH06227274A JP H06227274 A JPH06227274 A JP H06227274A JP 3460693 A JP3460693 A JP 3460693A JP 3460693 A JP3460693 A JP 3460693A JP H06227274 A JPH06227274 A JP H06227274A
Authority
JP
Japan
Prior art keywords
flange
yoke
joint
bolt mounting
propeller shaft
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
JP3460693A
Other languages
Japanese (ja)
Inventor
Atsushi Hirokawa
淳 広川
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.)
Suzuki Motor Corp
Original Assignee
Suzuki Motor Corp
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 Suzuki Motor Corp filed Critical Suzuki Motor Corp
Priority to JP3460693A priority Critical patent/JPH06227274A/en
Publication of JPH06227274A publication Critical patent/JPH06227274A/en
Pending legal-status Critical Current

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

Abstract

PURPOSE:To decrease surface deflection of a connection flange relative to the shaft body and decrease vibration of a propeller shaft by forming a surface deflection correcting means from detention holes between flange side bolt mounting parts in the connection flange and a protruding member which protrudes from the detention hole to the yoke plane part of a joint yoke. CONSTITUTION:A surface deflection correcting means 38 is formed from detention holes 34-1 thru 34-4 formed between flange bolt mounting holes 30-1 thru 30-4 provided in a connection flange 10 and a protruding member 36 which is in engagement so that it protrudes from the detention holes 34-1 thru 34-4 to the yoke plane 24 of a joint yoke 14. In this surface deflection correcting means 38, the protruding member 36 in screw engagement with the detention hole formed on the L1 side having smaller thickness is protruded to the yoke plane 24 side in an amount corresponding to the difference in the thickness so that the surface deflection of the connection flange 10 relative to the shaft body 4 is decreased when the flange plane 28 on the connection flange 10 has had different thickness between the width L1 on one side and the width L2 on the other side owing to tolerance or deflection generated under machining.

Description

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

【0001】[0001]

【産業上の利用分野】この発明は、プロペラシャフトに
係り、特に一端部位を駆動力発生手段に連結するととも
に他端部位に取り付けた自在継手のジョイントヨークに
動力伝達機に取り付けた接続用フランジを接合し、前記
接続用フランジの複数のフランジ側ボルト取付部と前記
ジョイントヨークの複数のヨーク側ボルト取付部とに接
続用ボルトを取り付けて他端部位を前記動力伝達機に連
結させたプロペラシャフトに関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a propeller shaft, and more particularly to a joint yoke of a universal joint having one end portion connected to a driving force generating means and the other end portion provided with a connection flange attached to a power transmission device. The present invention relates to a propeller shaft in which connecting bolts are joined to a plurality of flange side bolt mounting portions of the connecting flange and a plurality of yoke side bolt mounting portions of the joint yoke, and the other end portion is connected to the power transmission. .

【0002】[0002]

【従来の技術】車両においては、図5に示す如く、内燃
機関の動力を一の動力伝達機である変速機(図示せず)
からプロペラシャフト102を介して他の動力伝達機で
ある差動機106に伝達し、車輪軸に取り付けた後車輪
を回転させる動力伝達系が備えられている。
2. Description of the Related Art In a vehicle, as shown in FIG. 5, a power transmission (not shown), which is one power transmission unit for transmitting power of an internal combustion engine.
Is provided to the differential gear 106, which is another power transmission device, via the propeller shaft 102, and the power transmission system for rotating the rear wheels attached to the wheel shaft is provided.

【0003】プロペラシャフト102は、自在継手10
8及び接続用フランジ110を介して差動機106に連
結されている。自在継手108は、シャフト本体104
の端部に固定されたシャフトヨーク112とジョイント
ヨーク114とがスパイダ116によって結合して構成
されている。接続用フランジ110は、差動機106の
差動機ケース118に固設されている。
The propeller shaft 102 has a universal joint 10
8 and the connection flange 110, and is connected to the differential gear 106. The universal joint 108 is the shaft body 104.
A shaft yoke 112 and a joint yoke 114, which are fixed to the end portion of, are connected by a spider 116. The connection flange 110 is fixed to the differential case 118 of the differential 106.

【0004】ジョイントヨーク114と接続用フランジ
110とは、図示しないジョイントインロー部とフラン
ジインロー部とが嵌合しつつ接合されている。
The joint yoke 114 and the connecting flange 110 are joined together while a joint spigot portion and a flange spigot portion (not shown) are fitted.

