JPH0643544Y2 - Elastic joint structure - Google Patents

Elastic joint structure

Info

Publication number
JPH0643544Y2
JPH0643544Y2 JP1989062285U JP6228589U JPH0643544Y2 JP H0643544 Y2 JPH0643544 Y2 JP H0643544Y2 JP 1989062285 U JP1989062285 U JP 1989062285U JP 6228589 U JP6228589 U JP 6228589U JP H0643544 Y2 JPH0643544 Y2 JP H0643544Y2
Authority
JP
Japan
Prior art keywords
elastic
layer
bearing
shaft
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.)
Expired - Lifetime
Application number
JP1989062285U
Other languages
Japanese (ja)
Other versions
JPH031322U (en
Inventor
康彦 三原
嘉一 加藤
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 JP1989062285U priority Critical patent/JPH0643544Y2/en
Publication of JPH031322U publication Critical patent/JPH031322U/ja
Application granted granted Critical
Publication of JPH0643544Y2 publication Critical patent/JPH0643544Y2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • 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
    • F16DCOUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
    • F16D3/00Yielding couplings, i.e. with means permitting movement between the connected parts during the drive
    • F16D3/50Yielding couplings, i.e. with means permitting movement between the connected parts during the drive with the coupling parts connected by one or more intermediate members
    • F16D3/78Yielding couplings, i.e. with means permitting movement between the connected parts during the drive with the coupling parts connected by one or more intermediate members shaped as an elastic disc or flat ring, arranged perpendicular to the axis of the coupling parts, different sets of spots of the disc or ring being attached to each coupling part, e.g. Hardy couplings
    • 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
    • F16DCOUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
    • F16D3/00Yielding couplings, i.e. with means permitting movement between the connected parts during the drive
    • F16D3/50Yielding couplings, i.e. with means permitting movement between the connected parts during the drive with the coupling parts connected by one or more intermediate members
    • F16D3/60Yielding couplings, i.e. with means permitting movement between the connected parts during the drive with the coupling parts connected by one or more intermediate members comprising pushing or pulling links attached to both parts
    • F16D3/62Yielding couplings, i.e. with means permitting movement between the connected parts during the drive with the coupling parts connected by one or more intermediate members comprising pushing or pulling links attached to both parts the links or their attachments being elastic

Description

【考案の詳細な説明】 (産業上の利用分野) この考案はプロペラシャフトの弾性継手構造に関し、詳
しくは振動伝達防止のための技術手段に関する。
DETAILED DESCRIPTION OF THE INVENTION (Industrial field of application) The present invention relates to an elastic joint structure of a propeller shaft, and more particularly to a technical means for preventing vibration transmission.

(従来の技術) エンジンで発生した動力を後車軸に伝達するプロペラシ
ャフトの継手の一種として、第4図に示しているような
弾性継手が用いられている。この弾性継手は、ラバーカ
ップリング100の取付穴にプロペラシャフト102のヨーク
部104及び相手部材106(ここでは滑り継手のスリーブ)
のヨーク部108を夫々固定して、これらプロペラシャフ
ト102及びスリーブ106を互いに連結するもので、このラ
バーカップリング100の弾性作用により振動を低減した
り、駆動系に加わる衝撃荷重を緩和し得るなどの特長を
有している。
(Prior Art) An elastic joint as shown in FIG. 4 is used as a kind of joint of a propeller shaft for transmitting power generated by an engine to a rear axle. This elastic joint includes a yoke portion 104 of a propeller shaft 102 and a mating member 106 (here, a sleeve of a slip joint) in a mounting hole of a rubber coupling 100.
The yoke portions 108 are fixed to each other to connect the propeller shaft 102 and the sleeve 106 to each other. The elastic action of the rubber coupling 100 can reduce vibration and reduce impact load applied to the drive system. It has the features of

