JPH09303555A - Piston - Google Patents

Piston

Info

Publication number
JPH09303555A
JPH09303555A JP12578896A JP12578896A JPH09303555A JP H09303555 A JPH09303555 A JP H09303555A JP 12578896 A JP12578896 A JP 12578896A JP 12578896 A JP12578896 A JP 12578896A JP H09303555 A JPH09303555 A JP H09303555A
Authority
JP
Japan
Prior art keywords
piston
stress
pin
dispersing
recesses
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
JP12578896A
Other languages
Japanese (ja)
Inventor
Katsunari Matsumoto
克成 松本
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.)
Toyota Motor Corp
Original Assignee
Toyota 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 Toyota Motor Corp filed Critical Toyota Motor Corp
Priority to JP12578896A priority Critical patent/JPH09303555A/en
Publication of JPH09303555A publication Critical patent/JPH09303555A/en
Pending legal-status Critical Current

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  • Pistons, Piston Rings, And Cylinders (AREA)

Abstract

PROBLEM TO BE SOLVED: To improve the reliability of a piston. SOLUTION: The end edges 122 and 132 opposing to the pin holes 121 and 131 of a pin bosses 12 and 13 which are formed at the inner side of a piston 11 are inclined to separate each other as withdrawing from the top surface 111 of the piston. At the positions 16 and 17 at the end edges 122 and 132 at the piston top surface 111 side, recesses 18 and 19 for stress dispersion are provided. The recesses 18 and 19 for stress dispersion are formed by cutting in the redial direction of the pin holes 121 and 131 from the pin holes 121 and 131, so as to cross with the end edges 122 and 132. The wall surfaces 181 and 191 of the recesses 18 and 19 for stress dispersion connecting to the pin holes 121 and 131 are made in curved surfaces reversing at the bottom side of the pin holes 121 and 131.

Description

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

【0001】[0001]

【発明の属する技術分野】本発明は、ピストンの内側に
形成された一対のピンボスのピン孔にピストンピンを貫
通するピストンに関するものである。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a piston having a pair of pin bosses formed inside a piston and having a piston pin penetrating through the pin hole.

【0002】[0002]

【従来の技術】この種の内燃機関用ピストンの例が実開
平6−22549号公報に開示されている。図7に示す
ように、ピストン10の内側に形成された一対のピンボ
ス12,13のピン孔121,131に貫通されたピス
トンピン14は、ピストンシリンダ内の爆発によってピ
ストン頂面101に爆発圧力を受ける。この爆発圧力は
ピストン10及びピストンピン14を介してピストンロ
ッド15に伝わる。
2. Description of the Related Art An example of this type of piston for an internal combustion engine is disclosed in Japanese Utility Model Laid-Open No. 6-22549. As shown in FIG. 7, the piston pin 14 penetrating through the pin holes 121 and 131 of the pair of pin bosses 12 and 13 formed inside the piston 10 causes the explosion pressure in the piston top surface 101 due to the explosion in the piston cylinder. receive. This explosion pressure is transmitted to the piston rod 15 via the piston 10 and the piston pin 14.

【0003】[0003]

【発明が解決しようとする課題】この爆発圧力の伝達の
際にはピストンピン14が鎖線で示すように撓み変形す
る。ピストンピン14の撓み変形は、ピン孔121,1
31の対向する端縁122,132におけるピストン頂
面101側の部位16,17とピストンピン14との間
で局部的に強い当たりをもたらす。この局部的な当たり
は線状に強く当たる状態であり、前記部位には強い引っ
張り応力が集中する。この集中した引っ張り応力は前記
部位16,17を起点とした亀裂をもたらす。
During the transmission of the explosion pressure, the piston pin 14 is flexibly deformed as shown by the chain line. The bending deformation of the piston pin 14 is caused by the pin holes 121, 1
A strong local hit is provided between the piston pin 14 and the portions 16 and 17 on the piston top surface 101 side of the opposed edges 122 and 132 of 31. This local contact is in a state of striking linearly strongly, and a strong tensile stress concentrates on the above-mentioned site. This concentrated tensile stress causes a crack starting from the portions 16 and 17.