【0005】このようなプロペラシャフト102の動力
伝達系において、プロペラシャフト102のアンバラン
スに起因する車体振動及びこもり音を低減させるため
に、プロペラシャフト102側のアンバランス量の最大
方向と、接続用フランジ110側のインロー部位の心ず
れの最小方向とをできるだけ近づけて組付けることによ
り、プロペラシャフト102のアンバランスを打消そう
とする方法が知られている。
In such a power transmission system of the propeller shaft 102, in order to reduce body vibration and muffled noise caused by the imbalance of the propeller shaft 102, the maximum direction of the unbalance amount on the propeller shaft 102 side and the connecting direction are used. A method is known in which an imbalance of the propeller shaft 102 is canceled by assembling as close as possible to the minimum direction of misalignment of the spigot portion on the flange 110 side.

【0006】また、プロペラシャフトとしては、例え
ば、実公平2−2085号公報に開示されている。この
公報に記載のものは、第1シャフト後端にフランジ部材
をスプライン結合し、該フランジ部材と第2ジョイント
間にて第1シャフトを車体に回転自在に支持するととも
に、第3シャフト前端にフランジ部材をスプライン結合
し、該フランジ部材と第3ジョイント間にて第3シャフ
トを車体に回転自在に支持し、更に第2シャフトの前後
端にフランジ部を夫々形成し、該フランジ部をフランジ
部材に夫々ボルト結合することにより、第2シャフトの
交換を容易とし、組付後の誤差補正も第2シャフト部で
簡単に行わせ、メンテナンス作業、組付作業の簡単化を
図るものである。
A propeller shaft is disclosed, for example, in Japanese Utility Model Publication No. 2-2085. In the one disclosed in this publication, a flange member is spline-coupled to the rear end of the first shaft, the first shaft is rotatably supported by the vehicle body between the flange member and the second joint, and a flange is attached to the front end of the third shaft. The members are spline-joined, the third shaft is rotatably supported by the vehicle body between the flange member and the third joint, and further flange portions are formed at the front and rear ends of the second shaft, and the flange portions are used as the flange member. The bolts are connected to each other to facilitate the replacement of the second shaft and to easily perform the error correction after the assembling on the second shaft portion, thereby simplifying the maintenance work and the assembling work.

【0007】[0007]

【発明が解決しようとする課題】ところが、例えば、上
述した自在継手を取り付けたプロペラシャフトにおいて
は、ジョイントヨーク114のヨーク平面部124と接
続用フランジ110のフランジ平面部128との結合時
に、図5に示す如く、面振れが無い場合は、前記プロペ
ラシャフト102の振動が発生しない。
However, for example, in the propeller shaft to which the universal joint is attached as described above, when the yoke flat surface portion 124 of the joint yoke 114 and the flange flat surface portion 128 of the connecting flange 110 are coupled to each other, as shown in FIG. As shown in FIG. 7, when there is no surface wobbling, the propeller shaft 102 does not vibrate.

【0008】しかし、前記ジョイントヨーク114のヨ
ーク平面部124と前記接続用フランジ110のフラン
ジ平面部128との結合時に、図6に示す如く、面振れ
が有る場合は、前記プロペラシャフト102が大きく振
れ回ってしまい、振動が発生し、実用上不利であるとい
う不都合があった。
However, when the yoke flat surface portion 124 of the joint yoke 114 and the flange flat surface portion 128 of the connecting flange 110 are coupled with each other, as shown in FIG. 6, when there is surface wobbling, the propeller shaft 102 largely wobbles. There was a disadvantage that it was turned around and vibration was generated, which was disadvantageous in practical use.

【0009】前記ジョイントヨーク114のヨーク平面
部124と前記接続用フランジ110のフランジ平面部
128との面振れは、機械加工時の公差や振れによって
発生するので、この面振れによるプロペラシャフト10
2の振れも完全に消すことができなかった。
A surface runout between the yoke flat surface portion 124 of the joint yoke 114 and the flange flat surface portion 128 of the connecting flange 110 is caused by a tolerance or a runout during machining. Therefore, the surface runout causes the propeller shaft 10 to move.
The shake of 2 could not be completely eliminated.