(考案が解決しようとする課題) ところでこの弾性継手には心合せ機構が設けられてい
て、プロペラシャフト102とスリーブ106との軸心が合わ
されるようになっているが、従来この心合せ機構部にお
いて振動が伝達されてしまう不具合が生じていた。即ち
第4図の例において、スリーブ106の側には自動調心ベ
アリング110が設けられる一方、他方のプロペラシャフ
ト102の側には心合せ軸112が設けられ、この心合せ軸11
2が自動調心ベアリング110の嵌合孔に摺動可能に嵌合さ
れて、プロペラシャフト102とスリーブ106との軸心が一
致させられるようになっているが、この心合せ機構にお
いては、組付け時のずれ或いは使用期間中の荷重の作用
等により半径方向に力が加わったとき、心合せ軸112と
自動調心ベアリング110との嵌合面の面圧が高くなって
両者の軸方向の摺動抵抗が増大し、このためにかかる心
合せ機構部を通じてスリーブ106の側からプロペラシャ
フト102側へと振動が伝達されてしまうのである。
(Problems to be Solved by the Invention) By the way, this elastic joint is provided with a centering mechanism so that the shaft centers of the propeller shaft 102 and the sleeve 106 are aligned with each other. There was a problem that the vibration was transmitted in. That is, in the example of FIG. 4, a self-aligning bearing 110 is provided on the sleeve 106 side, and an alignment shaft 112 is provided on the other propeller shaft 102 side.
2 is slidably fitted in the fitting hole of the self-aligning bearing 110 so that the shaft centers of the propeller shaft 102 and the sleeve 106 are aligned with each other. When a force is applied in the radial direction due to the deviation during mounting or the action of load during use, etc., the surface pressure of the mating surface between the centering shaft 112 and the self-aligning bearing 110 increases, and Sliding resistance increases, and vibration is transmitted from the sleeve 106 side to the propeller shaft 102 side through the centering mechanism portion.

(課題を解決するための手段) 本考案はこのような課題を解決するためになされたもの
であり、その要旨は、プロペラシャフトをラバーカップ
リングを介して相手部材に連結するとともに、それらの
何れか一方に心合せ軸を、他方に外輪と内輪とを含むベ
アリングを固設して、該ベアリングの嵌合孔に対して該
心合せ軸を摺動可能に嵌合するようにした弾性継手構造
において、前記ベアリングにおける内輪の内周面側に円
筒状の弾性体層を固着・形成するとともに、更に該弾性
体層の内周面側に該弾性体とは異層となる潤滑層を形成
し、該潤滑層の内面を嵌合面として前記心合せ軸を該嵌
合面に摺動可能に嵌合するように成したことにある。
(Means for Solving the Problems) The present invention has been made to solve such problems, and its gist is to connect a propeller shaft to a mating member via a rubber coupling and An elastic joint structure in which a centering shaft is fixedly installed on one side and a bearing including an outer ring and an inner ring is fixedly installed on the other side, and the centering shaft is slidably fitted in a fitting hole of the bearing. In the bearing, a cylindrical elastic body layer is fixedly formed on the inner peripheral surface side of the inner ring of the bearing, and a lubricating layer different from the elastic body is further formed on the inner peripheral surface side of the elastic body layer. The centering shaft is slidably fitted on the fitting surface with the inner surface of the lubricating layer as the fitting surface.

(作用及び考案の効果) 本考案の弾性継手構造においては、プロペラシャフトと
相手部材との心合せ機構部に半径方向の力が加わったと
き、ベアリングにおける弾性体層の弾性変形作用によ
り、心合せ軸とベアリングとの嵌合面(摺動面)の面圧
の増大が抑制される。しかもその弾性体層の内周面側に
は潤滑層が形成されていて、その潤滑層内面に対して心
合せ軸が嵌合されているため、即ちベアリングと心合せ
軸との摺動抵抗が低く抑えられ、両者が軸方向に円滑に
相対運動できるため、上記心合せ機構部において半径方
向に力が加わった場合も、プロペラシャフト又は相手部
材の軸方向振動等が良好に遮断され、その軸方向振動等
が一方から他方に又はその逆方向に伝達されるのが効果
的に防止される。
(Operation and Effect of Invention) In the elastic joint structure of the present invention, when a radial force is applied to the alignment mechanism portion between the propeller shaft and the mating member, the elastic deformation of the elastic layer in the bearing causes the alignment. An increase in surface pressure on the fitting surface (sliding surface) between the shaft and the bearing is suppressed. Moreover, since the lubricating layer is formed on the inner peripheral surface side of the elastic layer and the centering shaft is fitted to the inner surface of the lubricating layer, that is, the sliding resistance between the bearing and the centering shaft is reduced. Since they are suppressed to a low level and they can smoothly move relative to each other in the axial direction, even if a force is applied in the radial direction in the centering mechanism section, the axial vibration of the propeller shaft or the mating member is well blocked and Directional vibrations, etc. are effectively prevented from being transmitted from one to the other or vice versa.

