JP2006329277A - Propeller shaft supporting structure - Google Patents

Propeller shaft supporting structure Download PDF

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Publication number
JP2006329277A
JP2006329277A JP2005151644A JP2005151644A JP2006329277A JP 2006329277 A JP2006329277 A JP 2006329277A JP 2005151644 A JP2005151644 A JP 2005151644A JP 2005151644 A JP2005151644 A JP 2005151644A JP 2006329277 A JP2006329277 A JP 2006329277A
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Prior art keywords
propeller shaft
stopper piece
center bearing
inner ring
cover
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JP2005151644A
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Japanese (ja)
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Ryohei Osawa
良平 大澤
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Showa Corp
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Showa Corp
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Priority to JP2005151644A priority Critical patent/JP2006329277A/en
Publication of JP2006329277A publication Critical patent/JP2006329277A/en
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2326/00Articles relating to transporting
    • F16C2326/01Parts of vehicles in general
    • F16C2326/06Drive shafts

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  • Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)
  • Mounting Of Bearings Or Others (AREA)
  • Sealing Of Bearings (AREA)

Abstract

<P>PROBLEM TO BE SOLVED: To prevent a center bearing fitted to a propeller shaft from falling off while easing the machining accuracy of an insertion portion between the propeller shaft and a stopper piece for positioning the center bearing in a propeller shaft supporting structure. <P>SOLUTION: In the propeller shaft supporting structure for supporting the propeller shaft 10 via the center bearing 20 on the inside of an inner collar 31 of an annular supporting member 30, the stopper piece 40 for colliding into an end face of an inner ring 21 of the center bearing 20 and positioning the center bearing 20 in the axial direction is inserted and fitted to the propeller shaft 10, and a nut 60 for supporting, in the axial direction, the colliding end of the stopper piece 40 to the inner ring 21 and the other end of the stopper piece 40 on the opposite side is screwed to the propeller shaft 10. <P>COPYRIGHT: (C)2007,JPO&INPIT

Description

本発明はプロペラシャフト支持構造に関する。   The present invention relates to a propeller shaft support structure.

自動車用のプロペラシャフト支持構造として、特許文献1に記載の如く、車体側に取付けられる支持ブラケットに環状支持部材を設け、環状支持部材の内環と外環を弾性部材により接続し、環状支持部材の内環の内側に、センタベアリングを介してプロペラシャフトを支持するものがある。
特開2004-44622
As a propeller shaft support structure for an automobile, as described in Patent Document 1, an annular support member is provided on a support bracket attached to the vehicle body side, and an inner ring and an outer ring of the annular support member are connected by an elastic member. Some of the inner rings support the propeller shaft via a center bearing.
JP2004-44622

特許文献1のプロペラシャフト支持構造では、プロペラシャフトに嵌合したセンタベアリングの抜け止めを図るため、センタベアリングの内輪の端面に衝合して該センタベアリングを軸方向に位置決めするストッパピースをプロペラシャフトに圧入している。ストッパピースとプロペラシャフトの挿着部に圧入のための適度な締め代を与え、ストッパピースをプロペラシャフトに固定するものである。   In the propeller shaft support structure of Patent Document 1, in order to prevent the center bearing fitted to the propeller shaft from coming off, a stopper piece that abuts the end surface of the inner ring of the center bearing and positions the center bearing in the axial direction is provided on the propeller shaft. Is press-fitted. An appropriate tightening allowance for press-fitting is given to the insertion portion between the stopper piece and the propeller shaft, and the stopper piece is fixed to the propeller shaft.

しかしながら、ストッパピースとプロペラシャフトの挿着部に適度な締め代を与えるためには、プロペラシャフトとストッパピースの両者を適度な寸法精度で加工する必要があり、生産性が悪い。   However, in order to give an appropriate tightening allowance to the insertion portion between the stopper piece and the propeller shaft, it is necessary to process both the propeller shaft and the stopper piece with an appropriate dimensional accuracy, resulting in poor productivity.

