JPH0542483B2 - - Google Patents

Info

Publication number
JPH0542483B2
JPH0542483B2 JP59123081A JP12308184A JPH0542483B2 JP H0542483 B2 JPH0542483 B2 JP H0542483B2 JP 59123081 A JP59123081 A JP 59123081A JP 12308184 A JP12308184 A JP 12308184A JP H0542483 B2 JPH0542483 B2 JP H0542483B2
Authority
JP
Japan
Prior art keywords
circular hole
die
hole
conical
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
JP59123081A
Other languages
Japanese (ja)
Other versions
JPS611438A (en
Inventor
Yoshinori Fukui
Susumu Yamamoto
Yoshio Sasaki
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.)
Kobe Steel Ltd
Original Assignee
Kobe Steel 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 Kobe Steel Ltd filed Critical Kobe Steel Ltd
Priority to JP59123081A priority Critical patent/JPS611438A/en
Publication of JPS611438A publication Critical patent/JPS611438A/en
Publication of JPH0542483B2 publication Critical patent/JPH0542483B2/ja
Granted legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21KMAKING FORGED OR PRESSED METAL PRODUCTS, e.g. HORSE-SHOES, RIVETS, BOLTS OR WHEELS
    • B21K1/00Making machine elements
    • B21K1/06Making machine elements axles or shafts
    • B21K1/08Making machine elements axles or shafts crankshafts
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21JFORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
    • B21J5/00Methods for forging, hammering, or pressing; Special equipment or accessories therefor
    • B21J5/06Methods for forging, hammering, or pressing; Special equipment or accessories therefor for performing particular operations
    • B21J5/12Forming profiles on internal or external surfaces

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Forging (AREA)

Description

【発明の詳細な説明】 〔産業上の利用分野〕 本発明は、先端に円錐形加工部を有するダイス
を用いて、曲げあるいはねじり荷重等を受ける伝
動軸の応力集中がある円孔の孔縁部分を強化する
ことによつて、軸全体としての強度を高め、伝動
軸の許容負担力を大きくする円孔付伝動軸の強化
法に係り、例えば、クランク軸、プロペラシヤフ
トを初め各種の伝動軸(駆動軸と従動軸および連
結軸を含む)の強化方法に関する。
[Detailed Description of the Invention] [Field of Industrial Application] The present invention uses a die having a conical processing portion at the tip to cut the hole edge of a circular hole where stress concentration of a transmission shaft is subjected to bending or torsional loads, etc. This method relates to a method for strengthening transmission shafts with circular holes, which increases the strength of the shaft as a whole and increases the permissible load of the transmission shaft by strengthening the parts. (including a driving shaft, a driven shaft, and a connecting shaft).

(従来の技術) クランク軸、プロペラシヤフトその他の各種の
伝動軸には、潤滑とか冷却とか等のためにそれら
の流体を通す円孔が形成されており、この円孔付
伝動軸に曲げあるいはねじり荷重等が作用すると
応力集中が起こり、従つて、応力集中がある孔縁
部分を強化しなければならない。
(Prior art) Crankshafts, propeller shafts, and other types of power transmission shafts are provided with circular holes through which fluid passes for lubrication, cooling, etc. When a load or the like is applied, stress concentration occurs, and therefore, the hole edge portion where the stress concentration is present must be strengthened.

即ち、 (1) 曲げ荷重により油孔(円孔)のはし即ち、孔
縁部分に生ずる応力 第6図に示す直径dの円孔をもつた直径Dの
軸材に曲げモーメントMが作用すると、円孔の
はしよりいくぶん中心には入つた点Aに応力集
中によつて大きな応力が生ずる。第7図に応力
集中の程度を示す。いま円孔の直径d=0.1・
Dとすると、応力集中率α=2.4となり、円孔
内面はしのA点付近に2.4・M/Zの応力が生
ずる。ただし、M:軸に加えられたモーメン
ト、Z:丸棒の断面係数(=πD3/32)。一般
に軸材につけられる油孔に直径は0.1〜0.2・D
であるため、A点付近に2.0〜2.4程度の応力集
中が生ずることはさけられない。
That is, (1) Stress generated at the edge of the oil hole (circular hole), that is, at the edge of the hole due to bending load.When a bending moment M acts on a shaft member of diameter D that has a circular hole of diameter d shown in Fig. 6. , a large stress is generated due to stress concentration at point A, which is located somewhat in the center of the circular hole. Figure 7 shows the degree of stress concentration. Now the diameter of the circular hole d = 0.1・
If D, the stress concentration rate α=2.4, and a stress of 2.4·M/Z is generated near point A on the inner edge of the circular hole. However, M: moment applied to the axis, Z: section modulus of the round bar (=πD 3 /32). Generally, the diameter of the oil hole attached to the shaft material is 0.1 to 0.2・D.
Therefore, it is inevitable that stress concentration of about 2.0 to 2.4 will occur near point A.