本考案においては、弾性体層の内周面側に形成された潤
滑層が弾性体層を保護する機能も有する。
In the present invention, the lubricating layer formed on the inner peripheral surface side of the elastic layer also has a function of protecting the elastic layer.

即ち、直接心合せ軸が弾性体層の内周面に嵌入した場
合、両者の相対運動に基づいて弾性体層が摩耗,損傷し
易いが、潤滑層があるためにこれが抑制される利点が得
られるのである。
That is, when the centering shaft is directly fitted to the inner peripheral surface of the elastic body layer, the elastic body layer is easily worn and damaged due to the relative movement of the two, but there is an advantage that this is suppressed because of the lubricating layer. Be done.

(実施例) 次に本考案の実施例を図面に基づいて詳しく説明する。(Example) Next, the Example of this invention is described in detail based on drawing.

第1図において、10及び12はプロペラシャフト及び滑り
継手のスリーブで、夫々ヨーク部14及び16を有し、それ
らヨーク部14,16がラバーカップリング18を介して互い
に連結されている。ラバーカップリング18は、第3図に
示しているように全体としてリング形状を成しており、
内部に補強糸束20が埋設されている。また円周方向に沿
って所定間隔毎に複数の取付穴22が設けられており、こ
れら取付穴22において、上記プロペラシャフト10及びス
リーブ12の各ヨーク部14,16がボルト24及びナット26に
より交互に固定されている。
In FIG. 1, 10 and 12 are sleeves of a propeller shaft and a slide joint, which have yoke portions 14 and 16, respectively, and these yoke portions 14 and 16 are connected to each other via a rubber coupling 18. The rubber coupling 18 has a ring shape as a whole as shown in FIG.
A reinforcing yarn bundle 20 is embedded inside. Further, a plurality of mounting holes 22 are provided at predetermined intervals along the circumferential direction, and the yoke portions 14 and 16 of the propeller shaft 10 and the sleeve 12 are alternated by bolts 24 and nuts 26 in the mounting holes 22. It is fixed to.

スリーブ12の端部には、ベアリング(自動調心ベアリン
グ)30が固設されている。このベアリング30は、第2図
に詳しく示しているように外輪32と内輪34とを含んでい
る。外輪32及び内輪34は夫々球面状の嵌合部36,38を有
しており、それら嵌合面36,38において外輪32及び内輪3
4が互いに摺動可能に嵌合されている。即ち内輪34が、
嵌合面36,38において外輪32により回転可能に保持され
ている。
A bearing (self-aligning bearing) 30 is fixed to the end of the sleeve 12. The bearing 30 includes an outer ring 32 and an inner ring 34 as shown in detail in FIG. The outer ring 32 and the inner ring 34 have spherical fitting portions 36 and 38, respectively, and the outer ring 32 and the inner ring 3 are fitted to the fitting surfaces 36 and 38, respectively.
4 are slidably fitted together. That is, the inner ring 34
The fitting surfaces 36 and 38 are rotatably held by the outer ring 32.

内輪34の内周面側には、円筒状のゴム弾性体層40が固着
・形成されており、更にこのゴム弾性体層40の内周面側
には四フッ化エチレン繊維より成る潤滑層42が形成され
ている。
A cylindrical rubber elastic body layer 40 is fixed and formed on the inner peripheral surface side of the inner ring 34, and a lubricating layer 42 made of tetrafluoroethylene fiber is further formed on the inner peripheral surface side of the rubber elastic body layer 40. Are formed.

