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JPS6133965B2 - - Google Patents
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JPS6133965B2 - - Google Patents

Info

Publication number
JPS6133965B2
JPS6133965B2 JP19370681A JP19370681A JPS6133965B2 JP S6133965 B2 JPS6133965 B2 JP S6133965B2 JP 19370681 A JP19370681 A JP 19370681A JP 19370681 A JP19370681 A JP 19370681A JP S6133965 B2 JPS6133965 B2 JP S6133965B2
Authority
JP
Japan
Prior art keywords
wheel
machining
center hole
outer end
thick
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
Application number
JP19370681A
Other languages
Japanese (ja)
Other versions
JPS5896101A (en
Inventor
Hiroshi Okunishi
Akira Namiki
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 JP19370681A priority Critical patent/JPS5896101A/en
Publication of JPS5896101A publication Critical patent/JPS5896101A/en
Publication of JPS6133965B2 publication Critical patent/JPS6133965B2/ja
Granted legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02Blade-carrying members, e.g. rotors
    • F01D5/04Blade-carrying members, e.g. rotors for radial-flow machines or engines
    • F01D5/043Blade-carrying members, e.g. rotors for radial-flow machines or engines of the axial inlet- radial outlet, or vice versa, type

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Description

【発明の詳細な説明】 本発明はエンジン用の過給機におけるタービン
ホイールの製造方法に関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a method for manufacturing a turbine wheel in a supercharger for an engine.

従来この種方法として、例えば第1図示のよう
にタービンホイールaをチタン合金その他の耐熱
性合金の鋳造により形成させた後これを作動軸b
の端部に摩擦溶接その他で結着させ、次でこれを
機械加工すべく該ホイールaの外端にセンタ孔c
を加工する式のものは知られるが、この場合該ホ
イールaは仝図示のように内部に中空部を有しな
いばかりでなく該センタ孔cの加工に備えてその
外端に長手にのびる肉厚部dを一体に有するもの
で、かゝるものでは全体として比較的大重量とな
り、これが該作動軸bを支承する中間の軸受eに
対しその外側にオーバハングして存する状態とな
り、かくてその作動によれば該軸受eに比較的大
きな負荷を与え勝ちである不都合を伴う。
Conventionally, this type of method involves forming a turbine wheel a by casting a titanium alloy or other heat-resistant alloy as shown in the first figure, and then forming the turbine wheel a into an operating shaft b.
A center hole c is attached to the outer end of the wheel a to be attached by friction welding or other means to the end of the wheel a, and then machined.
However, in this case, the wheel a not only does not have a hollow part inside as shown in the figure, but also has a thick wall extending longitudinally at the outer end in preparation for machining the center hole c. The part d is integrated, and such a part has a relatively large weight as a whole, and it overhangs the intermediate bearing e that supports the operating shaft b, thus hindering its operation. According to this method, a relatively large load is likely to be applied to the bearing e, which is disadvantageous.

本発明はかゝる不都合のないホイールを得る方
法を提供することをその目的としたもので、ター
ビンホイールをチタン合金その他の耐熱性合金の
鋳造により形成させた後これを作動軸の端部に摩
擦溶接その他で結着させ、次で該ホイールの外端
にセンタ孔を加工して研削その他の機械加工に備
える式のものにおいて、該ホイールを予め該セン
タ孔の加工に備えて外端に肉厚部と、その内側に
長さ方向にのびる中空部とを有する中空体に形成
させ、該機械加工の後に該肉厚部を除去して該中
空部を開口させて成る。
The object of the present invention is to provide a method for obtaining a wheel free of such disadvantages, in which the turbine wheel is formed by casting titanium alloy or other heat-resistant alloy and then attached to the end of the operating shaft. In the case of a type in which the wheel is joined by friction welding or other means, and then a center hole is machined in the outer end of the wheel in preparation for grinding or other machining, the outer end of the wheel is thinned in advance in preparation for machining the center hole. It is formed into a hollow body having a thick part and a hollow part extending in the length direction inside the thick part, and after the machining, the thick part is removed and the hollow part is opened.

本発明実施例の1例を別紙図面に付説明する。 An example of an embodiment of the present invention will be explained with reference to attached drawings.

第2図及び第3図はその1例を示すもので、1
はタービンホイールを示し、該ホイール1はチタ
ン合金その他の耐熱性合金の鋳造により作られる
ものとし、これを作動軸2の端部に摩擦溶接によ
り結着させた後、その外端にセンタ孔3を加工し
て研削その他の機械加工に備えるもので、この点
は従来のものと特に異らないが、本発明によれ
ば、該ホイール1を予め第3図示のように該セン
タ孔3の加工に備えて外端に肉厚部1aとその内
側に長さ方向にのびる中空部1bとを有する中空
体に形成させ、これを該作動軸2に結着すると共
にその外端に該センタ孔3を加工してこれに機械
加工を施した後、次で該肉厚部1aを切削その他
により除去して該中空部1aを外部に開口させ
る。この状態は第2図示の通りであり、図中4は
該作動軸2の他端のコンプレツサホイール、5は
その中間部の軸受を示す。尚これを使用する過給
機の全体は例えば第4図示の通りであり、該ター
ビンホイール1と該コンプレツサホイール4とは
中間の枠筐6から両外側にのびて該ホイール1は
エンジンの排気通路7内と該ホイール4は吸気通
路8内とに夫々介入されるものである。
Figures 2 and 3 show one example.
indicates a turbine wheel, and the wheel 1 is made by casting titanium alloy or other heat-resistant alloy, and after bonding it to the end of the operating shaft 2 by friction welding, a center hole 3 is formed at the outer end. The wheel 1 is prepared for grinding and other machining operations, and this point is not particularly different from conventional wheels. However, according to the present invention, the center hole 3 of the wheel 1 is machined in advance as shown in the third figure. In preparation for this, a hollow body is formed having a thick wall portion 1a at the outer end and a hollow portion 1b extending in the length direction inside the thick wall portion 1a, and this is connected to the actuating shaft 2, and the center hole 3 is formed at the outer end of the hollow body. After processing and performing machining on this, the thick portion 1a is then removed by cutting or other means to open the hollow portion 1a to the outside. This state is as shown in the second figure, in which reference numeral 4 indicates a compressor wheel at the other end of the operating shaft 2, and reference numeral 5 indicates a bearing at an intermediate portion thereof. The entire supercharger that uses this is as shown in FIG. The inside of the passage 7 and the wheel 4 are inserted into the inside of the intake passage 8, respectively.

