JPS6313361Y2 - - Google Patents

Info

Publication number
JPS6313361Y2
JPS6313361Y2 JP16275982U JP16275982U JPS6313361Y2 JP S6313361 Y2 JPS6313361 Y2 JP S6313361Y2 JP 16275982 U JP16275982 U JP 16275982U JP 16275982 U JP16275982 U JP 16275982U JP S6313361 Y2 JPS6313361 Y2 JP S6313361Y2
Authority
JP
Japan
Prior art keywords
shaft
hollow
metal
impeller
turbocharger
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
JP16275982U
Other languages
Japanese (ja)
Other versions
JPS5967539U (en
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 filed Critical
Priority to JP16275982U priority Critical patent/JPS5967539U/en
Publication of JPS5967539U publication Critical patent/JPS5967539U/en
Application granted granted Critical
Publication of JPS6313361Y2 publication Critical patent/JPS6313361Y2/ja
Granted legal-status Critical Current

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  • Supercharger (AREA)

Description

【考案の詳細な説明】 本考案はターボ過給機のシヤフト構造に関す
る。第1図は一般的なターボ過給機の断面図を示
すもので、機関からの排気が供給されるタービン
ハウジング1内に配設したタービンインペラ2
と、機関の吸気路に接続されたコンプレツサハウ
ジング3内に配設したコンプレツサインペラ4と
をシヤフト5を介して一体的に結合し、ラジアル
荷重を受けるメタル61,62が前記シヤフトに
装着されている。前記ラジアル荷重を受けるメタ
ル61,62の周囲は常に潤滑油で覆われ、シヤ
フト5は潤滑油中で浮上滑動しながら回転してい
る。一方前記タービンインペラ2は排気ガスの圧
力により回転力を与えられているため、高熱にさ
らされている。この高熱は前記シヤフト5を介
し、コンプレツサインペラ4側へと伝わる。その
際、前記メタル61,62の周囲に流れている潤
滑油が高温となり、潤滑油を劣化を促進し、最悪
の場合メタル焼き付きといつた不具合が生じる場
合がある。
[Detailed Description of the Invention] The present invention relates to a shaft structure of a turbocharger. Figure 1 shows a cross-sectional view of a typical turbocharger, in which a turbine impeller 2 is disposed within a turbine housing 1 to which exhaust gas from the engine is supplied.
and a compressor impeller 4 disposed in a compressor housing 3 connected to the intake passage of the engine are integrally coupled via a shaft 5, and metals 61 and 62 that receive radial loads are attached to the shaft. ing. The surroundings of the metals 61 and 62 that receive the radial load are always covered with lubricating oil, and the shaft 5 rotates while floating and sliding in the lubricating oil. On the other hand, since the turbine impeller 2 is given rotational force by the pressure of exhaust gas, it is exposed to high heat. This high heat is transmitted to the compressor impeller 4 side via the shaft 5. At this time, the lubricating oil flowing around the metals 61 and 62 becomes high in temperature, promoting deterioration of the lubricating oil, and in the worst case, problems such as metal seizure may occur.

本考案は上記のことに鑑み、ターボ過給機の構
造を大幅に変更すること無しに、潤滑油の劣化及
びメタル焼き付きを防止することを目的としたも
のである。加えて本考案の他の目的は、ターボ過
給機回転部分の慣性重量を低減し、効率の良い過
給を行なうことのできるターボ過給機を提供する
ことにある。
In view of the above, the present invention aims to prevent deterioration of lubricating oil and metal seizure without significantly changing the structure of a turbocharger. In addition, another object of the present invention is to provide a turbocharger that can reduce the inertia weight of the rotating parts of the turbocharger and perform efficient supercharging.

以下にこの考案を図面の実施例により説明す
る。第2図は本考案の第一実施例を示す要部断面
図である。図において、5′は中空管状に形成さ
れた中空部材で、前記メタルが装着される位置に
は円柱状の補強部材9が圧入等により嵌入されて
いる。
This invention will be explained below with reference to embodiments of the drawings. FIG. 2 is a sectional view of a main part showing a first embodiment of the present invention. In the figure, 5' is a hollow member formed in the shape of a hollow tube, and a cylindrical reinforcing member 9 is fitted by press-fitting or the like at the position where the metal is mounted.

