JPH0681907A - Manufacture of double planetary carrier - Google Patents

Manufacture of double planetary carrier

Info

Publication number
JPH0681907A
JPH0681907A JP4235695A JP23569592A JPH0681907A JP H0681907 A JPH0681907 A JP H0681907A JP 4235695 A JP4235695 A JP 4235695A JP 23569592 A JP23569592 A JP 23569592A JP H0681907 A JPH0681907 A JP H0681907A
Authority
JP
Japan
Prior art keywords
side plate
carrier
leg pieces
seat surfaces
planetary
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.)
Granted
Application number
JP4235695A
Other languages
Japanese (ja)
Other versions
JP3205947B2 (en
Inventor
Haruo Tanaka
治雄 田中
Tokuaki Takahashi
徳朗 高橋
Tetsuo Suzuki
哲男 鈴木
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.)
Honda Motor Co Ltd
Original Assignee
Honda Motor 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 Honda Motor Co Ltd filed Critical Honda Motor Co Ltd
Priority to JP23569592A priority Critical patent/JP3205947B2/en
Publication of JPH0681907A publication Critical patent/JPH0681907A/en
Application granted granted Critical
Publication of JP3205947B2 publication Critical patent/JP3205947B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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  • Structure Of Transmissions (AREA)
  • Retarders (AREA)
  • General Details Of Gearings (AREA)

Abstract

PURPOSE:To facilitate alignment of phases of leg pieces by forming a plurality of seat surfaces on an outer peripheral edge of a surface of one side plate opposing to the other side plate of a double planetary carrier which holds two pairs planetary gears, getting the leg pieces of one carrier butted against the seat surfaces, and welding them. CONSTITUTION:A cylindrical part 51a is formed on an outer periphery of a side plate 51 on an inner side of a second carrier 5 for receiving a side plate 41 on an inner side of a first carrier 4 opposing to the side plate 51. Outward and inward projecting serration teeth 45, 55 are formed on the outer periphery of the side plate 41 and the cylindrical part 51a. Both the carriers 4, 5 are serration-engaged with each other. A plurality of portions around an end of the cylindrical part 51a are caulked for integral assembling. In this case, on the second carrier 5, a plurality of seat surfaces 54 are formed on an outer peripheral edge of the surface of the inner side plate 51 opposing to the outer side plate 52 with a specified phase. Leg pieces 53 are agutted against the seat surfaces 54 for aligning the phases of the side plates 51, 52. Laser beam is irradiated to the connection part of the leg piece 53 for welding.

Description

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

【0001】[0001]

【産業上の利用分野】本発明は、主としてダブルプラネ
タリキャリアの片側のキャリアの製造に適用されるプラ
ネタリキャリアの製造方法に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a method of manufacturing a planetary carrier, which is mainly applied to manufacturing a one-sided carrier of a double planetary carrier.

【0002】[0002]

【従来の技術】プラネタリキャリアは、実公平1−17
712号公報に見られるように、プラネタリギアを挾ん
で対向する1対の側板を備え、該両側板をその一方の側
板の周囲複数箇所に曲成した他方の側板に向ってのびる
脚片を介して結合して構成されており、この場合各脚片
を他方の側板に形成した各係合孔に差し込んで溶接する
を一般としている。また、軸方向に離間した2組のプラ
ネタリギアを担持するダブルプラネタリキャリアを、各
組のプラネタリギアを担持する1対のプラネタリキャリ
アを軸方向に連結して構成するために、一方のプラネタ
リキャリアの軸方向内側の側板の外周に他方のプラネタ
リキャリアの軸方向内側の側板を受け入れる筒部を成形
し、筒部とこれに挿入される側板とにセレーション歯を
形成して、両プラネタリキャリアをセレーション係合さ
せることも考えられている。
2. Description of the Related Art Planetary carriers are actually fair 1-17
As disclosed in Japanese Laid-Open Patent Publication No. 712, a pair of side plates facing each other with a planetary gear in between are provided, and the both side plates are bent at a plurality of positions around the one side plate through leg pieces extending toward the other side plate. In this case, each leg piece is generally inserted into each engaging hole formed in the other side plate and welded. Further, in order to configure a double planetary carrier that carries two sets of planetary gears that are separated in the axial direction by connecting a pair of planetary carriers that carry each set of planetary gears in the axial direction, one planetary carrier A cylindrical portion that receives the axially inner side plate of the other planetary carrier is formed on the outer periphery of the axially inner side plate, and serration teeth are formed on the cylindrical portion and the side plate that is inserted into the cylindrical portion to form a serration support for both planetary carriers. It is also considered to combine them.