本発明の課題は、プロペラシャフト支持構造において、プロペラシャフトとセンタベアリング位置決め用ストッパピースとの挿着部の加工精度を緩和しながら、プロペラシャフトに嵌合したセンタベアリングの抜け止めを図ることにある。   An object of the present invention is to prevent a center bearing fitted to a propeller shaft from coming off while relaxing processing accuracy of an insertion portion between the propeller shaft and a center bearing positioning stopper piece in a propeller shaft support structure. .

請求項1の発明は、環状支持部材の内環内側に、センタベアリングを介してプロペラシャフトを支持するプロペラシャフト支持構造において、センタベアリングの内輪の端面に衝合して該センタベアリングを軸方向に位置決めするストッパピースをプロペラシャフトに挿着し、ストッパピースの前記内輪との衝合端と反対側の端部を軸方向で支持するナットをプロペラシャフトに螺着してなるようにしたものである。   According to the first aspect of the present invention, in the propeller shaft support structure that supports the propeller shaft via the center bearing inside the inner ring of the annular support member, the center bearing abuts on the end face of the inner ring of the center bearing in the axial direction. A stopper piece to be positioned is inserted into the propeller shaft, and a nut that supports the end of the stopper piece opposite to the abutting end with the inner ring in the axial direction is screwed onto the propeller shaft. .

請求項2の発明は、請求項1の発明において更に、前記ナットとストッパピースの間にカバーを挟持し、該カバーが前記内環の開口を覆うフランジを備えるようにしたものである。   According to a second aspect of the present invention, in the first aspect of the present invention, a cover is sandwiched between the nut and the stopper piece, and the cover includes a flange that covers the opening of the inner ring.

請求項3の発明は、請求項1又は2の発明において更に、前記カバーのピース嵌合筒に予めストッパピースを圧入してなるようにしたものである。   According to a third aspect of the present invention, in the first or second aspect of the present invention, a stopper piece is previously press-fitted into the piece fitting cylinder of the cover.

(請求項1)
(a)プロペラシャフトに螺着したナットにより、ストッパピースを軸方向で支持し、ひいてはセンタベアリングを抜け止めする。センタベアリングの抜け止め力が、プロペラシャフトへのストッパピースの圧入保持力に依存するものでないから、プロペラシャフトとストッパピースの挿着部に圧入のための寸法精度を必要としない。従って、プロペラシャフトとストッパピースの挿着部の加工精度を緩和しながら、プロペラシャフトに嵌合したセンタベアリングを抜け止めできる。
(Claim 1)
(a) The stopper piece is supported in the axial direction by a nut screwed onto the propeller shaft, and the center bearing is prevented from coming off. Since the retaining force of the center bearing does not depend on the press-fitting holding force of the stopper piece to the propeller shaft, dimensional accuracy for press-fitting is not required at the insertion portion of the propeller shaft and the stopper piece. Therefore, it is possible to prevent the center bearing fitted to the propeller shaft from coming off while relaxing the processing accuracy of the insertion portion between the propeller shaft and the stopper piece.

(請求項2)
(b)ストッパピースとナットの間に挟持したカバーのフランジが内環の開口を覆い、内環の内部、ひいてはセンタベアリングへの泥水等の浸入を防止し、センタベアリングの損傷を防止できる。
(Claim 2)
(b) The flange of the cover sandwiched between the stopper piece and the nut covers the opening of the inner ring, preventing the intrusion of muddy water or the like into the inner ring, and hence the center bearing, and the center bearing can be prevented from being damaged.

(請求項3)
(c)カバーのピース嵌合筒に予めストッパピースを圧入することにより、カバーを介してストッパピースを軸方向で確実に支持できる。また、カバー及びストッパピースを小組状態でプロペラシャフトに挿着でき、組付性を向上できる。
(Claim 3)
(c) The stopper piece can be reliably supported in the axial direction through the cover by press-fitting the stopper piece into the piece fitting cylinder of the cover in advance. Further, the cover and the stopper piece can be inserted into the propeller shaft in a small assembled state, and the assemblability can be improved.