【0010】[0010]

【課題を解決するための手段】そこで、この発明は、上
述の不都合を除去するために、一端部位を駆動力発生手
段に連結するとともに他端部位に取り付けた自在継手の
ジョイントヨークに動力伝達機に取り付けた接続用フラ
ンジを接合し、前記接続用フランジの複数のフランジ側
ボルト取付部と前記ジョイントヨークの複数のヨーク側
ボルト取付部とに接続用ボルトを取り付けて他端部位を
前記動力伝達機に連結させたプロペラシャフトにおい
て、前記接続用フランジに設けられた各フランジ側ボル
ト取付部間に形成した係合孔部と、この係合孔部から前
記ジョイントヨークのヨーク平面部位に少許突出すべく
係合する突出部材とにより前記接続用フランジと前記シ
ャフト本体との面振れを減少させる面振れ修正手段を設
けたことを特徴とする。
Therefore, in order to eliminate the above-mentioned inconvenience, the present invention uses a joint transmission yoke in a universal joint having one end portion connected to a driving force generating means and the other end portion. The connection flanges attached to the joint flanges are joined together, connection bolts are attached to the flange side bolt attachment portions of the connection flange and the yoke side bolt attachment portions of the joint yoke, and the other end portion is attached to the power transmission device. In the propeller shaft connected to, the engaging hole portion formed between the flange side bolt mounting portions provided on the connecting flange, and a small amount of protrusion from the engaging hole portion to the yoke plane portion of the joint yoke. A surface wobbling correction means for reducing the surface wobbling between the connecting flange and the shaft body by the engaging protruding member is provided. .

【0011】[0011]

【作用】上述の如く発明したことにより、駆動力発生手
段と動力伝達機とをプロペラシャフトによって連結する
際には、プロペラシャフトの他端部位に取り付けた自在
継手のジョイントヨークに動力伝達機に取り付けた接続
用フランジを接合し、この接続用フランジに設けられた
各フランジ側ボルト取付部間に形成した係合孔部から突
出部材をジョイントヨークのヨーク平面部位に少許突出
すべく係合させ、その後に前記接続用フランジの複数の
フランジ側ボルト取付部と前記ジョイントヨークの複数
のヨーク側ボルト取付部とに接続用ボルトを取り付け、
前記係合孔部と前記突出部材とからなる修正手段によっ
て前記接続用フランジと前記シャフト本体との面振れを
減少させている。
According to the invention as described above, when the driving force generating means and the power transmission are connected by the propeller shaft, the joint yoke of the universal joint attached to the other end of the propeller shaft is attached to the power transmission. The connecting flanges are joined together, and the projecting member is engaged with the yoke plane portion of the joint yoke so as to slightly project from the engaging holes formed between the flange-side bolt mounting portions provided on the connecting flanges, and thereafter. Attaching connection bolts to a plurality of flange side bolt mounting portions of the connecting flange and a plurality of yoke side bolt mounting portions of the joint yoke,
The surface deflection between the connection flange and the shaft body is reduced by the correction means including the engagement hole and the protruding member.

【0012】[0012]

【実施例】以下図面に基づいてこの発明の実施例を詳細
に説明する。
Embodiments of the present invention will be described in detail below with reference to the drawings.

【0013】図1〜図4は、この発明の実施例を示すも
のである。図4において、2はプロペラシャフト、4は
シャフト本体、6は動力伝達機である、例えば後側の差
動機である。前記プロペラシャフト2は、駆動力発生手
段たる内燃機関(図示せず)からの動力を他の動力伝達
機である前記差動機6に伝達するものであり、自在継手
8及び接続用フランジ10によって差動機6に連結され
ている。
1 to 4 show an embodiment of the present invention. In FIG. 4, 2 is a propeller shaft, 4 is a shaft main body, and 6 is a power transmission device, for example, a rear differential gear. The propeller shaft 2 is for transmitting power from an internal combustion engine (not shown), which is a driving force generating means, to the differential gear 6 which is another power transmitter, and is connected by a universal joint 8 and a connecting flange 10. It is linked to motive 6.

【0014】自在継手8は、シャフト本体4の他端部に
固定されたシフトヨーク12とジョイントヨーク14と
がスパイダ16によって結合して構成されている。
The universal joint 8 is constructed by connecting a shift yoke 12 fixed to the other end of the shaft body 4 and a joint yoke 14 with a spider 16.

【0015】接続用フランジ10は、差動機6の差動機
ケース18に固設されている。
The connecting flange 10 is fixed to the differential case 18 of the differential 6.

