JP2521695Y2 - Propeller shaft - Google Patents

Propeller shaft

Info

Publication number
JP2521695Y2
JP2521695Y2 JP6925591U JP6925591U JP2521695Y2 JP 2521695 Y2 JP2521695 Y2 JP 2521695Y2 JP 6925591 U JP6925591 U JP 6925591U JP 6925591 U JP6925591 U JP 6925591U JP 2521695 Y2 JP2521695 Y2 JP 2521695Y2
Authority
JP
Japan
Prior art keywords
spline shaft
shaft portion
hole
male
spline
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 - Fee Related
Application number
JP6925591U
Other languages
Japanese (ja)
Other versions
JPH0514624U (en
Inventor
淳之 生川
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.)
Matsui Manufacturing Co Ltd
Original Assignee
Matsui Manufacturing 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 Matsui Manufacturing Co Ltd filed Critical Matsui Manufacturing Co Ltd
Priority to JP6925591U priority Critical patent/JP2521695Y2/en
Publication of JPH0514624U publication Critical patent/JPH0514624U/en
Application granted granted Critical
Publication of JP2521695Y2 publication Critical patent/JP2521695Y2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

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  • Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)

Description

【考案の詳細な説明】[Detailed description of the device]

【0001】[0001]

【産業上の利用分野】本考案は、雌形スプライン軸部
と、この雌形スプライン軸部に対して相対回転不能かつ
軸線方向に摺動可能にスプライン挿入嵌合する雄形スプ
ライン軸部とよりなるプロペラシャフトに関するもので
ある。
BACKGROUND OF THE INVENTION The present invention comprises a female spline shaft portion and a male spline shaft portion which is relatively non-rotatable with respect to the female spline shaft portion and which is fitted into the spline so as to be slidable in the axial direction. It relates to a propeller shaft.

【0002】[0002]

【従来の技術】従来のこのようなプロペラシャフトにお
いては、図4に示したように、雄形スプライン軸部1が
背圧を受けることなく、外側の雌形スプライン軸部8の
スプライン軸孔9内に進入することができるよう、スプ
ライン軸孔9の軸線方向の雌形スプライン軸部8の先端
側とは反対側の端部を小通気孔15を介して大気と連通す
る。またこの雌形スプライン軸部8の外部に潤滑グリー
ス注入用のニップル16を設け、このニップル16から雌形
スプラインに設けた給油孔17を介して雄形スプラインと
のスプライン噛合面に潤滑グリースを供給していた。
2. Description of the Related Art In such a conventional propeller shaft, as shown in FIG. 4, the male spline shaft portion 1 does not receive back pressure and the outer female spline shaft portion 8 has a spline shaft hole 9 The end portion of the spline shaft hole 9 opposite to the tip end side of the female spline shaft portion 8 in the axial direction is communicated with the atmosphere through the small vent hole 15 so that the spline shaft hole 9 can enter the inside. Further, a nipple 16 for injecting lubricating grease is provided outside the female spline shaft portion 8, and lubricating grease is supplied from this nipple 16 to a spline engagement surface with a male spline through an oil supply hole 17 provided in the female spline. Was.

【0003】[0003]

【考案が解決しようとする課題】しかし、従来のこのよ
うなプロペラシャフトにおいては、スプライン軸孔の軸
線方向の雌形スプライン軸部の先端側とは反対側の端部
を小通気孔を介して大気と連通しているため、この小通
気孔から潤滑グリースが徐々に漏れ、長時間の使用後に
油切れを起こし、グリース再充填作業が必要となる。ま
たスプライン噛合面がスプライン軸孔及び小通気孔を介
して直接外気に連通しているため、水やほこりが進入
し、さびやよごれを生ずる恐れがある。
However, in such a conventional propeller shaft, the end of the female spline shaft portion in the axial direction of the spline shaft hole on the side opposite to the tip side is provided with a small vent hole. Since it is in communication with the atmosphere, the lubricating grease gradually leaks from the small vents, runs out of oil after long-term use, and grease refilling work is required. Further, since the spline meshing surface communicates directly with the outside air through the spline shaft hole and the small ventilation hole, water or dust may enter and cause rust or dirt.

