JPS5896101A - Manufacturing method of turbine wheel - Google Patents

Manufacturing method of turbine wheel

Info

Publication number
JPS5896101A
JPS5896101A JP19370681A JP19370681A JPS5896101A JP S5896101 A JPS5896101 A JP S5896101A JP 19370681 A JP19370681 A JP 19370681A JP 19370681 A JP19370681 A JP 19370681A JP S5896101 A JPS5896101 A JP S5896101A
Authority
JP
Japan
Prior art keywords
wheel
turbine wheel
center hole
hollow
outer end
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
JP19370681A
Other languages
Japanese (ja)
Other versions
JPS6133965B2 (en
Inventor
Hiroshi Okunishi
弘 奥西
Akira Namiki
公 並木
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 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)

Abstract

PURPOSE:To improve a turbine wheel in its weight and others by using a hollow body previously provided with a thick part on its outer end in the process of its production. CONSTITUTION:A turbine wheel 1 made of titanium alloy or other heat-resisting alloys is shaped into a hollow body with a thick part 1a and a hollow part 1b extended inward in previous preparation for the processing of a center hole 3. This turbine wheel is combined with an operation shaft 2, and the center hole 3 is processed by machinery. Then, the thick part 1a is removed, and the hollow part 1b is opened to the outside. This method permits to manufacture the turbine wheel at a light weight.

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.

従来この種畜法として、例えば第1v!i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すの端部に摩擦溶接
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0を加工する式のものは知られる
が、この場合該ホイール1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O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−るものでは全体として比較的大重量となり、これ
が該作動軸すを支承する中間の軸受・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・に比較的大きな負荷を与え勝ちである不
都合を伴う。
Conventionally, as this breeding stock method, for example, 1st v! As shown in i, a turbine wheel a is formed by casting a titanium alloy or other heat-resistant alloy, and then it is attached to the end of the operating shaft by friction welding or other means, and then the wheel is machined to be machined. A type of wheel 1 in which a center hole 0 is machined at the outer end of the wheel 1 is known, but in this case, the wheel 1 not only does not have a hollow part inside as shown in the figure, but also has a hole in the center hole 0 in preparation for machining the center hole 0. The outer end has a longitudinally extending thick wall part d, which is relatively heavy as a whole, and this overhangs the intermediate bearing that supports the operating shaft. This situation is accompanied by the disadvantage that its operation is likely to impose a relatively large load on the bearing.

本発明はか−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シ賞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。
SUMMARY OF THE INVENTION 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 a 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 wheel is attached in advance to the outer end in preparation for machining the center hole. Formed into a hollow body having a thick part and a hollow part extending in the length direction inside the thick part,
After the machining, the thick portion is removed to open the hollow portion.

本発明実施の1例を別紙図面に付説明する。An example of implementing the present invention will be explained with reference to the 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(liを予め第5
図示のように該センタ孔(3)の加工に備えて外端に肉
厚1%(1m)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(
21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(1b)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)の他端のコンプレッサホイール
、(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)と該コンプレッサホイール(4)とは
中間の枠管(6)から両外側にのびて該ホイール(11
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, and (1) shows a turbine wheel, which is made by casting titanium alloy or other heat-resistant alloy. (2) is attached to the end by friction welding, and then a center hole (3) is machined at the outer end to prepare for grinding or other machining, and this point is not particularly different from the conventional one. However, according to the present invention, the wheel (li) is
As shown in the figure, in preparation for machining the center hole (3), there is a wall thickness of 1% (1 m) at the outer end and a hollow part (
1b), and this is formed into a hollow body having the actuating shaft (1b).
21 and machined the center hole (3) at its outer end, then the thick part (1a
) is removed by cutting or other means to open the hollow part (1b) to the outside. This state is as shown in the second figure, in which (4) indicates the compressor wheel at the other end of the operating shaft (2), and (5) indicates the bearing at the middle thereof. The entire supercharger that uses this is as shown in FIG. (11
The wheel (4) is inserted into the exhaust passage (7) of the engine, and the wheel (4) is inserted into the intake passage (8).

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、該肉厚部にセンタ孔
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
ずあ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。
As described above, 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 a center hole in 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 bearings and allows for smooth operation. In addition, it has the effect of ensuring reliability.

【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2FI!J及び第5図は
本発明方法の1例の説明m図、第4図はその製品を使用
した過給機の1例の裁断側面図である。 (1)・・・・・・タービンホイール (21・・・・・・作 動 軸 (3)・・・・・・センタ孔 (1a)・・・肉 厚 部 (1b)・・・中 空 部 外2名 第4図
Figure 1 is an explanatory diagram of the conventional example, and the 2nd FI! Figures J and 5 are explanatory diagrams of an example of the method of the present invention, and Figure 4 is a cut side view of an example of a supercharger using the product. (1)...Turbine wheel (21...Operating shaft (3)...Center hole (1a)...Thick wall part (1b)...Hollow 2 outsiders Figure 4

Claims (1)

【特許請求の範囲】[Claims] 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、該機械加工の俵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
A turbine wheel is formed by casting a titanium alloy or other heat-resistant alloy, and then 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 then ground or otherwise In a type that is prepared for machining, the wheel is formed in advance into a hollow body having a thick wall portion at the outer end and a hollow portion extending in the length direction inside the wheel in preparation for machining the center hole. A method for manufacturing a turbine wheel comprising removing the thick part of a processed bale and opening the hollow part.
JP19370681A 1981-12-03 1981-12-03 Manufacturing method of turbine wheel Granted JPS5896101A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP19370681A JPS5896101A (en) 1981-12-03 1981-12-03 Manufacturing method of turbine wheel

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP19370681A JPS5896101A (en) 1981-12-03 1981-12-03 Manufacturing method of turbine wheel

Publications (2)

Publication Number Publication Date
JPS5896101A true JPS5896101A (en) 1983-06-08
JPS6133965B2 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 Manufacturing method of turbine wheel

Country Status (1)

Country Link
JP (1) JPS5896101A (en)

Cited By (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
JPS61229901A (en) * 1985-04-02 1986-10-14 Kawasaki Heavy Ind Ltd 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
US20120034084A1 (en) * 2009-04-09 2012-02-09 Basf Se Process for producing a turbine wheel for an exhaust gas turbocharger
JP2013170487A (en) * 2012-02-20 2013-09-02 Ihi Corp Supercharger

Families Citing this family (1)

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

Cited By (8)

* 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
JPH0351881B2 (en) * 1983-11-08 1991-08-08 Ngk Spark Plug Co
JPS61229901A (en) * 1985-04-02 1986-10-14 Kawasaki Heavy Ind Ltd Turbine rotor for supercharger
WO2006117847A1 (en) * 2005-04-27 2006-11-09 Hitachi, Ltd. Micro gas turbine
JPWO2006117847A1 (en) * 2005-04-27 2008-12-18 株式会社日立製作所 Micro gas turbine
JP2007120409A (en) * 2005-10-28 2007-05-17 Daido Castings:Kk Hot wheel for turbocharger
US20120034084A1 (en) * 2009-04-09 2012-02-09 Basf Se Process for producing a turbine wheel for an exhaust gas turbocharger
JP2013170487A (en) * 2012-02-20 2013-09-02 Ihi Corp Supercharger

Also Published As

Publication number Publication date
JPS6133965B2 (en) 1986-08-05

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