【0016】ジョイントヨーク14と接続用フランジ1
0とは、図1に示す如く、ジョイントインロー部20と
フランジインロー部22とが嵌合しつつ接合されてい
る。
The joint yoke 14 and the connecting flange 1
As shown in FIG. 1, the joint spigot portion 20 and the flange spigot portion 22 are fitted and joined together as shown in FIG.

【0017】前記ジョイントヨーク14のヨーク平面部
24には、図4に示す如く、等配された例えば4つのジ
ョイントボルト取付部である第1〜第4ジョイントボル
ト取付孔26−1〜26−4が形成されている。
As shown in FIG. 4, first to fourth joint bolt mounting holes 26-1 to 26-4, which are, for example, four joint bolt mounting portions, are equally arranged on the yoke flat surface portion 24 of the joint yoke 14. Are formed.

【0018】また、前記接続用フランジ10のフランジ
平面部28には、円周方向等間隔で且つ前記第1〜第4
ジョイントボルト孔26−1〜26−4に対応した位置
に例えば4つのフランジ側ボルト取付部である第1〜第
4フランジボルト取付孔30−1〜30−4が形成され
ている。
Further, on the flange flat surface portion 28 of the connecting flange 10, the first to fourth portions are arranged at equal intervals in the circumferential direction.
First to fourth flange bolt mounting holes 30-1 to 30-4, which are four flange side bolt mounting portions, are formed at positions corresponding to the joint bolt holes 26-1 to 26-4, for example.

【0019】前記第1〜第4ジョイントボルト取付孔2
6−1〜26−4に第1〜第4接続用ボルト32−1〜
32−4が挿入され、この第1〜第4接続用ボルト32
−1〜32−4が前記第1〜第4フランジボルト取付孔
30−1〜30−4に夫々取り付けられる。
The first to fourth joint bolt mounting holes 2
First to fourth connecting bolts 32-1 to 6-1 to 26-4
32-4 is inserted, and the first to fourth connecting bolts 32
-1 to 32-4 are attached to the first to fourth flange bolt attachment holes 30-1 to 30-4, respectively.

【0020】前記接続用フランジ10に設けられた第1
〜第4フランジボルト取付孔30−1〜30−4間に夫
々形成した第1〜第4係合孔部34−1〜34−4と、
この第1〜第4係合孔部34−1〜34−4から前記ジ
ョイントヨーク14のヨーク平面部24部位に少許突出
すべく係合する突出部材36とにより前記接続用フラン
ジ10と前記シャフト本体4との面振れを減少させる面
振れ修正手段38を設ける。
The first provided on the connecting flange 10
~ First to fourth engagement hole portions 34-1 to 34-4 formed between the fourth flange bolt mounting holes 30-1 to 30-4, respectively,
The connecting flange 10 and the shaft body are formed by the projecting member 36 that engages with the first to fourth engaging hole portions 34-1 to 34-4 so as to slightly project into the yoke flat surface portion 24 of the joint yoke 14. 4 is provided with a surface wobbling correction means 38 for reducing the surface wobbling.

【0021】詳述すれば、前記第1、第2フランジボル
ト取付孔30−1、30−2間の略中央部位に第1係合
孔部34−1を設け、第2、第3フランジボルト取付孔
30−2、30−3間の略中央部位に第2係合孔部34
−2を設け、第3、第4フランジボルト取付孔30−
3、30−4間の略中央部位に第3係合孔部34−3を
設け、第4、第1フランジボルト取付孔30−4、30
−1間の略中央部位に第4係合孔部34−1を設ける。
前記第1〜第4係合孔部26−1〜26−4は内周部位
が螺刻されている。
More specifically, the first and second flange bolt mounting holes 30-1 and 30-2 are provided with a first engaging hole portion 34-1 at a substantially central portion thereof, and second and third flange bolts are provided. The second engaging hole portion 34 is provided at a substantially central portion between the mounting holes 30-2 and 30-3.
-2 is provided, and the third and fourth flange bolt mounting holes 30-
A third engaging hole portion 34-3 is provided at a substantially central portion between the third and 30-4, and fourth and first flange bolt mounting holes 30-4 and 30 are provided.
The fourth engagement hole portion 34-1 is provided at a substantially central portion between -1.
The inner peripheral portions of the first to fourth engagement hole portions 26-1 to 26-4 are threaded.