図1は自動車用プロペラシャフトを示す全体図、図2は図1の要部断面図、図3はプロペラシャフト支持構造の組付前状態を示す断面図、図4はストッパピースとカバーとナットを示す断面図、図5はカバーを示す斜視図である。   1 is an overall view showing a propeller shaft for an automobile, FIG. 2 is a cross-sectional view of the main part of FIG. 1, FIG. 3 is a cross-sectional view showing a state before assembly of the propeller shaft support structure, and FIG. FIG. 5 is a perspective view showing a cover.

自動車(FR車又は4WD車)用衝撃吸収プロペラシャフト10は、図1に示す如く、前側分割シャフト10Aと後側分割シャフト10Bに分割された2本のシャフト部材からなり、両分割シャフト10A、10Bを等速継手(スライダブルジョイント)12により連結して構成される。前側分割シャフト10Aの前端部は、自在継手13を介して、エンジン側のトランスミッションの出力軸に接続される連結ヨーク14と連結され、後側分割シャフト10Bの後端部は、自在継手15を介して、デファレンシャルギヤに接続される連結ヨーク16と連結される。   As shown in FIG. 1, an impact absorbing propeller shaft 10 for an automobile (FR vehicle or 4WD vehicle) is composed of two shaft members divided into a front divided shaft 10A and a rear divided shaft 10B, and both divided shafts 10A, 10B. Are connected by a constant velocity joint (slidable joint) 12. The front end portion of the front split shaft 10A is connected to a connecting yoke 14 connected to the output shaft of the engine side transmission via a universal joint 13, and the rear end portion of the rear side split shaft 10B is connected to a universal joint 15. Thus, it is coupled to the coupling yoke 16 connected to the differential gear.

プロペラシャフト10(シャフト10B)は、図2、図3に示す如く、大径部11Aから、継手12が接続される継手部11Eに渡って、外径を階段状に小径化する第1中径部11B、第2中径部11C、小径部11Dを備える。プロペラシャフト10は、小径部11Dに嵌合されるセンタベアリング20を介して環状支持部材30に回転自在に支持される。   As shown in FIGS. 2 and 3, the propeller shaft 10 (shaft 10B) has a first medium diameter whose outer diameter is reduced stepwise from the large diameter portion 11A to the joint portion 11E to which the joint 12 is connected. A portion 11B, a second medium diameter portion 11C, and a small diameter portion 11D are provided. The propeller shaft 10 is rotatably supported by the annular support member 30 via a center bearing 20 fitted to the small diameter portion 11D.

センタベアリング20は、ボールベアリングであり、プロペラシャフト10の小径部11Dに嵌合し、内輪21の後端面を第2中径部11Cの側面に当接して位置決めされる。   The center bearing 20 is a ball bearing, is fitted to the small diameter portion 11D of the propeller shaft 10, and is positioned by contacting the rear end surface of the inner ring 21 with the side surface of the second medium diameter portion 11C.

環状支持部材30は、内環31と外環32をゴム弾性部材33を介して接続して構成され、外環32を支持ブラケット34に支持される。環状支持部材30の内環31は、大径部31A、中径部31B、小径部31Cを順に小径化した段付円筒環をなす。中径部31Bの内側にセンタベアリング20の外輪22が嵌合され、大径部31Aはプロペラシャフト10の第1中径部11Bの外周を覆うように後方へ延在し、小径部31Cはプロペラシャフト10の小径部11Dの外周を覆うように前方へ延在する。   The annular support member 30 is configured by connecting an inner ring 31 and an outer ring 32 via a rubber elastic member 33, and the outer ring 32 is supported by a support bracket 34. The inner ring 31 of the annular support member 30 forms a stepped cylindrical ring in which the large diameter portion 31A, the medium diameter portion 31B, and the small diameter portion 31C are sequentially reduced in diameter. The outer ring 22 of the center bearing 20 is fitted inside the medium diameter part 31B, the large diameter part 31A extends rearward so as to cover the outer periphery of the first medium diameter part 11B of the propeller shaft 10, and the small diameter part 31C is the propeller. The shaft 10 extends forward so as to cover the outer periphery of the small diameter portion 11D of the shaft 10.