【0003】[0003]

【発明が解決しようとする課題】ところで、プラネタリ
キャリアの一方の側板に曲成した脚片を他方の側板に形
成した係合孔に差し込んで溶接する従来法では、他方の
側板を係合孔の形成スペースを確保するために大径に形
成する必要があってキャリアが大型化する不具合があ
る。この場合、他方の側板の一方の側板に対する対向面
の外周縁部に脚片を突き当てて溶接することも考えられ
るが、図8に示す如く、他方の側板bの外周に一方の側
板aとの対向方向とは逆側にのびる筒部cがプレス成形
されていると、他方の側板bの一方の側板aに対する対
向面の外周縁部は筒部cに向って湾曲するアール部とな
り、脚片dの先端の径方向外縁寄りの部分が側板bから
浮いてしまう。そのため、脚片dをその先端の径方向内
縁寄りの部分のみで側板bに溶接せざるを得なくなっ
て、溶接強度の確保が困難になり、更にはプラネタリギ
アのスラスト受面となる脚片dの接合箇所の径方向内方
部分に溶接スパッタが飛散して、スパッタの除去工程が
必要となる。本発明は、以上の点に鑑み、一方の側板に
曲成した脚片を筒部をプレス成形した他方の側板の対向
面の外周縁部に良好に溶接し得るようにしたプラネタリ
キャリアの製造方法を提供することをその目的としてい
る。
By the way, in the conventional method in which the leg pieces bent to one side plate of the planetary carrier are inserted into the engagement holes formed in the other side plate and welded, the other side plate is formed into the engagement hole. It is necessary to form a large diameter in order to secure a forming space, which causes a problem that the carrier becomes large. In this case, it is conceivable that the leg pieces are abutted against the outer peripheral edge portion of the opposite surface of the other side plate to the one side plate and welded, but as shown in FIG. When the cylindrical portion c extending to the opposite side to the opposite direction is press-molded, the outer peripheral edge portion of the opposite surface of the other side plate b to the one side plate a becomes a rounded portion curved toward the cylindrical portion c, and A portion of the tip of the piece d near the outer edge in the radial direction floats from the side plate b. Therefore, the leg piece d has to be welded to the side plate b only at the portion near the radial inner edge of the tip end, which makes it difficult to secure the welding strength, and further, the leg piece d that serves as the thrust receiving surface of the planetary gear. The welding spatter scatters on the radially inner part of the joining portion of, and a spatter removing step is required. In view of the above points, the present invention is a method for manufacturing a planetary carrier, in which a leg piece bent to one side plate can be welded favorably to the outer peripheral edge part of the facing surface of the other side plate press-molded on the tubular portion. Its purpose is to provide.

