JPS58176499A - Fitting device for compressor wheel - Google Patents
Fitting device for compressor wheelInfo
- Publication number
- JPS58176499A JPS58176499A JP57058181A JP5818182A JPS58176499A JP S58176499 A JPS58176499 A JP S58176499A JP 57058181 A JP57058181 A JP 57058181A JP 5818182 A JP5818182 A JP 5818182A JP S58176499 A JPS58176499 A JP S58176499A
- Authority
- JP
- Japan
- Prior art keywords
- shaft
- wheel
- compressor wheel
- hole
- peripheral surface
- 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
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D1/00—Couplings for rigidly connecting two coaxial shafts or other movable machine elements
- F16D1/06—Couplings for rigidly connecting two coaxial shafts or other movable machine elements for attachment of a member on a shaft or on a shaft-end
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/025—Fixing blade carrying members on shafts
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Supercharger (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
Description
【発明の詳細な説明】
本発明は、ターlチャージャに用いるコンゾレツサホイ
ールの嵌合装置に関する。DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a fitting device for a console wheel used in a tar charger.
従来、ターlチャージャにおいては、コンゾレツサホイ
ールに軸孔を形成してこれにタービンシャフトを嵌合さ
せるを一般とするが、この場合コンプレッサケ−スとタ
ービンシャフトとは、木組付けに先立ち仮組付けしての
/?ランス取りを行う関係で、その着脱を容易にすべく
すきま嵌めにするを一般とし、その結果すきま嵌めのク
リアランスに相当する偏心を生じて超精密なバランスを
得にくくなる不都合を伴う。Conventionally, in a turbocharger, a shaft hole is generally formed in the compressor wheel and a turbine shaft is fitted into the shaft hole, but in this case, the compressor case and turbine shaft are first assembled with wood before being assembled. Temporarily assembled/? When lancing is performed, it is common to use a loose fit to facilitate attachment and detachment, but as a result, eccentricity corresponding to the clearance of the loose fit occurs, making it difficult to obtain ultra-precise balance.
又、嵌合をテーパ軸とチー・ゼ穴とで行う方法もあるが
、この場合はコンゾレッサホイールのタービンシャフト
に対する軸方向の嵌合深さがテーパぞによって規制され
、テーパぞ軸とテーパ穴とを高精度で加工しないと軸方
向位置にばらつきを生ずる不都合を伴う。There is also a method of fitting between a tapered shaft and a cheese hole, but in this case, the depth of fit in the axial direction of the conzoresor wheel to the turbine shaft is regulated by the taper groove; If the holes are not machined with high precision, there will be an inconvenience that variations will occur in the axial position.
本発明は、かかる不都合を解消した装置を提供すること
をその目的とするもので、コンプレッサケ−スに軸孔を
形成してこれにタービンシャフトを嵌合させるものにお
いて、該軸孔の内周面と該タービンシャフトの外周面と
の何れか方に締めじろを得るための円弧状膨出部を形成
して成る。SUMMARY OF THE INVENTION An object of the present invention is to provide a device that eliminates such inconveniences, and in which a shaft hole is formed in a compressor case and a turbine shaft is fitted into the shaft hole, An arcuate bulge is formed on either the surface or the outer circumferential surface of the turbine shaft to provide a tightening margin.
図面で(1)はエンジンの吸気通路に介在させるコンプ
レッサケース(2)内のコンゾレツサホイール、(3)
はエンジンの排気通路に介在させるタービンケース(4
)内のタービンホイールを示し、咳タービンホイール(
3)から一体にのびるタービンシャ7N51を該コンプ
レッサホイール(1)に形成する軸孔(6)に嵌合貫通
させて、その先端のナツト(7)で該ホイール(1)に
締結するものとした。In the drawing, (1) shows the consolator wheel in the compressor case (2), which is interposed in the intake passage of the engine, and (3)
is a turbine case (4) interposed in the exhaust passage of the engine.
) shows the turbine wheel in the cough turbine wheel (
3) The turbine shaft 7N51 extending integrally from the compressor wheel (1) is fitted into and penetrates the shaft hole (6) formed in the compressor wheel (1), and is fastened to the wheel (1) with a nut (7) at its tip. .