【0004】本発明は、前記した亀裂の発生を防止して
ピストンの信頼性を向上することを目的とする。
An object of the present invention is to prevent the occurrence of the above-mentioned cracks and improve the reliability of the piston.

【0005】[0005]

【課題を解決するための手段】そのために請求項1の発
明では、ピストンの内側に形成された一対のピンボスの
ピン孔の対向する端縁におけるピストン頂面側の部位に
応力分散用凹部を設けた。
To this end, according to the first aspect of the present invention, a stress-dispersing concave portion is provided at a portion of the pair of pin bosses formed inside the piston on the side of the top surface of the piston at the opposing edge of the pin holes. It was

【0006】ピストンシリンダ内の爆発によって撓み変
形したピストンピンは、ピン孔の前記端縁におけるピス
トン頂面側の部位に強く当たるが、応力分散用凹部が前
記当たりによって発生する引っ張り応力を分散する。こ
の引っ張り応力を分散させる作用が前記部位における亀
裂の発生を防止する。
The piston pin flexibly deformed due to the explosion in the piston cylinder hits strongly against the piston top surface side portion of the end edge of the pin hole, but the stress distribution concave portion distributes the tensile stress generated by the hit. This action of dispersing the tensile stress prevents the occurrence of cracks at the above-mentioned site.

【0007】請求項2の発明では、端縁と交差するよう
にピン孔からピン孔の半径方向へ切り込んで応力分散用
凹部を形成し、ピン孔に連なる応力分散用凹部の壁面を
ピン孔の奥側で反転する曲面とした。
According to the second aspect of the present invention, the stress-dispersing recess is formed by cutting the pin hole in the radial direction of the pin hole so as to intersect with the end edge, and the wall surface of the stress-dispersing recess that is continuous with the pin hole is defined as the pin hole. The curved surface is inverted on the back side.

【0008】ピン孔の周面における応力分散用凹部の開
口縁は略U字形状となる。ピストンシリンダ内の爆発に
よって撓み変形したピストンピンがピン孔の前記端縁に
おけるピストン頂面側の部位に強く当たったとき、応力
分散用凹部が拡開変形する。略U字形状の壁面の反転部
位の曲面形状は、この拡開変形に伴う応力の分散に寄与
する。
The opening edge of the stress dispersion concave portion on the peripheral surface of the pin hole has a substantially U shape. When the piston pin flexibly deformed due to the explosion in the piston cylinder hits strongly against the piston top surface side portion of the end edge of the pin hole, the stress dispersion concave portion is expanded and deformed. The curved surface shape of the inverted portion of the substantially U-shaped wall surface contributes to the dispersion of the stress due to the expansion deformation.

【0009】請求項3の発明では、ピストン頂面から遠
ざかるにつれて互いに離間するように前記対向する端縁
を傾斜させ、ピン孔に連なる応力分散用凹部の壁面は、
ピン孔に対する応力分散用凹部の奥壁面から遠ざかるに
つれて拡開する形状とし、前記端縁のピストン頂面とは
反対側の部位よりもピストンピンの長手方向において対
向相手の応力分散用凹部側に近い位置に応力分散用凹部
を設けた。
According to the third aspect of the present invention, the wall surfaces of the stress-dispersing concave portions that are inclined with respect to each other and in which the facing edges are inclined so as to be separated from each other as they move away from the piston top surface,
The shape is such that it expands as it goes away from the inner wall surface of the stress distribution recess for the pin hole, and it is closer to the opposing stress distribution recess side in the longitudinal direction of the piston pin than the portion of the end edge opposite to the piston top surface. A concave portion for stress dispersion was provided at the position.