プロペラシャフト10は、環状支持部材30の内環31に上述の如くに嵌合されるセンタベアリング20を介して、回転自在に支持され、センタベアリング20の前後両側(内環31の大径部31Aと小径部31Cの内周)にはシール部材23、24が挿着される。この状態で、センタベアリング20の内輪21の前端面に衝合して該センタベアリング20を軸方向に位置決めするストッパピース40をプロペラシャフト10の小径部11Dに挿着し、ストッパピース40の上記内輪21との衝合端と反対側の端部を軸方向で位置決め支持するナット60がプロペラシャフト10の小径部11Dに設けたねじ部61に螺着される。このとき、ナット60とストッパピース40の間にカバー50が挟持される。   The propeller shaft 10 is rotatably supported via the center bearing 20 that is fitted to the inner ring 31 of the annular support member 30 as described above, and both front and rear sides of the center bearing 20 (the large diameter portion 31A of the inner ring 31). And sealing members 23 and 24 are inserted into the inner circumference of the small diameter portion 31C. In this state, a stopper piece 40 that abuts the front end surface of the inner ring 21 of the center bearing 20 and positions the center bearing 20 in the axial direction is inserted into the small diameter portion 11D of the propeller shaft 10, and the inner ring of the stopper piece 40 is inserted. A nut 60 for positioning and supporting the end portion opposite to the abutting end with the shaft 21 in the axial direction is screwed to a screw portion 61 provided on the small diameter portion 11D of the propeller shaft 10. At this time, the cover 50 is sandwiched between the nut 60 and the stopper piece 40.

ストッパピース40は、図3、図4に示す如く、例えば鋼製の円筒状をなす。ストッパピース40はプロペラシャフト10の小径部11Dに軽く挿着可能にするように該小径部11Dの外径よりわずかに大きい内径を有する。   The stopper piece 40 has a cylindrical shape made of steel, for example, as shown in FIGS. The stopper piece 40 has an inner diameter slightly larger than the outer diameter of the small diameter portion 11D so that the stopper piece 40 can be lightly inserted into the small diameter portion 11D of the propeller shaft 10.

カバー50は、図4、図5に示す如く、例えばステンレス又は鋼製の薄板成形品からなり、端板51、ピース嵌合筒52、大径フランジ53を順に大径にした円筒体をなす。   As shown in FIGS. 4 and 5, the cover 50 is made of, for example, a thin plate product made of stainless steel or steel, and forms a cylindrical body in which an end plate 51, a piece fitting cylinder 52, and a large diameter flange 53 are sequentially increased in diameter.

端板51はプロペラシャフト10の小径部11D(ねじ部61)まわりに挿着し得るように該小径部11Dのねじ径よりわずかに大きい内径を有する。小径部11Dのねじ部61に螺着されたナット60の端面が端板51に衝接する。   The end plate 51 has an inner diameter slightly larger than the screw diameter of the small diameter portion 11D so that the end plate 51 can be inserted around the small diameter portion 11D (screw portion 61) of the propeller shaft 10. The end surface of the nut 60 screwed to the screw portion 61 of the small diameter portion 11D comes into contact with the end plate 51.

フランジ53は環状支持部材30の内環31の小径部31Cより外径が大きい。カバー50は、プロペラシャフト10の小径部11Dに挿着され、ストッパピース40とナット60により挟持される状態で、内環31の前側開口を覆い、泥水浸入防止用フランジを構成する。   The flange 53 has a larger outer diameter than the small diameter portion 31 </ b> C of the inner ring 31 of the annular support member 30. The cover 50 is inserted into the small diameter portion 11D of the propeller shaft 10 and covers the front opening of the inner ring 31 in a state of being sandwiched between the stopper piece 40 and the nut 60, and constitutes a muddy water intrusion prevention flange.