(2) ねじり荷重により油孔(円孔)のはしに生ず
る応力 第8図に示すごとく、円孔がある軸材に図示
されたトルクが加わつた場合、軸方向に対し
45゜傾いたAA点に引張り最大応力σmaxが生
じ、BB点に圧縮最大応力σminが生ずる。また
軸表皮上の軸線0−x,0−y上にもCおよび
D点から0.73・r(円孔の中心から√3・r)は
なれた点EおよびFにも1.33・τ0の最大応力が
生ずる。ただし、r:円孔の半径、τ0:軸表皮
に生ずるせん断応力(=16・T/π・D3、こ
こで、T:ねじりモーメント、D:軸の直径)。
(2) Stress generated on the edge of the oil hole (circular hole) due to torsional load As shown in Figure 8, when the torque shown in the figure is applied to the shaft material with the circular hole, the stress in the axial direction
The maximum tensile stress σmax occurs at the 45° inclined point AA, and the maximum compressive stress σmin occurs at the BB point. Also, on the axis 0-x, 0-y on the shaft skin, there is a maximum stress of 1.33·τ 0 at points E and F, which are 0.73·r away from points C and D (√ 3 ·r from the center of the circular hole). occurs. Here, r: radius of the circular hole, τ 0 : shear stress generated on the shaft skin (=16·T/π·D 3 , where T: torsional moment, D: diameter of the shaft).

A点およびB点に生ずる応力は第8図に示す
如く円孔はしよりやや中心には入つた点で最大
になる。円孔内壁の最大応力点A1およびB1
と円孔のはしとの距離は0.4・r程度である。
As shown in FIG. 8, the stress generated at points A and B reaches its maximum at a point that is slightly closer to the center than the edge of the circular hole. Maximum stress points A1 and B1 on the inner wall of the circular hole
The distance between the hole and the edge of the circular hole is about 0.4·r.

第9図にA,B点、A′,B′点およびE,F点
の応力集中率とd/D(または2.r/D)の関係を
示す。三者の内でA′,B′点の応力集中率αA′,B′が
最も大きく、油孔として普通あけられる孔径比
d/D=0.1〜0.2の場合についてみると、αA′,B
′=2.15〜2.30となり、油孔周辺に大きなせん断応
力が生ずる。このため油孔付き軸材においてはA
およびB点から軸線に対し45゜傾いた割れ(クロ
スマーク)を生じ折損することがある。
FIG. 9 shows the relationship between the stress concentration ratio and d/D (or 2.r/D) at points A, B, A', B', and E, F. Among the three, the stress concentration ratio α A ′, B ′ at points A ′ and B ′ is the largest, and considering the case where the hole diameter ratio d/D = 0.1 to 0.2, which is normally drilled as an oil hole, α A ′, B
' = 2.15 to 2.30, and a large shear stress is generated around the oil hole. For this reason, in shaft materials with oil holes, A
Also, a crack (cross mark) tilted at 45 degrees to the axis from point B may occur and breakage may occur.

このように伝動軸に油孔などの円孔があけられ
ると、曲げあるいはねじりいずれの応力条件にお
いても油孔の内面はし(孔縁)に基準応力の2.0
〜2.5倍の大きな応力が生ずるため、設計、工作
上下記の対策がとられているが、高力材の使用あ
るいは工数の増大による製造価格の上昇あるいは
設計上の不便はさけられない。
When a circular hole such as an oil hole is drilled in a transmission shaft in this way, the inner surface of the oil hole (hole edge) will have a stress of 2.0% of the standard stress under either bending or torsional stress conditions.
The following countermeasures have been taken in design and construction to avoid stress that is ~2.5 times as large. However, the use of high-strength materials and increased man-hours cannot avoid an increase in manufacturing costs or design inconveniences.

即ち、 (a) 設計上に工夫を加え、伝動軸に潤滑油供給用
の油孔を設けない。
That is, (a) the design has been improved and no oil hole for supplying lubricating oil is provided on the transmission shaft;

(b) 伝動軸の直径を大きくする、あるいは材料強
度を高めて油孔周辺の応力集中に耐えるように
する。
(b) Increase the diameter of the transmission shaft or increase the material strength to withstand stress concentration around the oil hole.

(c) 油孔のはしの部分の手入れを入念にしてバイ
ト跡などが残らないようにして応力集中係数が
大きくならないようにする。
(c) Carefully take care of the edge of the oil hole so that no bite marks remain and the stress concentration factor does not become large.

斯る技術背景から、油孔はしの強化法として従
来、第10図に示すごとく、平板あるいは凸板を
押付ける(第10図a)、またはボルト孔の強化
に利用されている方法であるが(第10図b)、
先端の円錐角α=90゜程度のポンチを押付けるな
どの方法が提案されている。これらは小試験片に
よる実験では50%以上疲れ限度が上昇し、有効な
円孔付軸材の強化法とされているが、全くといつ
てよい程実用化されていない。これはすでに提案
されている油孔の押付け強化法は実用化がむづか
しい、あるいは実用化させようとしても実用化で
きない下記の基本的欠陥が含まれているからであ
る。
From this technical background, conventional methods for strengthening oil hole holes include pressing a flat or convex plate (see Figure 10a), as shown in Figure 10, or methods used to strengthen bolt holes. (Figure 10b),
A method has been proposed, such as pressing a punch with a cone angle α of about 90° at the tip. In experiments using small test pieces, these methods increased the fatigue limit by more than 50% and are considered to be an effective method for strengthening shaft members with circular holes, but they have not been put to practical use at all. This is because the previously proposed methods of strengthening oil holes by pressing them are difficult to put into practical use, or contain the following basic defects that prevent them from being put into practical use even if they are attempted to be put into practical use.

