JP2760095B2 - Centrifugal compressor impeller - Google Patents
Centrifugal compressor impellerInfo
- Publication number
- JP2760095B2 JP2760095B2 JP28112689A JP28112689A JP2760095B2 JP 2760095 B2 JP2760095 B2 JP 2760095B2 JP 28112689 A JP28112689 A JP 28112689A JP 28112689 A JP28112689 A JP 28112689A JP 2760095 B2 JP2760095 B2 JP 2760095B2
- Authority
- JP
- Japan
- Prior art keywords
- rear end
- impeller
- shaft
- main body
- centrifugal compressor
- 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 - Lifetime
Links
Landscapes
- Structures Of Non-Positive Displacement Pumps (AREA)
Description
【発明の詳細な説明】 [産業上の利用分野] 本発明は軽量で強度の高い遠心型圧縮機の翼車に関す
るものである。Description: TECHNICAL FIELD The present invention relates to a light weight and high strength centrifugal compressor wheel.
[従来の技術] 特開昭56−13499号公報に開示されるように、羽根が
側板により覆われている形式の遠心型圧縮機の翼車で
は、側板の吸込口側端部が羽根から離れているので、こ
の部分の遠心応力負担が高く、疲労破壊を起しやすい。
そこで、側板の吸込口側端部外周に補強環体を嵌着して
いる。しかし、側板をもたない遠心型圧縮機の翼車で
は、上述のような問題はない。[Prior Art] As disclosed in JP-A-56-13499, in a centrifugal compressor impeller of a type in which the blades are covered by side plates, the suction port side end of the side plates is separated from the blades. Therefore, the centrifugal stress burden on this portion is high, and fatigue fracture is likely to occur.
Therefore, a reinforcing ring is fitted around the outer periphery of the suction port side end of the side plate. However, in the centrifugal compressor wheel having no side plate, the above-described problem does not occur.
第3,4図に示す従来の遠心型圧縮機の翼車では、羽根
5により軸前端の軸方向吸込口18から軸後端の径外方吐
出口19へ円弧状に湾曲する溝通路が区画される本体6を
軸2に嵌合し、本体6の後端壁7と軸2の段部9との間
に、軸受10の潤滑油が翼車側へ吸い込まれるのを防止す
るシール部材8を外嵌し、軸2の前端部にナツト3を螺
合して本体6が軸2に結合される。軸2は後端側で軸受
10により図示してないハウジングに支持される。In the impeller of the conventional centrifugal compressor shown in FIGS. 3 and 4, the blade 5 defines a groove passage curved in an arc shape from the axial suction port 18 at the front end of the shaft to the radially outward discharge port 19 at the rear end of the shaft. The main body 6 to be fitted is fitted to the shaft 2 and a seal member 8 is provided between the rear end wall 7 of the main body 6 and the step 9 of the shaft 2 to prevent the lubricating oil of the bearing 10 from being sucked into the impeller. The main body 6 is connected to the shaft 2 by screwing the nut 3 to the front end of the shaft 2. Shaft 2 is a bearing at the rear end
10 supports the housing (not shown).
[発明が解決しようとする問題点] 上述のように、軸2が後端側だけでハウジングに支持
される形式の翼車(例えば排気ターボ過給機に組み込ま
れるもの)では、本体6の重心Gと軸受10との間隔Bが
長いほど、軸受10の負担が大きくなる。また、本体6の
後端壁7の軸心側肉部は翼車の重量に大きく影響する。[Problems to be Solved by the Invention] As described above, in an impeller of a type in which the shaft 2 is supported by the housing only on the rear end side (for example, incorporated in an exhaust turbocharger), the center of gravity of the main body 6 The longer the distance B between G and the bearing 10, the greater the load on the bearing 10. In addition, the axially-facing portion of the rear end wall 7 of the main body 6 greatly affects the weight of the impeller.
本発明の目的は上述の問題に鑑み、本体の後端部軸心
側の肉部を削除して軽量化しても、遠心応力や熱応力に
対する強度が損われない、遠心型圧縮機の翼車を提供す
ることにある。SUMMARY OF THE INVENTION In view of the above-described problems, an object of the present invention is to provide a centrifugal compressor impeller that does not lose its strength against centrifugal stress and thermal stress even when the weight is reduced by removing the rear end axial side of the main body. Is to provide.
[問題を解決するための手段] 上記目的を達成するために、本発明の構成は羽根によ
り軸前端の軸方向吸込口から軸後端の径外方吐出口へ円
弧状に湾曲する溝通路が区画される翼車の後端部軸心側
に円錐状空部を形成し、後端部外周面に翼車よりも熱膨
張率の小さく高強度の材料からなる環体を嵌着したもの
である。[Means for Solving the Problem] In order to achieve the above object, in the configuration of the present invention, a groove passage curved in an arc shape from an axial suction port at a front end of a shaft to a radially outward discharge port at a rear end of a shaft by a blade is provided. A conical cavity is formed on the axis of the rear end of the impeller to be sectioned, and a ring made of a high-strength material with a smaller coefficient of thermal expansion than the impeller is fitted on the outer peripheral surface of the rear end. is there.
[作用] 翼車の後端部軸心側の一部を削除すると、本体が大幅
に軽量化される半面、遠心応力や熱応力に対し翼車の後
端部が径外方へ脹らむような変形力を受けるが、翼車の
後端部外周面に嵌着した補強環体により、遠心応力や熱
応力による変形が抑えられる。[Action] If the rear end of the impeller is partially removed on the axial center side, the main body is significantly reduced in weight, but the rear end of the impeller expands radially outward due to centrifugal stress and thermal stress. Deformation force is received, but deformation due to centrifugal stress and thermal stress is suppressed by the reinforcing ring fitted to the outer peripheral surface of the rear end of the impeller.