ストッパピース40とカバー50は、プロペラシャフト10の小径部11Dに挿着される前に予め、カバー50のピース嵌合筒52の内径部にストッパピース40の前端部を圧入した小組状態にされる(図3)。ピース嵌合筒52はストッパピース40を圧入可能にするように該ストッパピース40の外径よりわずかに小さい内径を有する。ストッパピース40の前端面は、上述の圧入状態で、カバー50のピース嵌合筒52の底面(端板51)に衝合する。   The stopper piece 40 and the cover 50 are in a small assembly state in which the front end portion of the stopper piece 40 is press-fitted into the inner diameter portion of the piece fitting cylinder 52 of the cover 50 before being inserted into the small diameter portion 11D of the propeller shaft 10. (Figure 3). The piece fitting cylinder 52 has an inner diameter slightly smaller than the outer diameter of the stopper piece 40 so that the stopper piece 40 can be press-fitted. The front end surface of the stopper piece 40 abuts against the bottom surface (end plate 51) of the piece fitting cylinder 52 of the cover 50 in the above-described press-fitted state.

従って、ストッパピース40及びカバー50は以下の如くに用いられる。
(1)小組状態にされたストッパピース40とカバー50をプロペラシャフト10の小径部11Dに軽く挿着する。ストッパピース40の後端がシール部材23の内側を貫通してセンタベアリング20の内輪21の前端面に当接し、センタベアリング20を位置決めする。
Therefore, the stopper piece 40 and the cover 50 are used as follows.
(1) The stopper piece 40 and the cover 50 in the small assembly state are lightly inserted into the small diameter portion 11D of the propeller shaft 10. The rear end of the stopper piece 40 penetrates the inside of the seal member 23 and comes into contact with the front end surface of the inner ring 21 of the center bearing 20 to position the center bearing 20.

(2)ナット60をプロペラシャフト10の小径部11Dのねじ部61に螺着し、ナット60の端面をカバー50の端板51に衝接する。これにより、ナット60はカバー50を介してストッパピース40を軸方向で支持し、センタベアリング20を抜け止めする。このとき、カバー50のフランジ53は、環状支持部材30の内環31の前側開口を覆う。   (2) The nut 60 is screwed to the screw portion 61 of the small diameter portion 11D of the propeller shaft 10 and the end surface of the nut 60 is brought into contact with the end plate 51 of the cover 50. As a result, the nut 60 supports the stopper piece 40 in the axial direction via the cover 50 and prevents the center bearing 20 from coming off. At this time, the flange 53 of the cover 50 covers the front opening of the inner ring 31 of the annular support member 30.

(3)プロペラシャフト10に泥水がかかった場合、環状支持部材30の内環31の前側開口がカバー50のフランジ53に覆われ、この泥水が内環31内へ浸入することを防止する。   (3) When muddy water is applied to the propeller shaft 10, the front opening of the inner ring 31 of the annular support member 30 is covered with the flange 53 of the cover 50, and this muddy water is prevented from entering the inner ring 31.

尚、内環31の後側開口は、プロペラシャフト10の大径部11Aで覆われて内環31内への泥水の浸入が防止されている。仮に大径部11Aから浸入した泥水があっても、この泥水は内環31の大径部31A内に配置されている第1中径部11Bに設けてある溝条部に直ちに捕捉されて下方へ落下排除され、内環31内へ浸入することが阻止される。   The rear opening of the inner ring 31 is covered with the large-diameter portion 11A of the propeller shaft 10 to prevent muddy water from entering the inner ring 31. Even if there is muddy water that has entered from the large-diameter portion 11A, this muddy water is immediately captured by the groove portion provided in the first medium-diameter portion 11B disposed in the large-diameter portion 31A of the inner ring 31 and below. And is prevented from entering the inner ring 31.

カバー50において、フランジ53に後続する溝条部を設け、この溝条部を内環31の小径部31C内に位置付ければ、プロペラシャフト10の第1中径部11Bが備える溝条部と同様の泥水落下排除機能を果たす。   In the cover 50, if a groove portion following the flange 53 is provided, and this groove portion is positioned in the small diameter portion 31 </ b> C of the inner ring 31, the groove portion provided in the first medium diameter portion 11 </ b> B of the propeller shaft 10 is the same. Fulfills the function of eliminating mud drops.