(発明が解決しようとする問題点) 第10図a,bに示す従来例にあつては次のよ
うな問題点がある。
(Problems to be Solved by the Invention) The conventional example shown in FIGS. 10a and 10b has the following problems.

(a) 円孔はしの最大応力部は先にも述べたが、第
6図に示すごとく、円孔はし(孔縁)から0.4r
程度中心側には入つた位置になる。小径軸の場
合であれば第5図aに示すごとく、単に円孔は
しに平板を押し付けても強化効果は最大応力部
に及ぶが、工業的に使われる中大形軸において
は、円孔はしに平板状ダイスを押し付けても有
効な強化効果はえられない。
(a) As mentioned earlier, the maximum stress part of the circular hole edge is 0.4r from the circular hole edge (hole edge) as shown in Figure 6.
It will be in a position closer to the center. In the case of small-diameter shafts, as shown in Figure 5a, simply pressing a flat plate onto the circular hole edge will have a reinforcing effect on the area of maximum stress, but for medium-sized and large-diameter shafts used industrially, the circular hole Even if a flat die is pressed against the chopsticks, no effective strengthening effect can be obtained.

(b) 回転軸などにおいて円孔部を平板状ダイスで
押し付けると円孔部は変形し、また軸そのもの
の真円度も悪くなるため回転軸として実用に耐
えなくなる。
(b) If the circular hole of a rotating shaft is pressed with a flat die, the circular hole will be deformed, and the roundness of the shaft itself will deteriorate, making it unusable for practical use as a rotating shaft.

(c) 第10図bに示すごとく、円錐状ポンチで単
に押付けても接触部に塑性流動が生じにくいた
め、強大な加圧力で円錐状ポンチを押し付けな
いと有効な強化効果はえられない。そのため第
10図bに示す方法によつたのでは軸に曲りな
どが生ずるため、軸材を対象にしてこの方法を
実用化させることはむづかしい。
(c) As shown in Figure 10b, simply pressing with a conical punch does not easily cause plastic flow in the contact area, so an effective strengthening effect cannot be obtained unless the conical punch is pressed with a strong pressure. Therefore, if the method shown in FIG. 10b is used, the shaft will be bent, so it is difficult to put this method into practical use for shaft members.

(問題を解決するための手段) 本発明は、斯る技術背景を基にして従来例の問
題点を解決するために案出されたものであつて、
先端に円錐形加工部を有するダイスを用いて、曲
げあるいはねじり荷重等を受ける伝動軸の応力集
中がある円孔の孔縁部分を強化する方法であつ
て、円錐形加工部の外周面にその母線に沿つた凸
部が周方向所定間隔おいて形成された第1のダイ
スを用いて、その円錐形加工部を円孔の孔縁部分
に押付け、凸部によりこれと対応する部分のみを
径方向外方に向つて塑性流動をおこさせ、次い
で、凸部が形成されていない別の第2のダイスの
円錐形加工部を円孔の孔縁部分に押付け、該第2
のダイスの円錐形加工部によつて前記第1のダイ
スで加工されていない部分を径方向外方に向つて
塑性流動をおこさせることを特徴とする円孔付伝
動軸の強化法を提供するのである。
(Means for solving the problem) The present invention was devised based on the above technical background to solve the problems of the conventional example, and includes:
This method uses a die with a conical shaped part at the tip to strengthen the edge of a circular hole where the stress concentration of the transmission shaft is subjected to bending or torsional loads. Using a first die in which convex portions are formed at predetermined intervals in the circumferential direction along the generatrix, press the conical processing portion against the hole edge portion of the circular hole, and use the convex portion to radially cut only the corresponding portion. A plastic flow is generated outward in the direction, and then a conical processing portion of another second die in which no convex portion is formed is pressed against the hole edge portion of the circular hole.
Provided is a method for strengthening a power transmission shaft with a circular hole, characterized in that a portion not processed by the first die is caused to undergo plastic flow radially outward by a conical processing portion of the die. It is.

(作 用) 第1図に示すごとく、先端に円錐形加工部を有
し、この加工部の外周面にその母線に沿つた4ケ
の凸部7−1〜7−4をもつた第1のダイス7−
5,7−5′を円孔はし(孔縁)に押付け、円孔
はしの45゜方向A,B,CおよびD部に塑性流動
をおこさせて強化する。次いで円錐形加工部を有
する第2の上下ダイス7−6,7−6′を円孔は
しに押付け、上記上下ダイス7−5,7−5′で
加工されていないE,F,GおよびH部に塑性流
動をおこさせて強化するとともに円孔はしをなめ
らかな円形にもどすことによつて、応力集中があ
る円孔の孔縁部分が強化され、伝動軸全体として
の強度を高め、該軸の許容負担力を大きくできる
ことになる。
(Function) As shown in Fig. 1, the first convex part has a conical processing part at the tip and four convex parts 7-1 to 7-4 along the generatrix on the outer peripheral surface of this processing part. Dice 7-
5, 7-5' are pressed against the circular hole edge (hole edge), and plastic flow is caused in the 45° direction A, B, C, and D portions of the circular hole edge to strengthen it. Next, the second upper and lower dies 7-6, 7-6' having conical processing parts are pressed against the circular hole edge, and the E, F, G and By creating plastic flow in the H section to strengthen it and returning the circular hole edge to a smooth circular shape, the edge of the circular hole where stress is concentrated is strengthened, increasing the strength of the transmission shaft as a whole. This means that the allowable load on the shaft can be increased.