【0004】[0004]

【課題を解決するための手段】上記目的を達成すべく、
本発明は、プラネタリギアを挾んで対向する1対の側板
を備え、該両側板をその一方の側板の周囲複数箇所に曲
成した他方の側板に向ってのびる脚片を介して結合して
成るプラネタリキャリアであって、他方の側板の外周に
一方の側板との対向方向とは逆側にのびる筒部をプレス
成形して成るものの製造方法において、他方の側板の一
方の側板に対する対向面の外周縁部にコイニング加工に
より所定の位相で複数の座面を形成し、該各座面に前記
各脚片を突き当てて溶接することを特徴とする。
[Means for Solving the Problems] In order to achieve the above object,
The present invention is provided with a pair of side plates facing each other across a planetary gear, and the both side plates are connected to each other through leg pieces extending toward the other side plate bent at a plurality of locations around the one side plate. In a manufacturing method of a planetary carrier, which comprises press-molding a cylindrical portion extending on the outer periphery of the other side plate in a direction opposite to the facing direction of the one side plate, in the manufacturing method of the other side plate, the outer side of the facing surface to the one side plate is It is characterized in that a plurality of seating surfaces are formed at a predetermined phase on the peripheral portion by coining, and the leg pieces are abutted against the seating surfaces and welded.

【0005】[0005]

【作用】他方の側板の一方の側板に対する対向面の外周
縁部が筒部のプレス成形でアール部になっていても、コ
イニング加工により平坦な座面が形成され、脚片をその
先端が全面に亘って座面に密着するように突き当てた状
態で該座面に良好に溶接でき、更にコイニングエッジに
より脚片の接合箇所の径方向内方部分への溶接スパッタ
の飛散が防止される。また、座面を所定の位相で形成す
ることにより、座面を基準にして両側板を位相合わせし
て結合できる。尚、座面を切削加工で形成することも考
えられるが、本発明の如く座面をコイニング加工で形成
すれば、筒部を成形するプレス工程でコイニング加工を
行って座面を形成でき、工数を削減してコストダウンを
図れる。
The flat seating surface is formed by coining even if the outer peripheral edge of the opposite surface of the other side plate to the one side plate is rounded by press molding of the cylindrical portion, and the leg pieces have their entire tip ends. The seating surface can be welded to the seating surface in close contact with the seating surface, and the coining edges prevent the welding spatter from scattering radially inward at the joint of the leg pieces. Further, by forming the seat surface in a predetermined phase, both side plates can be phase-matched and joined with the seat surface as a reference. Although it is conceivable to form the seat surface by cutting, if the seat surface is formed by coining as in the present invention, the seat surface can be formed by coining in the press step of forming the tubular portion. To reduce costs.

【0006】[0006]

【実施例】図1乃至図3を参照して、1はダブルプラネ
タリキャリアであり、該キャリア1に軸方向に離間した
2組のプラネタリギア2、3が担持されている。該キャ
リア1は、軸方向一側の4個のプラネタリギア2を担持
する第1キャリア4と、軸方向他側の4対のデュアルプ
ラネタリギア3を担持する第2キャリア5とを連結して
構成され、2組のプラネタリギア2、3に共通のサンギ
ア軸S上のサンギアS1、S2を噛合させると共に、夫々
リングギアR1、R2を噛合させてプラネタリギア機構を
構成し、第2キャリア5に取付けたハブ6を介して出力
を取出すようにした。
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS Referring to FIGS. 1 to 3, reference numeral 1 denotes a double planetary carrier, which carries two sets of planetary gears 2 and 3 axially separated from each other. The carrier 1 is configured by connecting a first carrier 4 carrying four planetary gears 2 on one side in the axial direction and a second carrier 5 carrying four pairs of dual planetary gears 3 on the other side in the axial direction. The two sets of planetary gears 2, 3 mesh the sun gears S 1 , S 2 on the common sun gear shaft S, and the ring gears R 1 , R 2 mesh with each other to form a planetary gear mechanism. The output is taken out through the hub 6 attached to the carrier 5.