【0022】また、前記突出部材36は、前記第1〜第
4係合孔部26−1〜26−4に夫々螺合すべく外周部
位が螺刻されている。この突出部材36と第1〜第4係
合孔部26−1〜26−4とによって面振れ修正手段3
8が形成されている。
The outer peripheral portion of the projecting member 36 is threaded so as to be screwed into the first to fourth engaging hole portions 26-1 to 26-4, respectively. The surface wobbling correction means 3 is formed by the projecting member 36 and the first to fourth engagement hole portions 26-1 to 26-4.
8 is formed.

【0023】前記面振れ修正手段38は、図3に示す如
く、接続用フランジ10のフランジ平面部28が機械加
工時に発生する公差や振れによって一側の幅L1と他側
の幅L2とが異なる厚さとなってしまった時に厚さの小
さい幅L1側に形成される係合孔部、例えば第1係合孔
部34−1に螺合される突出部材36を幅L1と幅L2
との厚さの差だけヨーク平面部24側に突出させて接続
用フランジ10とシャフト本体4との面振れを減少する
ものである。
As shown in FIG. 3, the surface wobbling correcting means 38 has a width L1 on one side and a width L2 on the other side which are different from each other due to a tolerance or a wobbling which occurs in the flange flat surface portion 28 of the connecting flange 10 during machining. When the thickness of the protruding member 36 is screwed to the engaging hole portion formed on the side of the width L1 having a small thickness, for example, the first engaging hole portion 34-1, the width L1 and the width L2 are provided.
The surface run-out between the connecting flange 10 and the shaft body 4 is reduced by projecting the same toward the flat surface 24 of the yoke by the difference in the thickness of

【0024】次に、この実施例の作用を説明する。Next, the operation of this embodiment will be described.

【0025】駆動力発生手段たる内燃機関(図示せず)
と動力伝達機差動機6とをプロペラシャフト2によって
連結する際には、前記プロペラシャフト2の他端部位に
取り付けた自在継手8のジョイントヨーク14に前記差
動機6に取り付けた接続用フランジ10を接合してい
る。
Internal combustion engine (not shown) as driving force generating means
When connecting the power transmission and the differential gear 6 with the propeller shaft 2, the joint yoke 14 of the universal joint 8 attached to the other end portion of the propeller shaft 2 is provided with the connecting flange 10 attached to the differential gear 6. It is joined.

【0026】また、例えば、接続用フランジ10のフラ
ンジ平面部28が機械加工時に発生する公差や振れによ
って一側の幅L1と他側の幅L2とが異なる厚さとなっ
ている場合には、厚さの小さい幅L1側に形成される係
合孔部、例えば第1係合孔部34−1に螺合される突出
部材36のみを幅L1と幅L2との厚さの差だけヨーク
平面部24側に突出させて接続用フランジ10とシャフ
ト本体4との面振れを減少している。
Further, for example, in the case where the flange flat surface portion 28 of the connecting flange 10 has a thickness L1 on one side and a width L2 on the other side which are different from each other due to tolerances and runouts generated during machining, An engaging hole formed on the smaller width L1 side, for example, only the protruding member 36 screwed into the first engaging hole 34-1 is provided with the yoke flat surface portion by the difference in thickness between the width L1 and the width L2. The surface run-out between the connecting flange 10 and the shaft body 4 is reduced by projecting it to the side of 24.

【0027】その後に前記接続用フランジ10の第1〜
第4フランジボルト取付孔30−1〜30−4と前記ジ
ョイントヨーク14の第1〜第4ジョイントボルト取付
孔26−1〜26−4とに接続用ボルト32を夫々取り
付けている。
After that, the first to
Connection bolts 32 are attached to the fourth flange bolt attachment holes 30-1 to 30-4 and the first to fourth joint bolt attachment holes 26-1 to 26-4 of the joint yoke 14, respectively.

【0028】これにより、従来のものでは修正しきれな
かった接続用フランジ10とシャフト本体4との面振れ
を面振れ修正手段38減少させることができ、この接続
用フランジ10とシャフト本体4との面振れに起因する
プロペラシャフト2の振動を低減し得て、実用上有利で
ある。
As a result, the surface runout between the connecting flange 10 and the shaft body 4 which could not be corrected by the conventional one can be reduced, and the surface runout correcting means 38 can be reduced. Vibration of the propeller shaft 2 due to surface wobbling can be reduced, which is practically advantageous.