(実施例) 第1図を参照して本発明の実施例を工程順に説
明する。
(Example) An example of the present invention will be described in order of steps with reference to FIG.

第1図において、8−10は伝動軸であり、本
例では横断方向に貫通された円孔8−9を有す
る。
In FIG. 1, reference numeral 8-10 is a transmission shaft, which in this example has a circular hole 8-9 passed through in the transverse direction.

7−5及び7−5′は先端に円錐形加工部8−
2,8−2′をそれぞれ有する第1のダイスであ
り、加工部のそれぞれには母線に沿つた凸部7−
1,7−2,7−3,7−4(なお、下のダイス
は共通部に符号ダツシユを付している)の4個を
有し、各凸部が周方向に等間隔をおいて形成さ
れ、本例では、各凸部の外周面は丸味を有するも
のとされ、各凸部間は丸味を有する凹部とされて
いる。
7-5 and 7-5' have a conical processing part 8- at the tip.
2 and 8-2', respectively, and each of the processing parts has a convex part 7-2 along the generatrix.
1, 7-2, 7-3, 7-4 (the lower die has a common part with a dash), and each convex part is equally spaced in the circumferential direction. In this example, the outer circumferential surface of each convex portion is rounded, and the space between each convex portion is a rounded concave portion.

而して、第1図aで示す如く、先ず凸部7−1
〜7−4を有する円錐形の第1のダイス7−5お
よび7−5′を円孔はしの上下から加圧し、最大
せん断応力が生ずる軸心に対し45゜の方向(A,
B,C,D点、第1図b参照)を加圧して径方向
外方に向つて塑性流動を起こさせて強化した後、
第1図cで示す如く前述の凸部を円錐形加工部に
有しない別の第2のダイス7−6,7−6′を上
下から円孔はしに押付け、先の工程で凹んだ45゜
方向A,B,C,D点(第7図b参照)の間の凸
部、E,F,G,H点、を加圧して径方向に向つ
て塑性流動を起こさせて強化し、円孔はしの凹凸
をなくして平滑にするとともに、まげ最大応力が
生ずる軸心方向を加圧強化する。
Therefore, as shown in FIG. 1a, first, the convex portion 7-1
The first conical dies 7-5 and 7-5' having sizes 7-4 and 7-4 are pressurized from above and below the circular hole edge, and the direction (A,
Points B, C, and D (see Figure 1 b) are pressurized to cause plastic flow radially outward and strengthened.
As shown in Fig. 1c, another second die 7-6, 7-6' which does not have the above-mentioned convex part in the conical processing part is pressed against the circular hole edge from above and below, and 45 The protrusions between points A, B, C, and D in the ゜ direction (see Figure 7b), points E, F, G, and H are pressurized to cause plastic flow in the radial direction and strengthened. In addition to eliminating the unevenness of the circular hole edge and making it smooth, the axial direction where the maximum bending stress occurs is strengthened by pressure.

円錐形ダイスの先端角α(第1図参照)は20゜〜
90゜が適当である。その選択は第11図に示す最
大応力部の位置、すなわち円孔直径d/軸直径D
の比および円孔はしのR/円孔直径dの比によつ
て変わる。円孔直径が15mm程度以下で小さいとき
はd/DおよびR/d比を考慮して最適な先端角
α1を決め、この先端角α1をもつたダイスのみで加
圧加工してよいが、円孔直径が15mm以上、とくに
20mmをこえる直径のときは、2種類または3種類
の先端角α1,α2またはα1,α2,α3をもつたダイス
によつて、最大応力部付近を広く加圧強化するの
がよい。
The tip angle α of the conical die (see Figure 1) is 20°~
90° is appropriate. The selection is based on the position of the maximum stress part shown in FIG.
and the ratio of R of the circular hole edge/diameter of the circular hole d. If the diameter of the circular hole is small (approximately 15 mm or less), consider the d/D and R/d ratios, determine the optimal tip angle α 1 , and pressurize only with a die with this tip angle α 1 . , the hole diameter is 15mm or more, especially
When the diameter exceeds 20 mm, it is recommended to use dies with two or three types of tip angles α 1 , α 2 or α 1 , α 2 , α 3 to pressurize and strengthen the area around the maximum stress area. good.

第2図を参照して、加圧加工装置の具体例を説
明する。
A specific example of the pressure processing apparatus will be described with reference to FIG.

第2図において8−1は固定フレームであつ
て、このフレームに下側ダイス7−5′、加圧用
シリンダー8−3および可動フレーム8−4が、
ピン8−5および8−6を介して取り付けられて
いる。可動フレーム8−4には上ダイス7−5が
球面座8−8を介して取り付けられており、この
球面座8−8によつて円孔8−9の軸心と上下ダ
イス7−5,7−5′の中心を結ぶ線が一致して
いなくても、上下ダイスの加圧によつて無理が生
ずることはない。軸材8−10の加圧治具からの
取り出し、あるいは挿入はピン8−5を取り外
し、可動フレーム8−4を加圧用シリンダー8−
3から外すことによつて行われる。
In FIG. 2, 8-1 is a fixed frame, on which a lower die 7-5', a pressurizing cylinder 8-3 and a movable frame 8-4 are attached.
It is attached via pins 8-5 and 8-6. An upper die 7-5 is attached to the movable frame 8-4 via a spherical seat 8-8, and the spherical seat 8-8 connects the axis of the circular hole 8-9 with the upper and lower dies 7-5, Even if the lines connecting the centers of 7-5' do not match, no strain will occur due to the pressure applied by the upper and lower dies. To take out or insert the shaft member 8-10 from the pressurizing jig, remove the pin 8-5 and move the movable frame 8-4 to the pressurizing cylinder 8-
This is done by removing it from 3.