【0007】第1と第2の各キャリア4、5は、軸方向
内側の側板41、51と軸方向外側の側板42、52と
を備えており、外側の側板42、52の周囲複数箇所に
曲成した軸方向内側にのびる脚片43、53の先端を内
側の側板41、51に溶接して各キャリア4、5を製造
する。その後、各キャリア4、5の両側板間に各プラネ
タリギア2、3をその両端にワッシャ21、31を添接
させた状態で挿入し、次いでプラネタリギア2、3の内
周に装着したニードルベアリング22、32に貫通する
ギア軸23、33を両側板に跨るように組付けた後、ギ
ア軸23、33をその両端をかしめて各キャリア4、5
に固定し、キャリアアッセンブリの組立を行う。第2キ
ャリア5の内側の側板51の外周には、該側板51に対
向する第1キャリア4の内側の側板41を受け入れる筒
部51aがプレス成形されており、該側板41の外周と
筒部51aとに夫々外向きと内向きのセレーション歯4
5、55を形成して、第1と第2の両キャリア4、5を
セレーション係合させ、次いで筒部51aの先端の周囲
複数箇所をかしめ、このかしめ部56を側板41に係合
させて両キャリア4、5を軸方向に抜け止めし、ダブル
プラネタリキャリア1の組立を行う。
Each of the first and second carriers 4, 5 is provided with side plates 41, 51 on the inner side in the axial direction and side plates 42, 52 on the outer side in the axial direction, and at a plurality of locations around the outer side plates 42, 52. The carriers 4, 5 are manufactured by welding the ends of the bent leg pieces 43, 53 extending inward in the axial direction to the inner side plates 41, 51. After that, the planetary gears 2 and 3 are inserted between both side plates of the carriers 4 and 5 with the washers 21 and 31 attached to both ends of the planetary gears 2 and 3, and then the needle bearings attached to the inner circumferences of the planetary gears 2 and 3. After assembling the gear shafts 23 and 33 penetrating the gears 22 and 32 so as to straddle the both side plates, the gear shafts 23 and 33 are caulked at both ends, and each carrier 4, 5 is attached.
Then, assemble the carrier assembly. On the outer periphery of the side plate 51 on the inner side of the second carrier 5, a cylinder portion 51a that faces the side plate 51 and receives the side plate 41 on the inner side of the first carrier 4 is press-molded, and the outer periphery of the side plate 41 and the cylinder portion 51a. And outward serration teeth 4 respectively
5, 55 are formed, the first and second carriers 4, 5 are engaged in serrations, then a plurality of locations around the tip of the tubular portion 51a are swaged, and the swaged portions 56 are engaged with the side plate 41. Both carriers 4, 5 are prevented from coming off in the axial direction, and the double planetary carrier 1 is assembled.

【0008】尚、両キャリア4、5の内側の側板41、
51間にはオイルプレート7が介挿されており、サンギ
ア軸Sに形成した油孔Saから供給される潤滑油をオイ
ルプレート7に形成した油溝を介して各プラネタリギア
2、3のギア軸23、33に形成した油孔24、34に
給油し得るようにした。
The side plates 41 inside the carriers 4 and 5,
The oil plate 7 is interposed between the gears 51, and the lubricating oil supplied from the oil hole Sa formed in the sun gear shaft S is passed through the oil groove formed in the oil plate 7 to the gear shaft of each planetary gear 2, 3. Oil can be supplied to the oil holes 24 and 34 formed in the holes 23 and 33.

【0009】ここで、第1キャリア4では、内側の側板
41に複数の係合孔44を形成して、該各孔44に各脚
片43の先端を挿入して溶接しているが、第2キャリア
5では、内側の側板51の外側の側板52に対する対向
面の外周縁部にコイニング加工により所定の位相で複数
の座面54を形成し、各脚片53を各座面54に突き当
てて両側板51、52を位相合わせし、脚片53の接合
部に径方向外方からレーザービームを照射して、図4に
示す如く脚片53を座面54に溶接するようにした。
Here, in the first carrier 4, a plurality of engagement holes 44 are formed in the inner side plate 41, and the tips of the leg pieces 43 are inserted into the holes 44 and welded. In the 2 carrier 5, a plurality of seat surfaces 54 are formed at a predetermined phase by coining on the outer peripheral edge of the surface of the inner side plate 51 facing the outer side plate 52, and each leg piece 53 is abutted against each seat surface 54. The two side plates 51 and 52 are aligned with each other, and the joint portion of the leg piece 53 is irradiated with a laser beam from the outside in the radial direction so that the leg piece 53 is welded to the seat surface 54 as shown in FIG.