【0010】一般的に、ピストンは鋳型成形によって形
成されるが、前記端縁の傾斜形状、ピン孔に連なる応力
分散用凹部の壁面の形状及び応力分散用凹部の位置の前
記設定により応力分散用凹部の鋳型成形が可能となる。
Generally, the piston is formed by molding, but the inclination of the end edge, the shape of the wall surface of the stress dispersion concave portion connected to the pin hole, and the position of the stress dispersion concave portion are set for the stress dispersion. It becomes possible to mold the recess.

【0011】[0011]

【発明の実施の形態】以下、本発明を具体化した第1の
実施の形態を図1〜図4に基づいて説明する。なお、図
7と同じ構成部には同じ符号が付してある。
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS A first embodiment of the present invention will be described below with reference to FIGS. The same components as those in FIG. 7 are designated by the same reference numerals.

【0012】図1(a)に示すように、ピストン11の
内側に形成されたピンボス12,13のピン孔121,
131の対向する端縁122,132は、ピストン頂面
111から遠ざかるにつれて互いに離間するように傾斜
している。図1(b)に示すように各端縁122,13
2におけるピストン頂面111側の部位16,17には
応力分散用凹部18,19が設けられている。
As shown in FIG. 1A, the pin holes 121, 13 of the pin bosses 12, 13 formed inside the piston 11 are
Opposing edges 122 and 132 of 131 are inclined so as to be separated from each other as the distance from the piston top surface 111 increases. As shown in FIG. 1 (b), each edge 122, 13
In portions 16 and 17 of the piston 2 on the piston top surface 111 side, stress dispersion recesses 18 and 19 are provided.

【0013】応力分散用凹部18,19は、端縁12
2,132と交差するようにピン孔121,131から
ピン孔121,131の半径方向へ切り込み形成されて
いる。ピン孔121,131に連なる応力分散用凹部1
8,19の壁面181,191は、ピン孔121,13
1の奥側で反転する曲面となっている。即ち、ピン孔1
21,131の周面における応力分散用凹部18,19
の開口縁183,193は略U字形状となっている。
The stress-dispersing recesses 18 and 19 are provided at the end edge 12.
It is formed by cutting from the pin holes 121 and 131 in the radial direction of the pin holes 121 and 131 so as to intersect with 2, 132. Stress-dispersing recess 1 connected to the pin holes 121 and 131
The wall surfaces 181, 191 of 8, 19 have pin holes 121, 13
It is a curved surface that is inverted on the back side of 1. That is, the pin hole 1
Stress-dispersing recesses 18, 19 on the peripheral surfaces of 21, 131
The opening edges 183 and 193 are substantially U-shaped.

【0014】応力分散用凹部18は、端縁122のピス
トン頂面111とは反対側の部位20よりもピストンピ
ン14の長手方向において対向相手の応力分散用凹部1
9側に近い位置にある。同様に、応力分散用凹部19
は、端縁132のピストン頂面111とは反対側の部位
21よりもピストンピン14の長手方向において対向相
手の応力分散用凹部18側に近い位置にある。そして、
ピン孔121,131に連なる応力分散用凹部18,1
9の壁面181,191は、ピン孔121,131に対
する応力分散用凹部18,19の奥壁面182,192
から遠ざかるにつれて拡開する形状にしてある。
The stress-dispersing recess 18 is opposed to the stress-dispersing recess 1 in the longitudinal direction of the piston pin 14 in the longitudinal direction of the piston pin 14 rather than the portion 20 of the end edge 122 opposite to the piston top surface 111.
It is located near the 9 side. Similarly, the stress dispersion recesses 19
Is closer to the opposing counterpart stress dispersion recess 18 side in the longitudinal direction of the piston pin 14 than the portion 21 of the end edge 132 opposite to the piston top surface 111. And
Stress dispersion recesses 18 and 1 connected to the pin holes 121 and 131
The wall surfaces 181 and 191 of the inner wall surface 181, 191 of the inner wall surface 182, 192 of the recesses 18, 19 for stress dispersion with respect to the pin holes 121, 131, respectively.
The shape is such that it expands as it moves away from it.

