JPH06227274A - Propeller shaft - Google Patents
Propeller shaftInfo
- 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
Links
Landscapes
- Motor Power Transmission Devices (AREA)
- Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)
Abstract
Description
【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.
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)
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.
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)
| 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 |
-
1993
- 1993-01-30 JP JP3460693A patent/JPH06227274A/en active Pending
Cited By (6)
| 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 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JPH06227274A (en) | Propeller shaft | |
| JPH01145426A (en) | Coupling for inboard and outboard engine | |
| JPH09254673A (en) | Vehicular propeller shaft and method for correcting its imbalance | |
| US6277027B1 (en) | Hydrodynamic torque converter with connecting elements attached by outward pressings | |
| EP1564059B1 (en) | Engine to transmission coupler | |
| JP2007302084A (en) | Torque rod | |
| JP2000071794A (en) | Axle housing support structure | |
| JP3194154B2 (en) | Propeller shaft | |
| US5644955A (en) | Structure for supporting driving reaction force on differential housing | |
| JPH09280325A (en) | Silk-hat type flexibly engaging gear device | |
| JPH089480Y2 (en) | Transmission case assembly structure | |
| JP2001213179A (en) | Automatic transmission mounting structure for hybrid vehicle | |
| JPH0810019Y2 (en) | Dynamic damper for transmission | |
| JPH0627816Y2 (en) | Engine cylinder block | |
| JP2605185Y2 (en) | Propeller shaft imbalance correction device | |
| JPH09169221A (en) | Joint part structure of propeller shaft | |
| JPH06239155A (en) | Propeller shaft for automobile | |
| JPS6222427Y2 (en) | ||
| JPS6319364B2 (en) | ||
| JPH05332347A (en) | Propeller shaft | |
| JPS6334982Y2 (en) | ||
| JPS6271725A (en) | Intermediate-shaft supporting structure of front-wheel drive vehicle | |
| JP3063821B2 (en) | Vehicle propeller shaft structure | |
| JP3178254B2 (en) | How to correct the connecting shaft balance | |
| JP2596592Y2 (en) | Boot band for drive shaft |