【0004】従って、本考案の目的は、スプライン噛合
面への再給油作業が不要であり、またスプライン噛合面
にさびやよごれを発生しないようにするプロペラシャフ
トを得るにある。
Therefore, an object of the present invention is to obtain a propeller shaft that does not require re-lubrication work on the spline meshing surface and prevents rust and dirt from occurring on the spline meshing surface.

【0005】[0005]

【課題を解決するための手段】この目的を達成するた
め、本考案プロペラシャフトは、雄形スプライン軸部に
この雄形スプライン軸部に対して同軸状の内部孔を設
け、この内部孔内にピストン素子を摺動自在に配置し、
前記内部孔の軸線方向の雄形スプライン軸部の先端側と
は反対側の端部を小通気孔を介して大気と連通したこと
を特徴とする。
In order to achieve this object, the propeller shaft of the present invention has a male spline shaft portion provided with an internal hole coaxial with the male spline shaft portion. The piston element is slidably arranged,
It is characterized in that the end of the internal hole opposite to the tip side of the male spline shaft in the axial direction is communicated with the atmosphere through a small vent hole.

【0006】[0006]

【作用】本考案のこの構成によれば、ピストン素子は、
内部孔の軸線方向の雄形スプライン軸部の先端側とは反
対側の端部が小通気孔を介して大気と連通しているた
め、スプライン軸部相互の抜差摺動時の内圧変化を内部
孔内での移動により吸収する。従って、スプライン軸部
相互は抵抗なく抜差摺動することができる。
According to this structure of the present invention, the piston element is
Since the end of the internal hole in the axial direction opposite to the tip side of the male spline shaft communicates with the atmosphere through the small ventilation hole, the internal pressure change during sliding sliding between the spline shafts Absorbs due to movement within the internal pores. Therefore, the spline shaft portions can slide and slide without resistance.

【0007】更に、本考案によれば、雄形スプラインの
内部孔に配置したピストン素子は、雌形スプライン軸部
のスプライン軸孔を、直接大気に連通させることなく、
大気から遮断する。
Further, according to the present invention, the piston element arranged in the inner hole of the male spline has the spline shaft hole of the female spline shaft portion without directly communicating with the atmosphere.
Shut off from the atmosphere.

【0008】[0008]

【実施例】次に、図面につき本考案の好適な実施例を説
明する。
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT A preferred embodiment of the present invention will now be described with reference to the drawings.

【0009】図1は、本考案プロペラシャフトの第1実
施例の線図的縦断面を示し、この実施例においては、雄
形スプライン軸部1に、先端部1aから二股ヨーク2の内
部底面まで貫通する内部孔3を設ける。二股ヨーク2の
内部底面には、閉鎖キャップ4を設け、この閉鎖キャッ
プ4に小通気孔5を設ける。内部孔3には、細長いコッ
プ状のピストン素子6を配置し、雄形スプライン軸部の
先端に近接する側の端部にフランジ6aを設ける。内部孔
3の雄形スプライン軸部の先端部1aの内面にはオイルシ
ール7を設ける。
FIG. 1 shows a schematic longitudinal section of a first embodiment of a propeller shaft of the present invention, in which the male spline shaft portion 1 extends from the tip portion 1a to the inner bottom surface of the forked yoke 2. An internal hole 3 that penetrates is provided. A closing cap 4 is provided on the inner bottom surface of the bifurcated yoke 2, and a small vent hole 5 is provided in the closing cap 4. An elongated cup-shaped piston element 6 is arranged in the internal hole 3, and a flange 6a is provided at the end portion of the male spline shaft portion on the side close to the tip. An oil seal 7 is provided on the inner surface of the tip portion 1a of the male spline shaft portion of the inner hole 3.