環状支持部材30の内環31に嵌合されているセンタベアリング20は、前後をシール部材23、24によりシールされる上に、内環31の前後開口からの泥水浸入を上述の如くに防止され、泥水から確実に保護される。   The center bearing 20 fitted to the inner ring 31 of the annular support member 30 is sealed by the seal members 23 and 24 at the front and rear, and the muddy water is prevented from entering from the front and rear openings of the inner ring 31 as described above. , Reliably protected from muddy water.

本実施例によれば以下の作用効果を奏する。
(a)プロペラシャフト10に螺着したナット60により、ストッパピース40を軸方向で支持し、ひいてはセンタベアリング20を抜け止めする。センタベアリング20の抜け止め力が、プロペラシャフト10へのストッパピース40の圧入保持力に依存するものでないから、プロペラシャフト10とストッパピース40の挿着部に圧入のための寸法精度を必要としない。従って、プロペラシャフト10とストッパピース40の挿着部の加工精度を緩和しながら、プロペラシャフト10に嵌合したセンタベアリング20を抜け止めできる。
According to the present embodiment, the following operational effects can be obtained.
(a) The stopper piece 40 is supported in the axial direction by the nut 60 screwed to the propeller shaft 10, and the center bearing 20 is prevented from coming off. Since the retaining force of the center bearing 20 does not depend on the press-fitting holding force of the stopper piece 40 to the propeller shaft 10, dimensional accuracy for press-fitting is not required at the insertion portion of the propeller shaft 10 and the stopper piece 40. . Therefore, the center bearing 20 fitted to the propeller shaft 10 can be prevented from coming off while relaxing the processing accuracy of the insertion portion between the propeller shaft 10 and the stopper piece 40.

(b)ストッパピース40とナット60の間に挟持したカバー50のフランジ53が内環31の開口を覆い、内環31の内部、ひいてはセンタベアリング20への泥水等の浸入を防止し、センタベアリング20の損傷を防止できる。   (b) The flange 53 of the cover 50 sandwiched between the stopper piece 40 and the nut 60 covers the opening of the inner ring 31 and prevents intrusion of muddy water or the like into the inner ring 31 and thus into the center bearing 20. 20 damage can be prevented.

(c)カバー50のピース嵌合筒52に予めストッパピース40を圧入保持することにより、カバー50を介してストッパピース40を軸方向で確実に支持できる。また、カバー50及びストッパピース40を小組状態でプロペラシャフト10に挿着でき、組付性を向上できる。   (c) The stopper piece 40 can be reliably supported in the axial direction via the cover 50 by press-fitting and holding the stopper piece 40 in advance in the piece fitting cylinder 52 of the cover 50. Further, the cover 50 and the stopper piece 40 can be inserted into the propeller shaft 10 in a small assembled state, and the assembling property can be improved.

以上、本発明の実施例を図面により詳述したが、本発明の具体的な構成はこの実施例に限られるものではなく、本発明の要旨を逸脱しない範囲の設計の変更等があっても本発明に含まれる。例えば、カバーとストッパピースは互いに圧入することを必須としない。   The embodiment of the present invention has been described in detail with reference to the drawings. However, the specific configuration of the present invention is not limited to this embodiment, and even if there is a design change or the like without departing from the gist of the present invention. It is included in the present invention. For example, it is not essential that the cover and the stopper piece are press-fitted together.

また、本発明の実施においては、プロペラシャフトに螺着したナットによりストッパピースを支持すれば足り、カバーを併せ用いることを必須としない。   In the practice of the present invention, it is sufficient to support the stopper piece with a nut screwed to the propeller shaft, and it is not essential to use a cover together.

図1は自動車用プロペラシャフトを示す全体図である。FIG. 1 is an overall view showing an automobile propeller shaft. 図2は図1の要部断面図である。FIG. 2 is a cross-sectional view of the main part of FIG. 図3はプロペラシャフト支持構造の組付前状態を示す断面図である。FIG. 3 is a cross-sectional view showing a state before assembly of the propeller shaft support structure. 図4はストッパピースとカバーとナットを示す断面図である。FIG. 4 is a sectional view showing the stopper piece, the cover, and the nut. 図5はカバーを示す斜視図である。FIG. 5 is a perspective view showing the cover.