ダイス押付力Pは式(1)によつて先ず算出する。 The die pressing force P is first calculated using equation (1).

P=k・π・d・√・・sinα/2・Ym ……(1) ここで k:加工法によつて定まる定数 本発明による方法 k=0.6 円錐ダイスによる方法 k=1.0 d:円孔の直径 mm R:円孔はしの半径 mm α:ダイス円錐先端角 Ym:材料の降伏点 Kg/mm2 式(1)によつて算出されたダイス押付力Pによつ
て円孔はしを加圧加工し、円孔径の最大変形率
Δd/di,ただし使用記号は第3図による、が0.02
〜0.03になるようダイス押付力を調整する。これ
は最大変形率が0.02〜0.03のとき第4図に示すご
とく最も強化効果が大きく、本発明の基本になる
数値の一つである。
P=k・π・d・√・・sinα/2・Ym ...(1) where k: Constant determined by processing method Method according to the present invention k=0.6 Method using conical die k=1.0 d: Circular hole Diameter mm R: Radius of the circular hole edge mm α: Die cone tip angle Ym: Yield point of material Kg/mm 2 The circular hole edge is The maximum deformation rate of the circular hole diameter is Δd/di, however, the symbols used are as shown in Figure 3, and are 0.02.
Adjust the die pressing force to ~0.03. This is one of the values that form the basis of the present invention, as the reinforcing effect is greatest when the maximum deformation rate is 0.02 to 0.03, as shown in FIG.

最大変形率が0.02〜0.03のときダイス接触長さ
h(第3図参照)は式(2)によつて近似的にあらわ
される。
When the maximum deformation rate is 0.02 to 0.03, the die contact length h (see FIG. 3) is approximately expressed by equation (2).

h〓0.28〜0.35・√・ ……(2) ここで、d:円孔の直径 mm R:円孔はしの半径 mm 実際操業においてダイス接触部長さを基準にと
るのが便利であるから、式(2)によつて算出される
hの値と、操業後測定されるダイス接触部長さの
測定値を比べることによつて操業の良否が判定で
きる。
h〓0.28~0.35・√・ ...(2) Here, d: Diameter of the circular hole mm R: Radius of the circular hole edge mm In actual operation, it is convenient to take the length of the die contact part as the standard. The quality of the operation can be determined by comparing the value of h calculated by equation (2) with the measured value of the length of the die contact portion measured after the operation.

このように上下のダイスで示す第1と第2の加
圧治具によると、上下ダイス7−5,7−5′を
円孔はしに押付ける加工工程において、軸材8−
10に曲げその他の負荷が加わらない。また4ケ
の凸部をもつたダイス7−5,7−5′および凸
部をもたない第2の円錐形ダイス7−6,7−
6′の2つに分けて円孔はしの加圧加工が行われ
るため、式(1)からも明らかなごとく、単純な円錐
形ダイスを用いた場合より40%小さい加圧力で円
孔周辺は所望の強さまで強化され、軸材8−10
に曲りはほとんど生じない。
According to the first and second pressurizing jigs shown by the upper and lower dies, in the machining process of pressing the upper and lower dies 7-5, 7-5' against the circular hole chopper, the shaft member 8-
No bending or other loads are applied to 10. Additionally, dies 7-5, 7-5' having four convex portions and second conical dies 7-6, 7- having no convex portions are used.
Since the pressure machining of the circular hole chopper is performed in two parts (6'), as is clear from equation (1), the pressure around the circular hole is 40% lower than when using a simple conical die. is reinforced to the desired strength, and the shaft material 8-10
Almost no bending occurs.

第5図に本発明の利用例を示す。第5図aはク
ランク軸の油孔開口部11−1,11−2に関す
るものである。クランク軸に曲げ荷重が負荷され
た場合、最大応力はピンおよびジヤーナルフイレ
ツト11−3,11−4に生ずる。ねじり荷重が
負荷されたときは油孔開口部11−1,11−2
に最大せん断応力が生ずる。ピンおよびジヤーナ
ルフイレツトは冷間ロール加工法などによつて強
化することはできるが、油孔開口部の強化法は開
発されていなかつた。
FIG. 5 shows an example of the use of the present invention. FIG. 5a relates to the oil hole openings 11-1 and 11-2 of the crankshaft. When a bending load is applied to the crankshaft, maximum stress occurs in the pins and the journal fillets 11-3, 11-4. When a torsional load is applied, the oil hole openings 11-1, 11-2
Maximum shear stress occurs at Although pins and journal fillets can be strengthened by cold rolling, a method for strengthening oil hole openings has not yet been developed.