一方前記プロペラシャフト10の側には、心合せ軸44がそ
の端部部材46に固設されており、この心合せ軸44が上記
潤滑層42の内周面に摺動可能に嵌合され、以てスリーブ
12とプロペラシャフト10との心合せが行なわれている。
On the other hand, on the side of the propeller shaft 10, a centering shaft 44 is fixedly mounted on the end member 46, and the centering shaft 44 is slidably fitted to the inner peripheral surface of the lubricating layer 42, With sleeve
12 and propeller shaft 10 are being aligned.

尚、ベアリング30におけるゴム弾性体層40及び潤滑層42
は、具体的には次のようにして形成することができる。
即ち内側に四フッ化エチレン繊維の層を、外側にポリエ
ステル等ゴムと接着する繊維の層を有する2層構造の布
を容易し、これを所定心体に巻いて上記ベアリング30と
共に加硫金型内にセットし、ゴム材料を例えばベアリン
グ30に形成した注入口48より注入して成形し、その後成
形体を金型より取り出して心体を成形品より抜き出せば
良い。
The rubber elastic layer 40 and the lubrication layer 42 in the bearing 30
Can be specifically formed as follows.
That is, it is easy to fabricate a two-layer structure having an inner layer of tetrafluoroethylene fiber and an outer layer of fiber that adheres to rubber such as polyester, which is wound around a predetermined core body and vulcanization mold together with the bearing 30. For example, a rubber material may be set inside and injected from an injection port 48 formed in the bearing 30 to be molded, and then the molded body may be taken out of the mold and the core body may be extracted from the molded product.

以上のように構成された本例の弾性継手においては、ス
リーブ12とプロペラシャフト10との心合せ部において、
具体的にはスリーブ12側のベアリング30と、プロペラシ
ャフト10側の心合せ軸44との嵌合部において半径方向の
力が作用した場合、ベアリング30におけるゴム弾性体層
40が弾性変形して心合せ軸44とベアリング30との嵌合面
の面圧増大を抑制する。またベアリング30と心合せ軸44
との嵌合部には四フッ化エチレン繊維の潤滑層42が形成
されていて摺動抵抗が極力低く抑えられているため、こ
れらベアリング30と心合せ軸44との摺動抵抗に基づく振
動の伝達が抑制される。
In the elastic joint of the present example configured as described above, in the centering portion between the sleeve 12 and the propeller shaft 10,
Specifically, when a radial force acts on the fitting portion of the bearing 30 on the sleeve 12 side and the centering shaft 44 on the propeller shaft 10 side, the rubber elastic layer of the bearing 30 is applied.
The elastic deformation of 40 suppresses an increase in the surface pressure of the fitting surface between the centering shaft 44 and the bearing 30. Also, the bearing 30 and the centering shaft 44
Since the lubricating layer 42 of ethylene tetrafluoride fiber is formed in the fitting portion with and the sliding resistance is suppressed as low as possible, the vibration due to the sliding resistance between the bearing 30 and the centering shaft 44 is suppressed. Transmission is suppressed.

以上本考案の実施例を詳述したが、本考案はその他の形
態で構成することも可能である。
Although the embodiments of the present invention have been described in detail above, the present invention can be configured in other forms.

例えばベアリングにおける内輪の内周面側に形成したゴ
ム弾性体層に代えて樹脂の弾性体層を形成することも可
能であるし、上記潤滑層を四フッ化エチレン繊維以外の
四フッ化エチレン樹脂等材料で形成することも可能であ
る。
For example, instead of the rubber elastic layer formed on the inner peripheral surface side of the inner ring of the bearing, it is possible to form an elastic layer of resin, and the lubricating layer is a tetrafluoroethylene resin other than tetrafluoroethylene fiber. It is also possible to form the same material.