【0010】座面54のコイニング加工は、図5に示す
プレス金型で筒部51aにセレーション歯55を成形す
る際に行われるもので、以下これを詳述する。プレス金
型は、下型100と昇降動される上型101とを備えて
おり、下型100に、筒部51aを予めプレス成形した
側板51を下向きにして外嵌セットするダイ102と、
ダイ102の周囲に位置させて図6に示す如く放射方向
に進退自在な複数の歯形パンチ103とを設け、一方、
上型101には、側板51をダイ102上に挾圧するパ
ッド104をばね104aで下方に付勢して取付けると
共に、歯形パンチ103を放射方向内方に押動するドラ
イバカム105を垂設した。ダイ102の外周面にはセ
レーション歯55に対応する歯溝102aが形成されて
おり、上型101の下動によりドライバカム105を介
して歯形パンチ103を放射方向内方に押動させ、該パ
ンチ103により筒部51aを歯溝102aに押し込ん
でセレーション歯55をプレス成形するようにし、更
に、パッド104の下面に図7に示す如くコイニング加
工用の突部104bを設け、シャットハイト状態で側板
51の前記対向面となる上面の外周縁部に該突部104
bによって座面54をコイニング加工するようにした。
The coining of the seat surface 54 is performed when the serration teeth 55 are formed on the tubular portion 51a with the press die shown in FIG. 5, which will be described in detail below. The press die includes a lower die 100 and an upper die 101 which is moved up and down, and a die 102 for externally fitting and setting the side plate 51 on which the tubular portion 51a is preformed in a downward direction on the lower die 100,
A plurality of tooth-shaped punches 103, which are located around the die 102 and can move back and forth in the radial direction as shown in FIG. 6, are provided.
A pad 104 for pressing the side plate 51 onto the die 102 is attached to the upper die 101 by urging it downward with a spring 104a, and a driver cam 105 for vertically pushing the tooth-shaped punch 103 in the radial direction is provided vertically. A tooth groove 102a corresponding to the serration teeth 55 is formed on the outer peripheral surface of the die 102, and when the upper die 101 is moved downward, the tooth profile punch 103 is pushed inward in the radial direction via the driver cam 105. The cylindrical portion 51a is pushed into the tooth groove 102a by 103 so that the serration teeth 55 are press-molded. Further, as shown in FIG. 7, a protrusion 104b for coining is provided on the lower surface of the pad 104, and the side plate 51 is kept in a shut height state. Of the protrusion 104 on the outer peripheral edge of the upper surface that is the opposite surface of the
The seating surface 54 is coined by b.

【0011】これによれば、側板51の上面外周縁部の
アール部分が押し潰されて平坦な座面54が形成され、
図4に示す如く脚片53の先端をその全面に亘って座面
54に密着させた状態で座面54に溶接できるようにな
り、更に、コイニングエッジ54aにより脚片53の接
合箇所の径方向内方部分への溶接スパッタの飛散が防止
され、スパッタの除去工程が不要となる。
According to this, the rounded portion of the outer peripheral portion of the upper surface of the side plate 51 is crushed to form the flat seat surface 54,
As shown in FIG. 4, the tip end of the leg piece 53 can be welded to the seat surface 54 in a state in which the tip end of the leg piece 53 is in close contact with the seat surface 54 over the entire surface thereof. Scattering of welding spatter to the inner part is prevented, and a spatter removing step is unnecessary.