該中空部材5′の一端部には前記コンプレツサ
インペラを取り付けるためのインペラ固定軸8の
連結部81が嵌入され、ロウ付けあるいは摩擦圧
着等により固着されており、該連結部81は前記
メタル61の装着位置に達する寸法に構成され補
強部材の機能も兼ね備えている。
A connecting portion 81 of the impeller fixing shaft 8 for attaching the compressed impeller is fitted into one end of the hollow member 5' and is fixed by brazing or friction bonding, and the connecting portion 81 is attached to the metal 61. It is constructed in such a size that it reaches the mounting position, and also has the function of a reinforcing member.

また中空部材5′の他端部には、タービンイン
ペラ2′に形成された連結部21が嵌入され、ロ
ウ付けあるいは摩擦圧着等により固着されてい
る。
Further, a connecting portion 21 formed on the turbine impeller 2' is fitted into the other end of the hollow member 5' and fixed by brazing, friction bonding, or the like.

なお、上記のように構成されたシヤフト5の中
空部分7に組み立ての際グラスウール等の断熱材
を充填してもよい。
Note that the hollow portion 7 of the shaft 5 configured as described above may be filled with a heat insulating material such as glass wool during assembly.

以上のように本実施例によれば、シヤフト5を
中空部材5′によつて構成したので、該中空部材
5′によつて形成される中空部7は熱伝達が低く、
従つて排気ガスからタービンインペラ21が受け
た熱のコンプレツサインペラ4側への熱伝達が大
幅に減少する結果となる。これによつてメタル6
1,62に流れる潤滑油の劣化及びメタルの焼き
付きを防止することができる。
As described above, according to this embodiment, since the shaft 5 is constituted by the hollow member 5', the hollow portion 7 formed by the hollow member 5' has low heat transfer.
Therefore, the heat transfer from the exhaust gas to the compressor impeller 4 side, which is received by the turbine impeller 21, is significantly reduced. Metal 6
It is possible to prevent the deterioration of the lubricating oil flowing through the pipes 1 and 62 and the seizure of the metal.

またシヤフト5を中空部材5′で形成するとと
もに、ラジアル荷重を受ける部分には、補強部材
を嵌入したことにより、シヤフト5の強度を従来
のものと同程度に保つたまま、シヤフト5の重量
を軽減することができ、これによりターボ過給機
回転部分の慣性重量が減少し、効率の良い過給を
行なうことができる。
In addition, by forming the shaft 5 with a hollow member 5' and inserting reinforcing members into the portions that receive radial loads, the weight of the shaft 5 can be reduced while maintaining the strength of the shaft 5 at the same level as conventional ones. As a result, the inertial weight of the rotating parts of the turbocharger is reduced, and efficient supercharging can be performed.

第3図は本考案の第2実施例を示すもので、中
空部材を2つの部材51″,52″に分割し、メタ
ル62が装着される部分で、両中空部材51″と
52″を補強部材9′によつて結合したものであ
る。該補強部材9′は中央部が中空部材51″及び
52″の外径と同一寸法の外径を有し、その両端
が中空材51″及び52″の内径と略々同一寸法の
外径に形成された小径部91″,92″を備えてお
り、該小径部91″及び92″を中空部材51″及
び52″に各々嵌入し、ロウ付けあるいは摩擦圧
着等により固着して両中空部材51″と52″とを
連結する。
Figure 3 shows a second embodiment of the present invention, in which the hollow member is divided into two members 51'' and 52'', and both hollow members 51'' and 52'' are reinforced at the part where the metal 62 is attached. They are connected by a member 9'. The reinforcing member 9' has an outer diameter at the center that is the same as the outer diameter of the hollow members 51'' and 52'', and an outer diameter at both ends that is approximately the same as the inner diameter of the hollow members 51'' and 52''. The small diameter portions 91'' and 92'' are fitted into the hollow members 51'' and 52'', respectively, and fixed by brazing or friction bonding, etc., so that both the hollow members 51 ” and 52” are connected.

また中空部材51″に連結されるコンプレツサ
インペラ固定軸8′の連結部81′にもその中空部
材51″の内径と略々同一寸法の外径に形成され
た小径部82′が設けられ、該小径部82′を中空
部材51″に嵌入して、ロウ付けあるいは摩擦圧
着等により固着し、この場合前記連結部81′の
外周にメタル61が嵌着される。
Further, a connecting portion 81' of the fixed impeller fixed shaft 8' connected to the hollow member 51'' is also provided with a small diameter portion 82' having an outer diameter that is approximately the same as the inner diameter of the hollow member 51''. The small diameter portion 82' is fitted into the hollow member 51'' and fixed by brazing or friction bonding, and in this case, the metal 61 is fitted around the outer periphery of the connecting portion 81'.