クランク軸の許容伝達トルクは油孔周辺の応力
によつてきまるため、最近開発される省エネルギ
ーの要求にそう機関のように、低回転速度、大ト
ルク伝達の要求をみたすクランク軸の軸径は大き
くしなければならなかつた。しかし本発明による
強化法によつて油孔開口部が強化されると、軸径
の減小あるいは低強度材の利用が可能になつた。
The permissible transmission torque of the crankshaft depends on the stress around the oil hole, so in response to the recently developed energy saving requirements, the shaft diameter of the crankshaft that satisfies the requirements for low rotational speed and large torque transmission, such as in engines, is I had to make it bigger. However, when the oil hole opening is strengthened by the strengthening method of the present invention, it becomes possible to reduce the shaft diameter or use a low-strength material.

第5図bは可変ピツチプロペラ(CPP)の管
制油導入開口部11−5に関するものである。
CPPはピツチ変更用に管制油導入孔が必要であ
るが、管制油導入孔開口部11−5が設けられる
軸11−6の直径は大きくし、開口部付近の応力
が大きくならないようにされている。しかし本発
明になる円孔はしの強化法を適用すると軸径拡大
の必要はなくなり原価低減が可能になる。
FIG. 5b relates to the control oil introduction opening 11-5 of a variable pitch propeller (CPP).
CPP requires a control oil introduction hole for pitch change, but the diameter of the shaft 11-6 on which the control oil introduction hole opening 11-5 is provided is made large to prevent stress near the opening from increasing. There is. However, if the method of strengthening circular hole chopsticks according to the present invention is applied, there is no need to increase the shaft diameter, making it possible to reduce the cost.

この他一般産業用機械に用いられる伝動軸にお
いて、強度上の観点から油孔を設けにくく不便を
感じる場合があるが、本発明による強化法が利用
されると油孔開口部の位置選択上の制約はほとん
どなくなる。
In addition, in power transmission shafts used in general industrial machinery, it is sometimes difficult to provide oil holes from the viewpoint of strength, but when the strengthening method of the present invention is used, it is difficult to select the position of the oil hole opening. There are almost no restrictions.

なお、本発明でいう円孔は、油孔の他、空気孔
等を含むものであり、有底円孔であつてもよく
又、凸部の個数は周方向に所定間隔おいて等配で
あれば、4個に限られることはない。
Note that the circular hole in the present invention includes an air hole in addition to an oil hole, and may be a circular hole with a bottom. If there are, the number is not limited to four.

(発明の効果) 本発明の効果は小さいダイス押付け力によつ
て、円孔付き軸材に曲りなどの寸法変化を生じさ
せることなく、軸材の疲れ限度を円孔がない場合
と同じ値にまで高めることができることにある。
(Effects of the Invention) The effects of the present invention are that, by using a small die pressing force, the fatigue limit of the shaft material with a circular hole can be set to the same value as that without a circular hole, without causing dimensional changes such as bending in the shaft material with a circular hole. The goal lies in the fact that it can be raised to the highest level.

以下実施例によつてその効果を説明する。 The effects will be explained below using examples.

1 今までに提案されている従来の方法 S45C、軸径20mm、円孔なしの軸材の疲れ限
度は30Kg/mm2であつたが、これに直径3.5mmの
円孔をつけると、疲れ限度は18Kg/mm2(円孔が
ないときの約60%)に低下する。この円孔付き
軸材の円孔部に平ダイスを用いて10tの荷重を
負荷すると(第10図a)の方法)、疲れ限度
は26Kg/mm2に上昇し、ほぼ円孔なしの場合の強
度に復元する。しかし10tの荷重が負荷される
と軸材は大きく変形し実用に供することはでき
なくなる。これは第11図に示すごとく、最大
応力部は円孔はしよりやや中心には入つたとこ
ろになるため、平ダイスによつて円孔はしを加
圧するのみで強化効果をうるには、大きな加圧
力で円孔はしを加圧しなければならないことを
示しており、工業的に使われる大形軸に平ダイ
スによる強化法を適用することはほとんど不可
能に近い。
1 The fatigue limit of the conventional method proposed so far for S45C, shaft material with a shaft diameter of 20 mm and no circular hole was 30 Kg/ mm2 , but if a circular hole of 3.5 mm in diameter was added to this, the fatigue limit The weight decreases to 18Kg/mm 2 (approximately 60% of that without the circular hole). When a load of 10 tons is applied to the hole part of this shaft material with a circular hole using a flat die (the method shown in Figure 10a), the fatigue limit increases to 26 kg/ mm2 , which is almost the same as that without a circular hole. Restore to strength. However, when a load of 10 tons is applied, the shaft material deforms significantly, making it impossible to put it to practical use. This is because, as shown in Figure 11, the maximum stress area is located slightly in the center of the circular hole edge, so in order to obtain a strengthening effect only by pressurizing the circular hole edge with a flat die, it is necessary to This indicates that a large pressure force must be applied to the circular hole chopper, making it almost impossible to apply the reinforcement method using flat dies to large shafts used industrially.

2 本発明による強化効果 上記試験と同様、S45C材で作られた直径100
mmの軸材の中央に、直径10mmの円孔をあけ、そ
の両はしに半径5mmのRをつけて平面曲げ疲れ
試験片を製作した。
2 Strengthening effect by the present invention Similar to the above test, a diameter 100 mm made of S45C material
A circular hole with a diameter of 10 mm was drilled in the center of the mm shaft member, and a radius of 5 mm was made on both edges to prepare a plane bending fatigue test piece.