【0015】爆発圧力がピストン頂面111に作用した
とき、ピストンピン14が図2及び図3に鎖線で示すよ
うに撓み変位する。この撓み変位により応力分散用凹部
18,19が鎖線で示すように拡開変形する。
When the explosion pressure acts on the piston top surface 111, the piston pin 14 is flexibly displaced as shown by a chain line in FIGS. Due to this bending displacement, the stress-dispersing concave portions 18 and 19 are expanded and deformed as shown by a chain line.

【0016】図4の曲線Eは、応力分散用凹部18,1
9がある場合に部位16,17において生じる引っ張り
応力を表す。曲線Dは応力分散用凹部18,19がない
場合に部位16,17において生じる引っ張り応力を表
す。横軸は図2に示すピン孔121,131の周方向の
位置P1から位置P2に至る位置を表す。位置Q1,Q
2は開口縁183,193の位置を表す。縦軸は引っ張
り応力を表す。
A curve E in FIG. 4 is a stress dispersion concave portion 18, 1.
9 shows the tensile stress generated in the portions 16 and 17 when 9 is present. The curve D represents the tensile stress generated in the portions 16 and 17 when the stress dispersion recesses 18 and 19 are not provided. The horizontal axis represents the position from the position P1 in the circumferential direction of the pin holes 121 and 131 shown in FIG. 2 to the position P2. Position Q1, Q
2 indicates the positions of the opening edges 183 and 193. The vertical axis represents tensile stress.

【0017】第1の実施の形態では以下の効果が得られ
る。 (1-1)爆発圧力によって撓み変形したピストンピン1
4はピン孔121,131の端縁122,132におけ
るピストン頂面111側の部位16,17に強く当た
る。このとき、応力分散用凹部18,19が図2及び図
3に鎖線で示すように拡開変形し、ピストンピン14の
周面が拡開変形した開口縁183,193に沿って接す
る形となる。従って、応力分散用凹部18,19の存在
は、応力分散用凹部18,19がない場合に比べてピス
トンピン14の周面と端縁122,132との接触割合
を高め、図4の曲線Eで示すように引っ張り応力が分散
する。この引っ張り応力を分散させる作用がピストン頂
面111側の部位16,17における亀裂の発生を防止
する。その結果、ピストン11の信頼性が向上する。 (1-2)ピン孔121,131に連なる応力分散用凹部
18,19の壁面181,191をピン孔121,13
1の奥側で反転する曲面とした構成では、略U字形状の
壁面181,191の反転部位184,194の曲面形
状が応力分散用凹部18,19の拡開変形に伴う応力の
分散に寄与する。 (1-3)ピン孔121,131に連なる応力分散用凹部
18,19の壁面181,191は、ピン孔121,1
31に対する応力分散用凹部18,19の奥壁面18
2,192から遠ざかるにつれて拡開する形状にしてあ
る。このような拡開形状の応力分散用凹部18,19
は、ピストン頂面111から遠ざかるにつれて互いに離
間するように傾斜する端縁122,132のピストン頂
面111とは反対側の部位20,21よりもピストンピ
ン14の長手方向において対向相手の応力分散用凹部側
に近い位置に設けてある。従って、応力分散用凹部1
8,19から応力分散用凹部18,19に対応する鋳型
部分をピストン11の中心軸線Lの方向に抜き出すこと
ができ、ピストン11は応力分散用凹部18,19と共
に鋳型成形によって形成できる。応力分散用凹部18,
19を鋳型成形できる構成は、ピストン11の鋳型成形
後の応力分散用凹部18,19の加工形成を不要とし、
ピストン11の製作工程が簡素になる。又、応力分散用
凹部18,19の鋳型成形は応力分散用凹部18,19
の高精度形成をもたらす。
The following effects are obtained in the first embodiment. (1-1) Piston pin 1 flexed and deformed by explosive pressure
4 strongly hits the portions 16 and 17 of the end edges 122 and 132 of the pin holes 121 and 131 on the piston top surface 111 side. At this time, the stress-dispersing concave portions 18 and 19 are expanded and deformed as shown by a chain line in FIGS. 2 and 3, and the peripheral surface of the piston pin 14 is in contact with the expanded and deformed opening edges 183 and 193. . Therefore, the presence of the stress-dispersing recesses 18 and 19 increases the contact ratio between the peripheral surface of the piston pin 14 and the end edges 122 and 132 as compared with the case where the stress-dispersing recesses 18 and 19 are not present, and the curve E of FIG. The tensile stress is dispersed as shown by. This action of dispersing the tensile stress prevents the occurrence of cracks in the portions 16 and 17 on the piston top surface 111 side. As a result, the reliability of the piston 11 is improved. (1-2) The wall surfaces 181 and 191 of the stress-dispersing recesses 18 and 19 connected to the pin holes 121 and 131 are attached to the pin holes 121 and 13, respectively.
In the configuration in which the curved surface is inverted on the inner side of 1, the curved surface shapes of the inverted portions 184 and 194 of the substantially U-shaped wall surfaces 181 and 191 contribute to the dispersion of the stress associated with the expansion deformation of the stress distribution recesses 18 and 19. To do. (1-3) The wall surfaces 181 and 191 of the stress dispersion recesses 18 and 19 connected to the pin holes 121 and 131 are the pin holes 121 and 1, respectively.
The inner wall surface 18 of the stress dispersion recesses 18 and 19 with respect to 31
The shape is such that it spreads away from 2,192. The stress-dispersing recesses 18 and 19 having such an expanded shape
Is for the purpose of stress distribution of the opposing partner in the longitudinal direction of the piston pin 14 in the longitudinal direction of the end portions 122, 132 of the end edges 122, 132 which are inclined so as to separate from each other as they move away from the piston top surface 111. It is provided at a position close to the recess side. Therefore, the stress dispersion concave portion 1
The mold portions corresponding to the stress-dispersing recesses 18, 19 can be extracted in the direction of the central axis L of the piston 11 from 8, 8, and the piston 11 can be formed by molding together with the stress-dispersing recesses 18, 19. Stress dispersion recess 18,
The structure capable of molding 19 does not require the formation of the stress dispersion recesses 18 and 19 after molding the piston 11,
The manufacturing process of the piston 11 is simplified. In addition, the molding of the stress-dispersing recesses 18, 19 is performed by molding the stress-dispersing recesses 18, 19
Results in high precision formation.