このように構成したことにより、シヤフト5に
は中空部7が形成され第2図で示した本考案の第
1実施例と同様の効果が得られるとともに、中空
部材を2つの部材51″と52″に分割したので、
補強部材7の嵌入作業の時間が短縮され、組付性
が向上するという作用効果が得られる。
With this structure, the shaft 5 is formed with the hollow part 7, and the same effect as the first embodiment of the present invention shown in FIG. ″, so
The effect of shortening the time required for inserting the reinforcing member 7 and improving the ease of assembly can be obtained.

以上のように本考案によれば、ターボ過給機の
シヤフトを中空部材で形成するとともに、メタル
装着部に補強部材を嵌入したので、ターボ過給機
の構造を大幅に変更することなく、またシヤフト
の強度を低下することなく、潤滑油の劣化あるい
はメタル焼き付きといつた不具合を防止でき、更
にターボ過給機の回転部分の慣性重量を低減し、
効率の良い過給を行なうことができるものであ
る。
As described above, according to the present invention, the shaft of the turbocharger is formed of a hollow member, and a reinforcing member is fitted into the metal attachment part, so that it is possible to avoid major changes to the structure of the turbocharger. This prevents problems such as lubricating oil deterioration and metal seizure without reducing the strength of the shaft, and also reduces the inertia of the rotating parts of the turbocharger.
This allows efficient supercharging.

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

第1図は従来のターボ過給機の断面図、第2図
は本考案の第1実施例を示す要部断面図、第3図
は本考案の第2実施例を示す要部断面図である。 2,2′,2″……タービンインペラ、4……コ
ンプレツサインペラ、5……シヤフト、7……中
空部、9……補強部材。
Fig. 1 is a sectional view of a conventional turbocharger, Fig. 2 is a sectional view of main parts showing the first embodiment of the present invention, and Fig. 3 is a sectional view of main parts showing the second embodiment of the invention. be. 2, 2', 2''...Turbine impeller, 4...Complex impeller, 5...Shaft, 7...Hollow portion, 9...Reinforcement member.

Claims (1)

【実用新案登録請求の範囲】 (1) 機関からの排気が供給されるタービンハウジ
ング内に配設したタービンインペラと機関の吸
気路に接続されたコンプレツサインペラとをシ
ヤフトを介して一体的に結合し、前記シヤフト
にラジアル荷重を受けるメタルを装着したター
ボ過給機において、前記シヤフトを中空部材で
形成すると共に、前記メタルを装着する部分に
補強部材を嵌入したことを特徴とする、ターボ
過給機のシヤフト構造。 (2) 前記中空部材を複数個に分割し、中空部材同
士を補強部材を介して結合したことを特徴とす
る、実用新案登録請求の範囲第1項記載のシヤ
フト構造。
[Claims for Utility Model Registration] (1) A turbine impeller disposed in a turbine housing to which exhaust gas from an engine is supplied and a compressed impeller connected to an intake passage of the engine are integrally coupled via a shaft. In the turbo supercharger in which the shaft is equipped with a metal that receives a radial load, the shaft is formed of a hollow member, and a reinforcing member is inserted into the part where the metal is attached. Machine shaft structure. (2) The shaft structure according to claim 1 of the utility model registration, characterized in that the hollow member is divided into a plurality of parts, and the hollow members are connected to each other via a reinforcing member.
JP16275982U 1982-10-27 1982-10-27 Shaft structure of turbocharger Granted JPS5967539U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP16275982U JPS5967539U (en) 1982-10-27 1982-10-27 Shaft structure of turbocharger

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP16275982U JPS5967539U (en) 1982-10-27 1982-10-27 Shaft structure of turbocharger

Publications (2)

Publication Number Publication Date
JPS5967539U JPS5967539U (en) 1984-05-08
JPS6313361Y2 true JPS6313361Y2 (en) 1988-04-15

Family

ID=30357318

Family Applications (1)

Application Number Title Priority Date Filing Date
JP16275982U Granted JPS5967539U (en) 1982-10-27 1982-10-27 Shaft structure of turbocharger

Country Status (1)

Country Link
JP (1) JPS5967539U (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0627761Y2 (en) * 1985-09-26 1994-07-27 日本碍子株式会社 Coupling shaft structure of ceramic turbine rotor and metal shaft
JPS63248926A (en) * 1987-04-04 1988-10-17 Isuzu Motors Ltd Shaft structure for turbocharger

Also Published As

Publication number Publication date
JPS5967539U (en) 1984-05-08

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