【0029】また、第1〜第4係合孔部34−1〜34
−4を形成する際に、この第1〜第4係合孔部34−1
〜34−4の螺刻ピッチと第1〜第4フランジボルト取
付孔30−1〜30−4の螺刻ピッチとを同一ピッチと
すれば、第1〜第4係合孔部34−1〜34−4をフラ
ンジボルト取付孔として機能させることができ、インロ
ー合わせのための接続用ボルト32の螺合時の選択の幅
を広げることができ、プロペラシャフト2のバランス状
態を向上し得て、実用上有利である。
The first to fourth engaging hole portions 34-1 to 34 are also provided.
-4, the first to fourth engagement hole portions 34-1 are formed.
To 34-4 and the thread pitches of the first to fourth flange bolt mounting holes 30-1 to 30-4 have the same pitch, the first to fourth engagement hole portions 34-1 to 34-1. 34-4 can be made to function as a flange bolt mounting hole, the range of selection at the time of screwing the connecting bolt 32 for inlay fitting can be widened, and the balance state of the propeller shaft 2 can be improved, It is practically advantageous.

【0030】[0030]

【発明の効果】以上詳細に説明した如くこの発明によれ
ば、一端部位を駆動力発生手段に連結するとともに他端
部位に取り付けた自在継手のジョイントヨークに動力伝
達機に取り付けた接続用フランジを接合し、接続用フラ
ンジの複数のフランジ側ボルト取付部とジョイントヨー
クの複数のヨーク側ボルト取付部とに接続用ボルトを取
り付けて他端部位を動力伝達機に連結させたプロペラシ
ャフトにおいて、接続用フランジに設けられた各フラン
ジ側ボルト取付部間に形成した係合孔部と、係合孔部か
らジョイントヨークのヨーク平面部位に少許突出すべく
係合する突出部材とにより接続用フランジとシャフト本
体との面振れを減少させる面振れ修正手段を設けたの
で、従来のものでは修正しきれなかった接続用フランジ
とシャフト本体との面振れを減少でき、接続用フランジ
とシャフト本体との面振れに起因するプロペラシャフト
の振動を減少し得て、実用上有利である。
As described in detail above, according to the present invention, the connecting yoke, which is attached to the power transmission device, is attached to the joint yoke of the universal joint which is connected to the driving force generating means at one end portion and is attached to the other end portion. In a propeller shaft that has been joined, connecting bolts have been attached to the flange-side bolt mounting portions of the connecting flange and the yoke-side bolt mounting portions of the joint yoke, and the other end portion has been connected to the power transmission. The connection flange and the shaft body are formed by the engagement holes formed between the flange-side bolt attachment portions provided on the flange, and the projecting members that engage with the yoke flat surface portion of the joint yoke from the engagement holes to slightly allow the connection. Since a surface wobbling correction means for reducing the surface wobbling of the connection flange and the shaft main body was not able to be corrected by the conventional one, Shake can be reduced to, and give reduced vibrations of the propeller shaft due to the surface deflection of the connecting flange and the shaft body, it is practically advantageous.

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

【図1】この発明の実施例を示すプロペラシャフトの要
部拡大図である。
FIG. 1 is an enlarged view of a main part of a propeller shaft showing an embodiment of the present invention.

【図2】接続用フランジの概略断面図である。FIG. 2 is a schematic sectional view of a connecting flange.

【図3】接続用フランジの断面図である。FIG. 3 is a sectional view of a connecting flange.

【図4】動力伝達系の組立斜視図である。FIG. 4 is an assembled perspective view of a power transmission system.

【図5】この発明の従来の技術を示す動力伝達系の概略
図である。
FIG. 5 is a schematic diagram of a power transmission system showing a conventional technique of the present invention.

【図6】動力伝達系の概略斜視図である。FIG. 6 is a schematic perspective view of a power transmission system.