【0018】次に、図5の第2の実施の形態を説明す
る。第1の実施の形態と同じ構成部には同じ符号が付し
てある。この実施の形態では、応力分散用凹部18,1
9の反転部位184,194は、端縁122,132の
ピストン頂面111とは反対側の部位20,21よりも
ピン孔121,131の奥側へ入り込んでいる。そし
て、応力分散用凹部18,19の拡開形状をそのままピ
ストン11の中心軸線Lの方向へ延長した形状の抜き溝
22,23が端縁122,132におけるピストン頂面
111とは反対側の部位20,21に形成されている。
抜き溝22,23の存在は、応力分散用凹部18,19
に対応する鋳型部分をピストン11の中心軸線Lの方向
に抜き出すことを可能にする。
Next, a second embodiment shown in FIG. 5 will be described. The same components as those in the first embodiment are denoted by the same reference numerals. In this embodiment, the stress dispersion recesses 18, 1
The reversal portions 184 and 194 of 9 enter the inner side of the pin holes 121 and 131 more than the portions 20 and 21 of the end edges 122 and 132 on the side opposite to the piston top surface 111. Then, the cutout grooves 22 and 23 in which the expanded shapes of the stress dispersion recesses 18 and 19 are extended in the direction of the central axis L of the piston 11 as they are are the end edges 122 and 132 on the side opposite to the piston top surface 111. 20 and 21 are formed.
The presence of the grooves 22 and 23 means that the stress-dispersing recesses 18 and 19
It is possible to pull out the mold part corresponding to the direction of the central axis L of the piston 11.