【0010】雌形スプライン軸部8のスプライン軸孔9
の奥端部9aには通気孔を設けず、スプライン軸孔9のス
プライン内面にグリースを塗布するか、又はスプライン
軸孔9の内部に潤滑油を充填しておく。この後、ピスト
ン素子6を装着した雄形スプライン軸部1をスプライン
軸孔9に挿入嵌合し、雌形スプライン軸部8の先端部に
おいてスプライン軸孔9をオイルシール10によりシール
する。
Spline shaft hole 9 of female spline shaft portion 8
No vent hole is provided in the rear end portion 9a of the spline shaft, and grease is applied to the inner surface of the spline shaft hole 9 or the inside of the spline shaft hole 9 is filled with lubricating oil. Thereafter, the male spline shaft portion 1 having the piston element 6 mounted therein is inserted and fitted into the spline shaft hole 9, and the spline shaft hole 9 is sealed by the oil seal 10 at the tip of the female spline shaft portion 8.

【0011】雄形スプライン軸部1がスプライン軸孔9
の奥端部9aに向かって前進するとき、雄形スプライン軸
部1の先端部1aとスプライン軸孔9の奥端部9aとの間の
閉塞空間11に存在する空気は圧縮されて圧力が高くなろ
うとするが、雄形スプライン軸部1の内部孔3の大気連
通空間12の空気が小通気孔5を経て排気され、ピストン
素子6が雄形スプライン軸部1の内部孔3内に後退する
ことにより、閉塞空間11内の圧力が一定に維持され、雄
形スプライン軸部1は、抵抗なくスプライン軸孔9の奥
端部9aに向かって前進することができる。
The male spline shaft portion 1 has a spline shaft hole 9
When advancing toward the rear end portion 9a of the male spline shaft portion 1, the air existing in the closed space 11 between the front end portion 1a of the male spline shaft portion 1 and the rear end portion 9a of the spline shaft hole 9 is compressed and the pressure becomes high. However, the air in the atmosphere communicating space 12 in the inner hole 3 of the male spline shaft portion 1 is exhausted through the small vent hole 5, and the piston element 6 retracts into the inner hole 3 of the male spline shaft portion 1. As a result, the pressure in the closed space 11 is maintained constant, and the male spline shaft portion 1 can advance toward the rear end portion 9a of the spline shaft hole 9 without resistance.

【0012】また、雄形スプライン軸部1がスプライン
軸孔9の奥端部9aから離れる方向に後退するとき、雄形
スプライン軸部1の内部孔3の大気連通空間11に小通気
孔5を経て空気が吸入され、ピストン素子6が雄形スプ
ライン軸部1の内部孔3から突出移動することにより、
閉塞空間12内の圧力は一定に維持され、雄形スプライン
軸部1は、抵抗なくスプライン軸孔9の奥端部9aから離
れる方向に後退することができる。
When the male spline shaft portion 1 retracts in the direction away from the inner end 9a of the spline shaft hole 9, a small vent hole 5 is formed in the atmosphere communication space 11 of the inner hole 3 of the male spline shaft portion 1. Air is sucked in through the piston element 6 and the piston element 6 projects from the internal hole 3 of the male spline shaft portion 1,
The pressure in the closed space 12 is maintained constant, and the male spline shaft portion 1 can be retracted in a direction away from the inner end portion 9a of the spline shaft hole 9 without resistance.

【0013】雄形スプライン軸部1の先端部1aとスプラ
イン軸孔9の奥端部9aとの間の閉塞空間11は、ピストン
素子6により大気連通空間12から遮断されているため、
スプライン噛合面の潤滑グリース又は潤滑油は小通気孔
5から漏れることはなく、従来のプロペラシャフトのよ
うに、潤滑油の再充填作業は不要となり、メインテナン
スフリーとなり、スプライン噛合面のさび、よごれの発
生はなくなる。
Since the closed space 11 between the tip portion 1a of the male spline shaft portion 1 and the rear end portion 9a of the spline shaft hole 9 is cut off from the atmosphere communication space 12 by the piston element 6,
Lubricating grease or lubricating oil on the spline meshing surface does not leak from the small air holes 5, and unlike conventional propeller shafts, there is no need to refill the lubricating oil, maintenance is free, and rust and dirt on the spline meshing surface are eliminated. Outbreak disappears.