符号の説明Explanation of symbols

10 プロペラシャフト
20 センタベアリング
21 内輪
30 環状支持部材
31 内環
40 ストッパピース
50 カバー
52 ピース嵌合筒
53 フランジ
60 ナット
10 propeller shaft 20 center bearing 21 inner ring 30 annular support member 31 inner ring 40 stopper piece 50 cover 52 piece fitting cylinder 53 flange 60 nut

Claims (3)

環状支持部材の内環内側に、センタベアリングを介してプロペラシャフトを支持するプロペラシャフト支持構造において、
センタベアリングの内輪の端面に衝合して該センタベアリングを軸方向に位置決めするストッパピースをプロペラシャフトに挿着し、
ストッパピースの前記内輪との衝合端と反対側の端部を軸方向で支持するナットをプロペラシャフトに螺着してなることを特徴とするプロペラシャフト支持構造。
In the propeller shaft support structure that supports the propeller shaft via the center bearing inside the inner ring of the annular support member,
A stopper piece that abuts the end surface of the inner ring of the center bearing and positions the center bearing in the axial direction is inserted into the propeller shaft,
A propeller shaft support structure, wherein a nut for axially supporting an end of the stopper piece opposite to the abutting end with the inner ring is screwed to the propeller shaft.
前記ナットとストッパピースの間にカバーを挟持し、該カバーが前記内環の開口を覆うフランジを備える請求項1に記載のプロペラシャフト支持構造。   The propeller shaft support structure according to claim 1, wherein a cover is sandwiched between the nut and the stopper piece, and the cover includes a flange that covers the opening of the inner ring. 前記カバーのピース嵌合筒に予めストッパピースを圧入してなる請求項1又は2に記載のプロペラシャフト支持構造。   The propeller shaft support structure according to claim 1 or 2, wherein a stopper piece is press-fitted in advance into the piece fitting cylinder of the cover.
JP2005151644A 2005-05-24 2005-05-24 Propeller shaft supporting structure Pending JP2006329277A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2005151644A JP2006329277A (en) 2005-05-24 2005-05-24 Propeller shaft supporting structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2005151644A JP2006329277A (en) 2005-05-24 2005-05-24 Propeller shaft supporting structure

Publications (1)

Publication Number Publication Date
JP2006329277A true JP2006329277A (en) 2006-12-07

Family

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Family Applications (1)

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Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6122927U (en) * 1984-07-13 1986-02-10 ダイハツ工業株式会社 Dust-proof structure of oil seal on drive axle
JPH0251768U (en) * 1988-10-05 1990-04-12
JPH0732226U (en) * 1993-11-16 1995-06-16 株式会社ユニシアジェックス Center bearing of propeller shaft
JPH0882317A (en) * 1994-09-13 1996-03-26 Jidosha Buhin Kogyo Kk Vehicular propeller shaft
JP2000170759A (en) * 1998-12-10 2000-06-20 Showa Corp Propeller shaft supporting structure
JP2002327730A (en) * 2001-05-01 2002-11-15 Ntn Corp Connecting bar and connecting bar with bearing

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6122927U (en) * 1984-07-13 1986-02-10 ダイハツ工業株式会社 Dust-proof structure of oil seal on drive axle
JPH0251768U (en) * 1988-10-05 1990-04-12
JPH0732226U (en) * 1993-11-16 1995-06-16 株式会社ユニシアジェックス Center bearing of propeller shaft
JPH0882317A (en) * 1994-09-13 1996-03-26 Jidosha Buhin Kogyo Kk Vehicular propeller shaft
JP2000170759A (en) * 1998-12-10 2000-06-20 Showa Corp Propeller shaft supporting structure
JP2002327730A (en) * 2001-05-01 2002-11-15 Ntn Corp Connecting bar and connecting bar with bearing

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