図面で(81(91は該シャ7N5+に挿通したスラス
トカラーとシールリングカラーを示し、該シールリング
カラー(9)を位置決め部材としてこれと該コンプレッ
サホイール(1)との当接で該ホイール(1)の該シャ
フト(5)に対する軸方向位置が決定されるようにした
。In the drawing (81 (91) indicates a thrust collar and a seal ring collar inserted into the shaft 7N5+, the seal ring collar (9) is used as a positioning member, and when this and the compressor wheel (1) come into contact, the wheel (1 ) with respect to the shaft (5) is determined.
以上は上記した従来式のものと特に異らないが本発明に
よれば軸孔(6)の内周面とタービンシャ7N51の外
周面との何れか一方、例えば第2図示の如くタービンシ
ャフト(5)の外周面或いは第3図示の如く軸孔(6)
の内周面に締めじろを得るための円弧状膨出部QQIを
形成した。Although the above is not particularly different from the conventional type described above, according to the present invention, either one of the inner circumferential surface of the shaft hole (6) and the outer circumferential surface of the turbine shaft 7N51, for example, as shown in the second figure, the turbine shaft ( 5) or the shaft hole (6) as shown in the third figure.
An arcuate bulge QQI was formed on the inner circumferential surface of the cylinder to obtain a tightening margin.
該膨出部0Iは、整形砥石による研削加工でも又旋削加
工でも成形可能であり、その寸法は1〜2μ程度の極め
てわずかな締めしるが得られるように設定する。The bulging portion 0I can be formed by grinding with a shaping grindstone or by turning, and its dimensions are set so as to obtain an extremely slight tightening of about 1 to 2 μm.
次いでその作動を説明するに、コンプレッサホイール(
1)とタービンシャフト(5)との嵌合に際しては、該
シャツ) (5) t−112ホイール(1)の軸孔(
6)内に圧入するもので、これによれば膨出部四におい
て両者(1)(5)は締シ嵌めされるが、本発明の如く
該膨出部αりを円弧状に形成するときは、両者(1)
(5)の抜差しが容易となル、且該膨出部QQIに他方
の部材が必ずその全周に亘って当接して同心度も得られ
易くなる。Next, to explain its operation, the compressor wheel (
1) and the turbine shaft (5), the shaft hole (1) of the T-112 wheel (1)
According to this, both (1) and (5) are tightly fitted in the bulge 4, but when the bulge α is formed into an arc shape as in the present invention. are both (1)
(5) can be easily inserted and removed, and the other member always comes into contact with the bulged portion QQI over its entire circumference, making it easier to obtain concentricity.
この様に本発明によるときは、コンプレッサホイールに
形成する軸孔の内周面とこれに嵌合するタービンシャフ
トの外周間との何れか一方に締めじろを得るための膨出
部を形成し、コンプレッサホイールとタービンシャフト
とを締夛嵌めするもので、両者全すきま嵌めする従来例
の如く該ホイールの偏心を生ずることが無く、且つ該膨
出部は円弧状に形成されるため、両者の抜差しは締シ嵌
めに係らず比較的容易に行い得られて、仮組付けしての
バランス取ル後、両者を分解して木組付けする作業に支
障を来たすことが無く、而もこの円弧状の膨出部には他
方の部材が必ずその全周に亘シ尚接して同心度も確保さ
れ、超精密なノ々ランスを得ることが可能となり、更に
テーパ軸とチーA穴とで嵌合する式のものと異シコンゾ
レツサホイールのタービンシャフトへの嵌合深さが規制
されず、これを位置決め部材による所定の軸方向位置に
確実に取付けられる効果を有する。As described above, according to the present invention, a bulge is formed between the inner peripheral surface of the shaft hole formed in the compressor wheel and the outer periphery of the turbine shaft that fits into the shaft hole for obtaining a tightening margin, The compressor wheel and turbine shaft are tightly fitted together, and there is no eccentricity of the wheel unlike in the conventional case where both are fitted with all the clearance, and since the bulge is formed in an arc shape, it is easy to insert and remove the two. It is relatively easy to do regardless of the tightening and fitting, and after temporarily assembling and balancing, it does not interfere with the work of disassembling the two and assembling them with wood. The other member is always in contact with the bulge over its entire circumference, ensuring concentricity, making it possible to obtain an ultra-precise nose lance, and further fitting with the tapered shaft and the chi A hole. This method has the effect that the fitting depth of the compressor wheel to the turbine shaft is not restricted, and it can be reliably attached to a predetermined axial position by the positioning member.