このように本発明によるときはタービンホイー
ルを予め外端に肉厚部を有する中空体とし、該肉
厚部のセンタ孔を加工して機械加工を施した後は
該肉厚部を除去して内部の中空部を開口させるも
ので、機械加工に不都合を生ずることがないと共
に該ホイールは製品の状態において全体として極
めて軽量となりこれが軸受に大きな負荷を与える
ようなことがなく、作動を円滑且確実にする等の
効果を有する。
In this way, according to the present invention, the turbine wheel is made into a hollow body having a thick walled portion at the outer end in advance, and after machining is performed by machining the center hole of the thick walled portion, the thick walled portion is removed. The internal hollow part is opened, so there is no problem with machining, and the wheel is extremely lightweight as a product, which does not put a large load on the bearing, allowing smooth and reliable operation. It has the effect of making it.

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

第1図は従来例の説明線図、第2図及び第3図
は本発明方法の1例の説明線図、第4図はその製
品を使用した過給機の1例の截断側面図である。 1……タービンホイール、2……作動軸、3…
…センタ孔、1a……肉厚部、1b……中空部。
Fig. 1 is an explanatory diagram of a conventional example, Figs. 2 and 3 are explanatory diagrams of an example of the method of the present invention, and Fig. 4 is a cutaway side view of an example of a supercharger using the product. be. 1... Turbine wheel, 2... Operating shaft, 3...
...Center hole, 1a... Thick part, 1b... Hollow part.

Claims (1)

【特許請求の範囲】[Claims] 1 タービンホイールをチタン合金その他の耐熱
性合金の鋳造により形成させた後これを作動軸の
端部に摩擦溶接その他で結着させ、次で該ホイー
ルの外端にセンタ孔を加工して研削その他の機械
加工に備える式のものにおいて、該ホイールを予
め該センタ孔の加工に備えて外端に肉厚部と、そ
の内側に長さ方向にのびる中空部とを有する中空
体に形成させ、該機械加工の後に該肉厚部を除去
して該中空部を開口させて成るタービンホイール
の製造方法。
1. After forming a turbine wheel by casting a titanium alloy or other heat-resistant alloy, it is attached to the end of the operating shaft by friction welding or other means, and then a center hole is machined in the outer end of the wheel, and the wheel is ground, etc. In a type prepared for machining, the wheel is formed in advance into a hollow body having a thick part at the outer end and a hollow part extending in the length direction inside the thick part in preparation for the machining of the center hole. A method of manufacturing a turbine wheel, which comprises removing the thick part and opening the hollow part after machining.
JP19370681A 1981-12-03 1981-12-03 Turbine wheel manufacturing method Granted JPS5896101A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP19370681A JPS5896101A (en) 1981-12-03 1981-12-03 Turbine wheel manufacturing method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP19370681A JPS5896101A (en) 1981-12-03 1981-12-03 Turbine wheel manufacturing method

Publications (2)

Publication Number Publication Date
JPS5896101A JPS5896101A (en) 1983-06-08
JPS6133965B2 true JPS6133965B2 (en) 1986-08-05

Family

ID=16312424

Family Applications (1)

Application Number Title Priority Date Filing Date
JP19370681A Granted JPS5896101A (en) 1981-12-03 1981-12-03 Turbine wheel manufacturing method

Country Status (1)

Country Link
JP (1) JPS5896101A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6151471U (en) * 1984-09-10 1986-04-07

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS60101201A (en) * 1983-11-08 1985-06-05 Ngk Spark Plug Co Ltd Joining structure in turbine shaft
JPH0652047B2 (en) * 1985-04-02 1994-07-06 川崎重工業株式会社 Method for manufacturing turbine rotor for supercharger
WO2006117847A1 (en) * 2005-04-27 2006-11-09 Hitachi, Ltd. Micro gas turbine
JP2007120409A (en) * 2005-10-28 2007-05-17 Daido Castings:Kk Hot wheel for turbocharger
KR20120042728A (en) * 2009-04-09 2012-05-03 바스프 에스이 Process for producing a turbine wheel for an exhaust gas turbocharger
JP5966417B2 (en) * 2012-02-20 2016-08-10 株式会社Ihi Turbocharger

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6151471U (en) * 1984-09-10 1986-04-07

Also Published As

Publication number Publication date
JPS5896101A (en) 1983-06-08

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