【0019】第2の実施の形態では以下の効果が得られ
る。 (2-1)第1の実施の形態と同じ効果が得られる。 (2-2)応力分散用凹部18,19に関するピン孔12
1,131の奥側への入り込み量が大きくなり、応力分
散用凹部18,19の拡開変形時におけるピストンピン
14と開口縁183、193との接触割合が第1の実施
の形態の場合よりも高くなる。
The following effects are obtained in the second embodiment. (2-1) The same effect as in the first embodiment can be obtained. (2-2) Pin hole 12 relating to the stress dispersion recesses 18 and 19
The amount of penetration of 1,131 into the back side is large, and the contact ratio between the piston pin 14 and the opening edges 183, 193 when the stress dispersion recesses 18, 19 are expanded and deformed is larger than that in the first embodiment. Will also be higher.

【0020】次に、図6の第3の実施の形態を説明す
る。第1の実施の形態と同じ構成部には同じ符号が付し
てある。この実施の形態では、応力分散用凹部24,2
5における奥壁面241,251がピン孔121,13
1に連なる壁面242に対して滑らかに接続する曲面に
してある。応力分散用凹部24,25におけるその他の
構成は第1の実施の形態と同じである。
Next, a third embodiment shown in FIG. 6 will be described. The same components as those in the first embodiment are denoted by the same reference numerals. In this embodiment, the stress dispersion recesses 24, 2
5, the inner wall surfaces 241 and 251 are pin holes 121 and 13
The curved surface smoothly connects to the wall surface 242 connected to 1. The other configurations of the stress-dispersing recesses 24 and 25 are the same as those of the first embodiment.

【0021】第3の実施の形態では以下の効果が得られ
る。 (3-1)第1の実施の形態と同じ効果が得られる。 (3-2)ピン孔121,131に対する応力分散用凹部
24,25の奥壁面241,251を反転する曲面とし
た構成では、奥壁面241,242の曲面形状が応力分
散用凹部24,25の拡開変形に伴う応力の分散に寄与
する。
The following effects can be obtained in the third embodiment. (3-1) The same effect as the first embodiment can be obtained. (3-2) In the configuration in which the inner wall surfaces 241 and 251 of the stress distribution recesses 24 and 25 with respect to the pin holes 121 and 131 are curved surfaces that are inverted, the curved surface shapes of the inner wall surfaces 241 and 242 correspond to the stress distribution recesses 24 and 25. It contributes to the dispersion of stress associated with the expansion deformation.

【0022】[0022]

【発明の効果】以上詳述したように本発明では、ピスト
ンの内側に形成された一対のピンボスのピン孔の対向す
る端縁におけるピストン頂面側の部位に応力分散用凹部
を設けたので、爆発圧力に伴って前記端縁に発生する引
っ張り応力を分散して前記部位における亀裂の発生を防
止し、ピストンの信頼性を向上するという優れた効果を
奏する。
As described in detail above, according to the present invention, since the stress dispersion concave portion is provided at the piston top surface side portion at the opposing edges of the pin holes of the pair of pin bosses formed inside the piston, The tensile stress generated at the edge due to the explosion pressure is dispersed to prevent the occurrence of cracks at the site, and the excellent effect of improving the reliability of the piston is achieved.

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

【図1】第1の実施の形態を示し、(a)は側断面図。
(b)は要部斜視図。
FIG. 1 shows a first embodiment, in which (a) is a side sectional view.
(B) is a perspective view of a main part.

【図2】図1のA−A線拡大断面図。FIG. 2 is an enlarged sectional view taken along line AA of FIG.

【図3】応力分散用凹部の形状及び拡開変形を示す線
図。
FIG. 3 is a diagram showing the shape and expansion deformation of a stress dispersion recess.

【図4】引っ張り応力を表すグラフ。FIG. 4 is a graph showing tensile stress.