第1図は本発明装置を適用するター2チヤージヤの截断
側間図、第2図は本発明装置の1例の要部の分解截断側
面図、第3図はその変形例の要部の分解截断側面図であ
る。
(1)・・・、コンプレッサホイール
(5)・・・タービンシャフト (6)・・・軸孔−
・・・膨出部
特許出願人 本田技研工業株式会社
代 理 人 北 村 欣 :、l:
1(IJ :外2名Fig. 1 is a cut-away side view of a two-wheel charger to which the device of the present invention is applied, Fig. 2 is an exploded cut-away side view of the main parts of an example of the device of the present invention, and Fig. 3 is an exploded view of the main parts of a modification thereof. FIG. (1)..., Compressor wheel (5)...Turbine shaft (6)...Shaft hole-
...Bulging portion patent applicant: Honda Motor Co., Ltd. Representative: Kin Kitamura:, l:
1 (IJ: 2 other people)
Claims (1)
ンシャフトを嵌合させるものにおいて、該軸孔の内周面
と該タービンシャフトの外周面との何れか一方に締めじ
ろを得るための円弧状膨出部を形成して成るコンゾレッ
サホイールの吠合装置。- In a device in which a shaft hole is formed in the wheel and a turbine shaft is fitted into the shaft hole, a tightening margin is provided on either the inner circumferential surface of the shaft hole or the outer circumferential surface of the turbine shaft. A consolestor wheel jointing device formed with an arcuate bulge.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP57058181A JPS58176499A (en) | 1982-04-09 | 1982-04-09 | Fitting device for compressor wheel |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP57058181A JPS58176499A (en) | 1982-04-09 | 1982-04-09 | Fitting device for compressor wheel |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS58176499A true JPS58176499A (en) | 1983-10-15 |
JPH0211760B2 JPH0211760B2 (en) | 1990-03-15 |
Family
ID=13076831
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP57058181A Granted JPS58176499A (en) | 1982-04-09 | 1982-04-09 | Fitting device for compressor wheel |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS58176499A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2015087414A1 (en) * | 2013-12-11 | 2015-06-18 | 三菱重工業株式会社 | Rotating body and method for manufacturing rotating body |
EP3626870A1 (en) * | 2018-09-20 | 2020-03-25 | Saurer Spinning Solutions GmbH & Co. KG | Spinning rotor and holder for rotating a rotor socket of a spinning rotor, method for producing a press-fit connection between a rotor socket and a holder |
CN112360567A (en) * | 2020-10-26 | 2021-02-12 | 北京动力机械研究所 | High-speed radial-flow turbine and compressor composite impeller |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS4871270U (en) * | 1971-12-14 | 1973-09-07 | ||
JPS5666492A (en) * | 1979-11-06 | 1981-06-04 | Toyota Motor Corp | Fitting structure of impeller for small turbo machine |
-
1982
- 1982-04-09 JP JP57058181A patent/JPS58176499A/en active Granted
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS4871270U (en) * | 1971-12-14 | 1973-09-07 | ||
JPS5666492A (en) * | 1979-11-06 | 1981-06-04 | Toyota Motor Corp | Fitting structure of impeller for small turbo machine |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2015087414A1 (en) * | 2013-12-11 | 2015-06-18 | 三菱重工業株式会社 | Rotating body and method for manufacturing rotating body |
EP3081746A4 (en) * | 2013-12-11 | 2016-12-21 | Mitsubishi Heavy Ind Ltd | Rotating body and method for manufacturing rotating body |
JPWO2015087414A1 (en) * | 2013-12-11 | 2017-03-16 | 三菱重工業株式会社 | Rotating body and method for manufacturing the rotating body |
US10578116B2 (en) | 2013-12-11 | 2020-03-03 | Mitsubishi Heavy Industries, Ltd. | Rotational body and method for manufacturing the same |
EP3626870A1 (en) * | 2018-09-20 | 2020-03-25 | Saurer Spinning Solutions GmbH & Co. KG | Spinning rotor and holder for rotating a rotor socket of a spinning rotor, method for producing a press-fit connection between a rotor socket and a holder |
CN110923862A (en) * | 2018-09-20 | 2020-03-27 | 卓郎纺织解决方案两合股份有限公司 | Holder, spinning rotor and method for producing a crimp between a cup body and a holder |
CN112360567A (en) * | 2020-10-26 | 2021-02-12 | 北京动力机械研究所 | High-speed radial-flow turbine and compressor composite impeller |
Also Published As
Publication number | Publication date |
---|---|
JPH0211760B2 (en) | 1990-03-15 |
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