【0014】図2は、本考案プロペラシャフトの第2の
実施例の線図的縦断面を示し、この実施例においては、
コップ状ピストン素子6及びオイルシール7を設けるの
代わりに鼓形のオイルシールピストン60を設け、このオ
イルシールピストン60が内部孔3から抜け出るのを防止
するストップリング13を内部孔3の両端の近傍に設けた
点が異なるだけでその他は第1の実施例と同一である。
FIG. 2 shows a schematic longitudinal section of a second embodiment of the propeller shaft according to the present invention. In this embodiment,
Instead of providing the cup-shaped piston element 6 and the oil seal 7, a drum-shaped oil seal piston 60 is provided, and stop rings 13 for preventing the oil seal piston 60 from coming out of the inner hole 3 are provided near both ends of the inner hole 3. The third embodiment is the same as the first embodiment except that the second embodiment is different.

【0015】図3は、本考案プロペラシャフトの第3の
実施例の線図的縦断面を示し、この実施例においては、
雄形スプライン軸部1に設ける内部孔3を貫通孔とはせ
ず、スプラインの歯が先端に向かって形成されるスプラ
イン部の近傍まで形成した盲孔とし、この盲内部孔3の
奥端の近傍から雄形スプライン軸部1に半径方向にスプ
ラインの谷部に貫通する半径方向孔14を周方向に互いに
等間隔離して複数個設けた点が異なるだけで、他の点は
図2の第2の実施例と同一である。
FIG. 3 shows a schematic longitudinal section of a third embodiment of the propeller shaft according to the present invention. In this embodiment,
The inner hole 3 provided in the male spline shaft portion 1 is not a through hole, but a blind hole formed up to the vicinity of the spline portion where the teeth of the spline are formed toward the tip. 2 is different from that shown in FIG. 2 only in that a plurality of radial holes 14 penetrating radially from the vicinity to the male spline shaft portion 1 in the valley portion of the spline are provided at equal intervals in the circumferential direction. This is the same as the second embodiment.

【0016】図3の第3の実施例の場合、雄形スプライ
ン軸部1と雌形スプライン軸部8のスプライン噛合面に
おける僅かなクリアランスが潤滑油経路を形成し、スプ
ライン軸部相互の抜き差し摺動による吸引及び押し出し
により潤滑油がスプライン噛合面を流動して潤滑を行
い、潤滑が効率よく行われる。
In the case of the third embodiment shown in FIG. 3, a slight clearance between the male spline shaft portion 1 and the female spline shaft portion 8 at the spline meshing surface forms a lubricating oil passage, and the spline shaft portions are mutually inserted and removed. Lubricating oil flows through the spline meshing surface and is lubricated by dynamic suction and extrusion, so that lubrication is efficiently performed.

【0017】[0017]

【考案の効果】以上説明したように、スプライン摺動時
における内圧変化を吸収し、内圧を一定に保つことによ
り、摺動抵抗を軽減し、シールの安定化、潤滑油保持特
性を向上し、スプライン噛合面への再給油作業が不要で
あり、またスプライン噛合面にさびやよごれを発生しな
いメインテナンスフリーの構造が得られるという効果が
得られる。
[Effects of the Invention] As described above, by absorbing the internal pressure change during the spline sliding and keeping the internal pressure constant, the sliding resistance is reduced, the seal is stabilized, and the lubricating oil retention characteristic is improved. There is no need for re-lubrication work on the spline meshing surface, and there is an effect that a maintenance-free structure that does not cause rust or dirt on the spline meshing surface can be obtained.

【0018】更に、潤滑油経路をスプライン噛合面とす
る実施例の場合、潤滑効率が極めて良好となり、歯面へ
の油切れを無くし、焼き付けを完全に防止することがで
きるという効果が得られる。
Furthermore, in the case of the embodiment in which the lubricating oil path is the spline meshing surface, the lubricating efficiency is extremely good, and it is possible to obtain the effect that oil running out on the tooth surface can be eliminated and seizure can be completely prevented.

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

【図1】本考案によるプロペラシャフトの第1の実施例
の一部切除して断面を示す側面図である。
FIG. 1 is a partially cutaway side view of a first embodiment of a propeller shaft according to the present invention.

【図2】本考案によるプロペラシャフトの第2の実施例
の一部切除して断面を示す側面図である。
FIG. 2 is a partially cutaway side view of a second embodiment of a propeller shaft according to the present invention.