【符号の説明】[Explanation of symbols]

2 プロペラシャフト 4 シャフト本体 6 動力伝達機 8 自在継手 10 接続用フランジ 12 シフトヨーク 14 ジョイントヨーク 18 差動機ケース 24 ヨーク平面部 26 ジョイントボルト取付孔 28 フランジ平面部 30 フランジボルト取付孔 32 接続用ボルト 34 係合孔部 36 突出部材 38 面振れ修正手段 2 Propeller shaft 4 Shaft body 6 Power transmission device 8 Universal joint 10 Connection flange 12 Shift yoke 14 Joint yoke 18 Differential gear case 24 Yoke flat part 26 Joint bolt mounting hole 28 Flange flat part 30 Flange bolt mounting hole 32 Connection bolt 34 Engagement hole portion 36 Projecting member 38 Surface deflection correcting means

【手続補正書】[Procedure amendment]

【提出日】平成5年4月20日[Submission date] April 20, 1993

【手続補正1】[Procedure Amendment 1]

【補正対象書類名】図面[Document name to be corrected] Drawing

【補正対象項目名】全図[Correction target item name] All drawings

【補正方法】変更[Correction method] Change

【補正内容】[Correction content]

【図1】 [Figure 1]

【図2】 [Fig. 2]

【図3】 [Figure 3]

【図4】 [Figure 4]

【図5】 [Figure 5]

【図6】 [Figure 6]

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】 一端部位を駆動力発生手段に連結すると
ともに他端部位に取り付けた自在継手のジョイントヨー
クに動力伝達機に取り付けた接続用フランジを接合し、
前記接続用フランジの複数のフランジ側ボルト取付部と
前記ジョイントヨークの複数のヨーク側ボルト取付部と
に接続用ボルトを取り付けて他端部位を前記動力伝達機
に連結させたプロペラシャフトにおいて、前記接続用フ
ランジに設けられた各フランジ側ボルト取付部間に形成
した係合孔部と、この係合孔部から前記ジョイントヨー
クのヨーク平面部位に少許突出すべく係合する突出部材
とにより前記接続用フランジと前記シャフト本体との面
振れを減少させる面振れ修正手段を設けたことを特徴と
するプロペラシャフト。
1. A connecting flange attached to a power transmission machine is joined to a joint yoke of a universal joint attached to the other end portion while connecting one end portion to a driving force generating means,
In the propeller shaft in which connecting bolts are attached to a plurality of flange side bolt mounting portions of the connecting flange and a plurality of yoke side bolt mounting portions of the joint yoke, and the other end portion is connected to the power transmission, The connecting holes are formed between the flange-side bolt mounting portions provided on the flange for use, and the projecting member is engaged with the yoke flat surface portion of the joint yoke from the engaging hole portions so as to slightly project the connection. A propeller shaft comprising a surface wobbling correction means for reducing surface wobbling between a flange and the shaft body.
JP3460693A 1993-01-30 1993-01-30 Propeller shaft Pending JPH06227274A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP3460693A JPH06227274A (en) 1993-01-30 1993-01-30 Propeller shaft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP3460693A JPH06227274A (en) 1993-01-30 1993-01-30 Propeller shaft

Publications (1)

Publication Number Publication Date
JPH06227274A true JPH06227274A (en) 1994-08-16

Family

ID=12419025

Family Applications (1)

Application Number Title Priority Date Filing Date
JP3460693A Pending JPH06227274A (en) 1993-01-30 1993-01-30 Propeller shaft

Country Status (1)

Country Link
JP (1) JPH06227274A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7361092B2 (en) * 2006-01-30 2008-04-22 Chrysler Llc Balance assembly for coupling first and second rotating members
US9309929B2 (en) * 2012-05-01 2016-04-12 Micro-Poise Measurement Systems, Llc Drive shaft adaptor and coupling
US20160190675A1 (en) * 2013-01-16 2016-06-30 Vipula DASANAYAKA Universal adapter plate assembly
US11225138B2 (en) * 2018-06-27 2022-01-18 Neapco Intellectual Property Holdings, Llc Center bearing assembly including a rotatable weld collar with a tuned damper

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7361092B2 (en) * 2006-01-30 2008-04-22 Chrysler Llc Balance assembly for coupling first and second rotating members
US9309929B2 (en) * 2012-05-01 2016-04-12 Micro-Poise Measurement Systems, Llc Drive shaft adaptor and coupling
US20160190675A1 (en) * 2013-01-16 2016-06-30 Vipula DASANAYAKA Universal adapter plate assembly
US10897071B2 (en) * 2013-01-16 2021-01-19 Haeco Americas, Llc Universal adapter plate assembly
US11575191B2 (en) 2013-01-16 2023-02-07 Haeco Americas, Llc Universal adapter plate assembly
US11225138B2 (en) * 2018-06-27 2022-01-18 Neapco Intellectual Property Holdings, Llc Center bearing assembly including a rotatable weld collar with a tuned damper

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