その他、上例は本考案をプロペラシャフトとスリーブと
を連結する弾性継手に適用した場合の例であるが、本考
案はこれをプロペラシャフトとデファレンシャル装置と
を連結する弾性継手に対して適用することも可能である
など、その主旨を逸脱しない範囲において、様々な変更
を加えた形態で構成可能である。
In addition, the above example is an example in which the present invention is applied to an elastic joint that connects a propeller shaft and a sleeve, but the present invention should be applied to an elastic joint that connects a propeller shaft and a differential device. It is also possible to configure in a form in which various changes are made without departing from the spirit of the invention.

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

第1図は本考案の一実施例である弾性継手構造の断面図
であり、第2図は第1図の要部の拡大断面図、第3図
(A)は第1図におけるラバーカップリングの正面図、
第3図(B)は第3図(A)のIIIB−IIIB断面図、第4
図は従来の弾性継手構造の断面図である。 10……プロペラシャフト 12……スリーブ 18……ラバーカップリング 30……ベアリング 32……外輪、34……内輪 40……弾性体層、42……潤滑層
FIG. 1 is a cross-sectional view of an elastic joint structure which is an embodiment of the present invention, FIG. 2 is an enlarged cross-sectional view of an essential part of FIG. 1, and FIG. 3 (A) is a rubber coupling in FIG. Front view of the
FIG. 3B is a sectional view taken along the line IIIB-IIIB in FIG.
The figure is a cross-sectional view of a conventional elastic joint structure. 10 …… Propeller shaft 12 …… Sleeve 18 …… Rubber coupling 30 …… Bearing 32 …… Outer ring, 34 …… Inner ring 40 …… Elastic layer, 42 …… Lubrication layer

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 【請求項1】プロペラシャフトをラバーカップリングを
介して相手部材に連結するとともに、それらの何れか一
方に心合せ軸を、他方に外輪と内輪とを含むベアリング
を固設して、該ベアリングの嵌合孔に対して該心合せ軸
を摺動可能に嵌合するようにした弾性継手構造におい
て、 前記ベアリングにおける内輪の内周面側に円筒状の弾性
体層を固着・形成するとともに、更に該弾性体層の内周
面側に該弾性体とは異層となる潤滑層を形成し、該潤滑
層の内面を嵌合面として前記心合せ軸を該嵌合面に摺動
可能に嵌合するように成したことを特徴とするプロペラ
シャフトの弾性継手構造。
1. A propeller shaft is connected to a mating member via a rubber coupling, a centering shaft is fixed to one of the propeller shafts, and a bearing including an outer ring and an inner ring is fixed to the other of the propeller shafts. In an elastic joint structure in which the centering shaft is slidably fitted in a fitting hole, a cylindrical elastic layer is fixed and formed on the inner peripheral surface side of the inner ring of the bearing, and A lubricating layer, which is different from the elastic body, is formed on the inner peripheral surface side of the elastic body layer, and the centering shaft is slidably fitted on the fitting surface with the inner surface of the lubricating layer as the fitting surface. An elastic joint structure for a propeller shaft, characterized in that they are made to fit together.
JP1989062285U 1989-05-29 1989-05-29 Elastic joint structure Expired - Lifetime JPH0643544Y2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1989062285U JPH0643544Y2 (en) 1989-05-29 1989-05-29 Elastic joint structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1989062285U JPH0643544Y2 (en) 1989-05-29 1989-05-29 Elastic joint structure

Publications (2)

Publication Number Publication Date
JPH031322U JPH031322U (en) 1991-01-09
JPH0643544Y2 true JPH0643544Y2 (en) 1994-11-14

Family

ID=31591291

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1989062285U Expired - Lifetime JPH0643544Y2 (en) 1989-05-29 1989-05-29 Elastic joint structure

Country Status (1)

Country Link
JP (1) JPH0643544Y2 (en)

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4212408Y1 (en) * 1965-02-19 1967-09-29
JPS6149143U (en) * 1984-09-05 1986-04-02

Also Published As

Publication number Publication date
JPH031322U (en) 1991-01-09

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