【0012】尚、筒部51aのプレス成形時に座面54
をコイニング加工することも可能である。また、本発明
は、上記実施例の如きダブルプラネタリキャリア1用の
キャリア5に限らず、片側の側板に筒部をプレス成形す
るプラネタリキャリアの製造に広く適用できる。
The seat surface 54 is formed during the press forming of the tubular portion 51a.
It is also possible to perform coining. Further, the present invention is not limited to the carrier 5 for the double planetary carrier 1 as in the above embodiment, but can be widely applied to the manufacture of a planetary carrier in which a tubular portion is press-molded on one side plate.

【0013】[0013]

【発明の効果】以上の説明から明らかなように、本発明
によれば、プラネタリキャリアの一方の側板に対する他
方の側板の対向面の外周縁部が該他方の側板に筒部をプ
レス成形することによりアール部になっても、該外周縁
部に所定の位相で座面を形成することにより、両側板を
位相合わせした状態で、一方の側板に曲成した脚片を該
座面において該外周縁部に良好に突き当て溶接でき、更
に、脚片の接合箇所の径方向内方部分への溶接スパッタ
の飛散を防止できて、スパッタの除去工程が不要とな
り、且つ座面をコイニング加工で形成するため、他方の
側板のプレス工程において座面を形成でき、工数を削減
してコストダウンを図れる。
As is apparent from the above description, according to the present invention, the outer peripheral edge portion of the facing surface of the other side plate to the one side plate of the planetary carrier is formed by press-molding the tubular portion on the other side plate. Even if it becomes a rounded part by forming a seat surface at a predetermined phase on the outer peripheral edge part, a leg piece bent to one side plate is formed on the seat surface in the state where both side plates are aligned with each other. It is possible to butt weld well to the peripheral edge, and further, it is possible to prevent the spatter of welding spatter to the radially inner part of the joint part of the leg piece, eliminating the spatter removal step and forming the seat surface by coining. Therefore, the seating surface can be formed in the pressing process of the other side plate, and the number of steps can be reduced and the cost can be reduced.

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

【図1】 本発明で製造されたキャリアを具備するダブ
ルプラネタリキャリアの縦断面図
FIG. 1 is a vertical sectional view of a double planetary carrier including a carrier manufactured by the present invention.

【図2】 図1の右側面図FIG. 2 is a right side view of FIG.

【図3】 図1の左側面図FIG. 3 is a left side view of FIG.

【図4】 本発明で製造されたキャリアの脚片の接合部
を示す拡大断面図
FIG. 4 is an enlarged cross-sectional view showing a joint portion of leg pieces of a carrier manufactured by the present invention.

【図5】 そのキャリアの筒部にセレーション歯を成形
するプレス金型の截断側面図
FIG. 5 is a cutaway side view of a press die for forming serration teeth on the tubular portion of the carrier.

【図6】 図5のVI−VI線拡大断面図6 is an enlarged sectional view taken along line VI-VI of FIG.

【図7】 図6のVII−VII線截断面図7 is a sectional view taken along the line VII-VII in FIG.

【図8】 座面を形成せずに脚片を突き当て溶接した場
合の脚片の接合部を示す断面図
FIG. 8 is a cross-sectional view showing a joint portion of the leg pieces when the leg pieces are butted and welded without forming a seat surface.