この円孔はし(孔縁部分)を本発明になる円
錐先端角22.5゜および45゜のダイスを用い、押付
力約1000Kgおよび1800Kgで加圧加工した後、平
面曲げ疲れ試験を行つたところ、疲れ限度は28
Kg/mm2と測定された。この値は1項で述べた20
mm直径の軸材の疲れ限度30Kg/mm2に比べてやや
低いが、寸法効果によるものであつて、疲れ限
度28Kg/mm2の値は、円孔があけられていない場
合のφ100mm軸材の疲れ限度にほぼ匹敵する。
After pressurizing this circular hole edge (hole edge portion) using dies with conical tip angles of 22.5° and 45° according to the present invention at pressing forces of approximately 1000 kg and 1800 kg, a plane bending fatigue test was conducted. Fatigue limit is 28
It was measured as Kg/ mm2 . This value is 20 as mentioned in section 1.
This is slightly lower than the fatigue limit of 30Kg/mm 2 for a shaft with a diameter of mm, but this is due to a dimensional effect, and the fatigue limit of 28Kg/mm 2 is lower than that of a 100mm shaft without a circular hole. Almost equal to the fatigue limit.

このように本発明になる円孔はしの強化技術
によると、軸材に油孔などの円孔があけられた
としても、2000Kg程度の加圧力を負荷すること
によつて円孔はしは強化され、円孔がない場合
とほぼ同じ疲れ限度になる。また本項で述べた
実例は平面曲げ疲れ限度に関するもののみであ
るが、平面曲げ疲れ限度(σw)bとねじり疲
れ限度τwとの間には式(3)に示す関係が成立つ
ことが一般に認められているため、 τw=(σw)b/√3 ……(3) ねじり疲れ限度も曲げ疲れ限度と同様、空孔
がない場合の値にまで高まることは充分推察さ
れる。
As described above, according to the technology for strengthening circular hole chopsticks of the present invention, even if a circular hole such as an oil hole is made in the shaft material, the circular hole chopstick can be strengthened by applying a pressure of about 2000 kg. It is reinforced and has almost the same fatigue limit as without the hole. Furthermore, although the examples described in this section are only related to the plane bending fatigue limit, it is generally understood that the relationship shown in equation (3) holds between the plane bending fatigue limit (σw) b and the torsional fatigue limit τw. Since τw = (σw)b/√3...(3) It is highly inferred that the torsional fatigue limit, like the bending fatigue limit, will increase to the value when there are no holes.

金属材料は静水圧のような等しい圧力を全表
面にかてもほとんど硬化しない、また残留応力
もほとんど発生しない。金属材料を加圧加工に
よつて硬化させ強化するには塑性流動をおこさ
せなければならない。本発明は第2図に示した
加工治具によつて、直交する方向に4ケの凸部
をもつた円錐形ダイスを用い、その凸部を円孔
はしの軸心に対し45゜傾いた方向に当て加圧し、
塑性流動が生じやすい加工条件のもとでねじり
荷重によつて最大せん断応力が生ずる個所を強
化し、次いで円孔はしの凸出部(先の工程で円
錐形ダイスがあたらなかつた個所)を凸部を有
しない別の円錐形ダイスによつて加圧加工し、
曲げ荷重のもとで最大応力が生ずる個所を強化
するとともに、円孔はしをなめらかに成形す
る。このようにダイス当り面が塑性流動しやす
い条件で加圧加工することによつて、小さい加
圧力で大きい強化効果をうることができる。
Even if a metal material is subjected to an equal pressure such as hydrostatic pressure on its entire surface, it will hardly harden, and almost no residual stress will be generated. In order to harden and strengthen metal materials through pressure working, plastic flow must occur. The present invention uses the processing jig shown in Fig. 2, and uses a conical die having four protrusions in orthogonal directions, with the protrusions tilted at 45 degrees with respect to the axis of the circular hole chopper. Apply pressure in the direction of
The areas where the maximum shear stress occurs due to torsional load under processing conditions where plastic flow is likely to occur are strengthened, and then the convex part of the circular hole edge (the area where the conical die did not touch in the previous process) is strengthened. Pressure-processed using another conical die that does not have a convex part,
The parts where the maximum stress occurs under bending load are strengthened, and the circular hole edges are formed smoothly. In this way, by pressurizing the die contact surface under conditions that facilitate plastic flow, a large strengthening effect can be obtained with a small pressurizing force.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図a,b,c,dは本発明の実施例を工程
順に示す平面図と横断面図、第2図a,bは同装
置一例の立面図とA矢示図、第3図はダイス接触
部分の記号を表わした説明図、第4図は孔径拡大
率と疲れ限度上昇率の関係を示す説明図、第5図
a,bは本発明の使用乃至利用例2つを示す正面
図と一部破断の正面図、第6図は曲げ応力のかか
る状態を示す説明図、第7図は曲げモーメントが
使用たときの円孔はし(孔縁)の応力集中率を示
すグラフ、第8図はねじりトルクのかかる状態の
説明図、第9図はねじりトルクが作用したときの
円孔はしの応力集中率を示すグラフ、第10図
a,bは従来例の2例を示す説明図、第11図は
円孔はしの最大応力部を示す説明図である。 7−1,7−4……凸部、7−5,7−5′…
…第1のダイス、7−6,7−6′……第2のダ
イス、8−2,8−2′……円錐形加工部、8−
9……円孔、8−10……伝動軸。
Figures 1 a, b, c, and d are a plan view and a cross-sectional view showing an embodiment of the present invention in the order of steps, Figures 2 a and b are an elevational view and a view indicated by arrow A of an example of the same device, and Figure 3 4 is an explanatory diagram showing the symbol of the die contact part, FIG. 4 is an explanatory diagram showing the relationship between hole diameter expansion rate and fatigue limit increase rate, and FIGS. 5 a and b are front views showing two usage examples of the present invention. Figure 6 is an explanatory diagram showing the state where bending stress is applied, Figure 7 is a graph showing the stress concentration rate of the circular hole edge (hole edge) when bending moment is applied, Fig. 8 is an explanatory diagram of the state in which torsional torque is applied, Fig. 9 is a graph showing the stress concentration rate of the circular hole edge when torsional torque is applied, and Fig. 10 a and b show two conventional examples. The explanatory diagram, FIG. 11, is an explanatory diagram showing the maximum stress part of the circular hole chopstick. 7-1, 7-4... Convex portion, 7-5, 7-5'...
...First die, 7-6, 7-6'... Second die, 8-2, 8-2'... Conical processing part, 8-
9...Circular hole, 8-10...Transmission shaft.