【図5】第2の実施の形態を示す側断面図。FIG. 5 is a side sectional view showing a second embodiment.

【図6】第3の実施の形態を示す要部拡大断面図。FIG. 6 is an enlarged cross-sectional view of an essential part showing a third embodiment.

【図7】従来のピストンを示す側断面図。FIG. 7 is a side sectional view showing a conventional piston.

【符号の説明】[Explanation of symbols]

11…ピストン、111…ピストン頂面、12,13…
ピンボス、121,131…ピン、122,132…端
縁、14…ピストンピン、18,19,24,25…応
力分散用凹部、181,191…壁面、182,192
…奥壁面。
11 ... Piston, 111 ... Piston top surface, 12, 13 ...
Pin bosses, 121, 131 ... Pins, 122, 132 ... Edges, 14 ... Piston pins, 18, 19, 24, 25 ... Stress dispersion recesses, 181, 191 ... Wall surfaces, 182, 192
… The inner wall.

Claims (3)

【特許請求の範囲】[Claims] 【請求項1】ピストンの内側に形成された一対のピンボ
スのピン孔にピストンピンを貫通するピストンにおい
て、 各ピンボスのピン孔の対向する端縁におけるピストン頂
面側の部位に応力分散用凹部を設けたピストン。
1. A piston for penetrating a piston pin into a pair of pin holes of a pin boss formed inside the piston, wherein a stress-dispersing concave portion is provided at a portion on the piston top surface side of the opposing edge of the pin hole of each pin boss. The piston provided.
【請求項2】応力分散用凹部は、端縁と交差するように
ピン孔からピン孔の半径方向へ切り込み形成されてお
り、ピン孔に連なる応力分散用凹部の壁面は、ピン孔の
奥側で反転する曲面となっている請求項1に記載のピス
トン。
2. The stress-dispersing recess is formed by cutting from the pin hole in the radial direction of the pin hole so as to intersect with the end edge, and the wall surface of the stress-dispersing recess that is continuous with the pin hole is on the inner side of the pin hole. The piston according to claim 1, wherein the piston has a curved surface that is inverted by.
【請求項3】前記対向する端縁は、ピストン頂面から遠
ざかるにつれて互いに離間するように傾斜しており、応
力分散用凹部は、前記端縁のピストン頂面とは反対側の
部位よりもピストンピンの長手方向において対向相手の
応力分散用凹部側に近い位置にあり、ピン孔に連なる応
力分散用凹部の壁面は、ピン孔に対する応力分散用凹部
の奥壁面から遠ざかるにつれて拡開する請求項1及び請
求項2のいずれか1項に記載のピストン。
3. The opposed edges are inclined so as to be separated from each other as they move away from the top surface of the piston, and the stress dispersion concave portion is formed at a position closer to the piston than the top surface of the end edge of the piston. The wall surface of the stress-dispersing recess, which is located near the opposing stress-dispersing recess side in the longitudinal direction of the pin and is continuous with the pin hole, widens away from the inner wall surface of the stress-dispersing recess with respect to the pin hole. And the piston according to claim 2.
JP12578896A 1996-05-21 1996-05-21 Piston Pending JPH09303555A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP12578896A JPH09303555A (en) 1996-05-21 1996-05-21 Piston

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP12578896A JPH09303555A (en) 1996-05-21 1996-05-21 Piston

Publications (1)

Publication Number Publication Date
JPH09303555A true JPH09303555A (en) 1997-11-25

Family

ID=14918886

Family Applications (1)

Application Number Title Priority Date Filing Date
JP12578896A Pending JPH09303555A (en) 1996-05-21 1996-05-21 Piston

Country Status (1)

Country Link
JP (1) JPH09303555A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103511119A (en) * 2012-06-21 2014-01-15 本田技研工业株式会社 Piston

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103511119A (en) * 2012-06-21 2014-01-15 本田技研工业株式会社 Piston
CN103511119B (en) * 2012-06-21 2016-08-31 本田技研工业株式会社 Piston

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