【符号の説明】[Explanation of symbols]

5 第2キャリア(本発明で製造されるプラネタリキャ
リア) 51 他方の側板 51a 筒部 52 一方の側板 53 脚片 54 座面
5 2nd carrier (planetary carrier manufactured by this invention) 51 Other side plate 51a Cylindrical part 52 One side plate 53 Leg piece 54 Seat surface

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】 プラネタリギアを挾んで対向する1対の
側板を備え、該両側板をその一方の側板の周囲複数箇所
に曲成した他方の側板に向ってのびる脚片を介して結合
して成るプラネタリキャリアであって、他方の側板の外
周に一方の側板との対向方向とは逆側にのびる筒部をプ
レス成形して成るものの製造方法において、他方の側板
の一方の側板に対する対向面の外周縁部にコイニング加
工により所定の位相で複数の座面を形成し、該各座面に
前記各脚片を突き当てて溶接することを特徴とするプラ
ネタリキャリアの製造方法。
1. A pair of side plates facing each other across a planetary gear, wherein the both side plates are coupled to each other through leg pieces extending toward the other side plate curved at a plurality of locations around the one side plate. A planetary carrier consisting of, in the manufacturing method of what is formed by press-molding a cylindrical portion extending to the outer periphery of the other side plate in the opposite direction to the facing direction of the one side plate, in the manufacturing method of the opposite surface of the other side plate to the one side plate. A method of manufacturing a planetary carrier, comprising forming a plurality of seat surfaces at a predetermined phase on the outer peripheral edge portion by coining, and abutting and welding the leg pieces to the seat surfaces.
JP23569592A 1992-09-03 1992-09-03 Method for manufacturing planetary carrier Expired - Fee Related JP3205947B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP23569592A JP3205947B2 (en) 1992-09-03 1992-09-03 Method for manufacturing planetary carrier

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP23569592A JP3205947B2 (en) 1992-09-03 1992-09-03 Method for manufacturing planetary carrier

Publications (2)

Publication Number Publication Date
JPH0681907A true JPH0681907A (en) 1994-03-22
JP3205947B2 JP3205947B2 (en) 2001-09-04

Family

ID=16989855

Family Applications (1)

Application Number Title Priority Date Filing Date
JP23569592A Expired - Fee Related JP3205947B2 (en) 1992-09-03 1992-09-03 Method for manufacturing planetary carrier

Country Status (1)

Country Link
JP (1) JP3205947B2 (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100736949B1 (en) * 2005-11-30 2007-07-09 현대자동차주식회사 Planet carrier
JP2008089051A (en) * 2006-09-29 2008-04-17 Aisin Aw Co Ltd Planetary gear device
JP2008209010A (en) * 2008-06-09 2008-09-11 Kikuchi Co Ltd Power transmission component
DE102009027066A1 (en) * 2009-06-22 2010-12-23 Zf Friedrichshafen Ag Welded component, in particular planet carrier, method for producing the component and apparatus for carrying out the method
WO2013088860A1 (en) * 2011-12-16 2013-06-20 アイシン・エィ・ダブリュ株式会社 Planetary carrier
JP2020085017A (en) * 2018-11-16 2020-06-04 住友重機械工業株式会社 Eccentric oscillation type speed reduction device

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100736949B1 (en) * 2005-11-30 2007-07-09 현대자동차주식회사 Planet carrier
JP2008089051A (en) * 2006-09-29 2008-04-17 Aisin Aw Co Ltd Planetary gear device
JP2008209010A (en) * 2008-06-09 2008-09-11 Kikuchi Co Ltd Power transmission component
DE102009027066A1 (en) * 2009-06-22 2010-12-23 Zf Friedrichshafen Ag Welded component, in particular planet carrier, method for producing the component and apparatus for carrying out the method
WO2013088860A1 (en) * 2011-12-16 2013-06-20 アイシン・エィ・ダブリュ株式会社 Planetary carrier
CN103797278A (en) * 2011-12-16 2014-05-14 爱信艾达株式会社 Planetary carrier
JP5668871B2 (en) * 2011-12-16 2015-02-12 アイシン・エィ・ダブリュ株式会社 Planetary carrier
US9157521B2 (en) 2011-12-16 2015-10-13 Aisin Aw Co., Ltd. Planetary carrier
JP2020085017A (en) * 2018-11-16 2020-06-04 住友重機械工業株式会社 Eccentric oscillation type speed reduction device

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