Claims (1)

【特許請求の範囲】 1 先端に円錐形加工部を有するダイスを用い
て、曲げあるいはねじり荷重等を受ける伝動軸の
応力集中がある円孔の孔縁部分を強化する方法で
あつて、 円錐形加工部の外周面にその母線に沿つた凸部
が周方向所定間隔おいて形成された第1のダイス
を用いて、その円錐形加工部を円孔の孔縁部分に
押付け、凸部によりこれと対応する部分のみを径
方向外方に向つて塑性流動をおこさせ、 次いで、凸部が形成されていない別の第2のダ
イスの円錐形加工部を円孔の孔縁部分に押付け、
該第2のダイスの円錐形加工部によつて前記第1
のダイスで加工されていない部分を径方向外方に
向つて塑性流動をおこさせる ことを特徴とする円孔付伝動軸の強化法。
[Scope of Claims] 1. A method of strengthening the hole edge portion of a circular hole where the stress concentration of a transmission shaft that is subjected to bending or torsional loads is performed using a die having a conical shaped portion at the tip, the die having a conical shape. Using a first die in which convex portions are formed on the outer circumferential surface of the processed portion along its generatrix at predetermined intervals in the circumferential direction, the conical processed portion is pressed against the hole edge portion of the circular hole, and the conical portion is pressed against the hole edge portion of the circular hole. Plastic flow is caused only in the portion corresponding to the hole in the radial direction outward, and then the conical processing portion of another second die in which no convex portion is formed is pressed against the hole edge portion of the circular hole.
The conical processing portion of the second die
A method for strengthening a power transmission shaft with a circular hole, which is characterized by causing plastic flow in the portion that has not been machined with a die radially outward.
JP59123081A 1984-06-14 1984-06-14 Reinforcing method of transmission shaft having circular hole Granted JPS611438A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP59123081A JPS611438A (en) 1984-06-14 1984-06-14 Reinforcing method of transmission shaft having circular hole

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP59123081A JPS611438A (en) 1984-06-14 1984-06-14 Reinforcing method of transmission shaft having circular hole

Publications (2)

Publication Number Publication Date
JPS611438A JPS611438A (en) 1986-01-07
JPH0542483B2 true JPH0542483B2 (en) 1993-06-28

Family

ID=14851721

Family Applications (1)

Application Number Title Priority Date Filing Date
JP59123081A Granted JPS611438A (en) 1984-06-14 1984-06-14 Reinforcing method of transmission shaft having circular hole

Country Status (1)

Country Link
JP (1) JPS611438A (en)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110396582A (en) * 2019-08-14 2019-11-01 南通大学 A nanometerization device for the surface of the hole wall of a metal component

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP4825282B2 (en) * 2009-03-30 2011-11-30 株式会社神戸製鋼所 Crankshaft fatigue strength improving method and processing device
KR101144129B1 (en) 2009-10-29 2012-05-24 현대 파워텍 주식회사 Shaft for transmission and treatment method thereof
US8187133B2 (en) 2010-03-31 2012-05-29 Ford Global Technologies, Llc Fatigue resistant transverse lubrication passage for transmission shafts
JP5256327B2 (en) * 2011-06-20 2013-08-07 株式会社神戸製鋼所 Crankshaft fatigue strength improving method and processing device
CN102433420A (en) * 2011-12-16 2012-05-02 陕西飞机工业(集团)有限公司 Strengthening method suitable for part holes in non-open area
US12276332B1 (en) 2023-10-25 2025-04-15 GM Global Technology Operations LLC Torque transfer member having a strengthened fluid port and method of making the same

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110396582A (en) * 2019-08-14 2019-11-01 南通大学 A nanometerization device for the surface of the hole wall of a metal component

Also Published As

Publication number Publication date
JPS611438A (en) 1986-01-07

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