【図3】本考案によるプロペラシャフトの第3の実施例
の一部切除して断面を示す側面図である。
FIG. 3 is a side view showing a partially cutaway cross section of a third embodiment of a propeller shaft according to the present invention.

【図4】従来のプロペラシャフトの線図的説明図であ
る。
FIG. 4 is a diagrammatic explanatory view of a conventional propeller shaft.

【符号の説明】[Explanation of symbols]

1 雄形スプライン軸部 2 二股ヨーク 3 内部孔 4 閉鎖キャップ 5 小通気孔 6,60 ピストン素子 6a フランジ 7,10 オイルシール 8 雌形スプライン軸部 9 スプライン軸孔 9a 奥端部 11 閉塞空間 12 大気連通空間 13 ストップリング 14 半径方向孔 1 Male Spline Shaft 2 Bifurcated Yoke 3 Inner Hole 4 Closing Cap 5 Small Vent 6,60 Piston Element 6a Flange 7,10 Oil Seal 8 Female Spline Shaft 9 Spline Shaft 9a Back End 11 Closed Space 12 Atmosphere Communication space 13 Stop ring 14 Radial hole

Claims (1)

(57)【実用新案登録請求の範囲】(57) [Scope of utility model registration request] 【請求項1】雌形スプライン軸部と、この雌形スプライ
ン軸部に対して相対回転不能かつ軸線方向に摺動可能に
スプライン挿入嵌合する雄形スプライン軸部とよりなる
プロペラシャフトにおいて、前記雄形スプライン軸部に
この雄形スプライン軸部に対して同軸状の内部孔を設
け、この内部孔内にピストン素子を摺動自在に配置し、 前記内部孔の軸線方向の雄形スプライン軸部の先端側と
は反対側の端部を小通気孔を介して大気と連通したこと
を特徴とするプロペラシャフト。
1. A propeller shaft comprising a female spline shaft portion and a male spline shaft portion which is non-rotatable relative to the female spline shaft portion and is spline-inserted into the female spline shaft portion so as to be slidable in the axial direction. The male spline shaft portion is provided with an internal hole coaxial with the male spline shaft portion, and the piston element is slidably arranged in the internal hole, and the male spline shaft portion in the axial direction of the internal hole is provided. The propeller shaft is characterized in that the end portion on the side opposite to the tip side of the is communicated with the atmosphere through a small ventilation hole.
JP6925591U 1991-08-06 1991-08-06 Propeller shaft Expired - Fee Related JP2521695Y2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP6925591U JP2521695Y2 (en) 1991-08-06 1991-08-06 Propeller shaft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP6925591U JP2521695Y2 (en) 1991-08-06 1991-08-06 Propeller shaft

Publications (2)

Publication Number Publication Date
JPH0514624U JPH0514624U (en) 1993-02-26
JP2521695Y2 true JP2521695Y2 (en) 1996-12-25

Family

ID=13397436

Family Applications (1)

Application Number Title Priority Date Filing Date
JP6925591U Expired - Fee Related JP2521695Y2 (en) 1991-08-06 1991-08-06 Propeller shaft

Country Status (1)

Country Link
JP (1) JP2521695Y2 (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102014008719B3 (en) * 2014-06-18 2015-07-16 Ifa-Technologies Gmbh Connection arrangement for axial securing a shaft-hub connection and method for axial securing a shaft-hub connection
JP6367659B2 (en) * 2014-09-18 2018-08-01 日立オートモティブシステムズ株式会社 Power transmission shaft and vehicle propeller shaft
JP6497997B2 (en) * 2015-03-19 2019-04-10 日立オートモティブシステムズ株式会社 Power transmission shaft
US11053983B2 (en) * 2018-01-19 2021-07-06 The Boeing Company Torque tube assemblies for use with aircraft high lift devices
US11060566B2 (en) 2018-01-19 2021-07-13 The Boeing Company Apparatus and methods for rigging a torque tube assembly in an aircraft
CN114233742B (en) * 2021-12-16 2023-03-24 北京动力机械研究所 Segmented shaft transmission structure based on flexible spline connection

Also Published As

Publication number Publication date
JPH0514624U (en) 1993-02-26

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