[発明の実施例] 第1図は本発明による遠心型圧縮機の翼車の概略構成
を示す側面断面図である。本発明によれば、本体6の後
端部軸心側に円錐面14と端壁面15で区画される空部17が
形成され、これにより本体6が大幅に軽量化される。端
壁面15と軸2の段部9との間にシール部材8が介装さ
れ、軸2の前端側に螺合したナツト3により締結され
る。[Embodiment of the Invention] Fig. 1 is a side sectional view showing a schematic configuration of an impeller of a centrifugal compressor according to the present invention. According to the present invention, a hollow portion 17 defined by the conical surface 14 and the end wall surface 15 is formed on the axial center side of the rear end of the main body 6, whereby the weight of the main body 6 is significantly reduced. A seal member 8 is interposed between the end wall surface 15 and the step 9 of the shaft 2 and fastened by a nut 3 screwed to the front end of the shaft 2.
本体6の後端部の変形を抑えるために、後端部外周面
に、本体6よりも熱膨張率が小さく強靭な材料例えば炭
素繊維強度プラスチツク(CSRP)製の環体16が嵌着され
る。In order to suppress deformation of the rear end of the main body 6, an annular body 16 made of a material having a smaller coefficient of thermal expansion than the main body 6, for example, carbon fiber strength plastic (CSRP), is fitted to the outer peripheral surface of the rear end. .
第3図に示すように、本体6の後端部外周面に環状溝
13を形成し、環状溝13の内部にカーボン長繊維、ケブラ
と称するセラミツク系長繊維などを巻き付け、エポキシ
樹脂などを充填して固定してもよい。As shown in FIG. 3, an annular groove is formed on the outer peripheral surface of the rear end of the main body 6.
13 may be formed, and a carbon long fiber, a ceramic long fiber called Kevlar, or the like may be wound inside the annular groove 13 and filled with an epoxy resin or the like to be fixed.
次に、本発明による遠心型圧縮機の翼車の作用につい
て説明する。第2図に鎖線で示すように、空気の圧縮に
伴う温度上昇に伴い、翼車の本体6が加熱されると、熱
膨張と遠心応力を受けて変形する(図は膨張して表
す)。このような変形は、熱膨張率が本体6よりも小さ
く、強度が高い環体16により抑えられる。すなわち、本
体6を構成するアルミニウム合金、マグネシウム合金、
エンジニアリングプラスチツクなどに比べて、カーボン
長繊維やセラミツク系長繊維などは熱膨張率が小さく、
強度が高いので、本体6の熱応力や遠心応力による変形
を抑えることができる。Next, the operation of the impeller of the centrifugal compressor according to the present invention will be described. As shown by a chain line in FIG. 2, when the body 6 of the impeller is heated due to a rise in temperature accompanying the compression of air, the impeller is deformed by thermal expansion and centrifugal stress (the figure is expanded). Such deformation is suppressed by the annular body 16 having a smaller coefficient of thermal expansion than the main body 6 and a high strength. That is, aluminum alloy, magnesium alloy,
Compared to engineering plastics, carbon long fibers and ceramic long fibers have a low coefficient of thermal expansion,
Since the strength is high, deformation of the main body 6 due to thermal stress or centrifugal stress can be suppressed.
[発明の効果] 本発明は上述のように、羽根により軸前端の軸方向吸
込口から軸後端の径外方吐出口へ円弧状に湾曲する溝通
路が区画される翼車の後端部軸心側に円錐状空部を形成
し、後端部外周面に翼車よりも熱膨張率の小さく高強度
の材料からなる環体を嵌着したものであり、本体の後端
部軸心側に円錐状空部を設けたことにより、本体が大幅
に軽量化され、高速回転での軸受の負担が軽減される。[Effects of the Invention] As described above, the present invention provides a rear end portion of an impeller in which a blade path defines an arc-shaped curved groove passage from an axial suction port at a front end of a shaft to a radially outward discharge port at a rear end of a shaft. A conical cavity is formed on the axis side, and a ring made of a high-strength material having a smaller coefficient of thermal expansion than the impeller is fitted on the outer peripheral surface of the rear end. The provision of the conical hollow portion on the side significantly reduces the weight of the main body and reduces the load on the bearing at high speed rotation.
本体の後端部軸心側に円錐状空部を設けたことによ
り、本体と軸受との間隔が短縮され、この意味でも軸受
の負担が軽減される。By providing the conical hollow portion on the axial center side of the rear end of the main body, the distance between the main body and the bearing is reduced, and in this sense, the load on the bearing is also reduced.
本体が軽量化されるので、回転系の固有振動数(2次
の)が常用される回転域よりも高くなり、振動破壊に対
する安全性が向上される。Since the weight of the main body is reduced, the natural frequency (second order) of the rotating system is higher than a commonly used rotation range, and safety against vibration destruction is improved.
第1図は本発明に係る遠心型圧縮機の翼車の側面図、第
2図は同翼車の熱変形を表す側面断面図、第3図は環体
の変更実施例を示す側面断面図、第4図は従来の遠心型
圧縮機の翼車の側面断面図である。 2:軸、4:翼車、5:羽根、16:環体、17:空部、18:吸込
口、19:吐出口1 is a side view of a wheel of a centrifugal compressor according to the present invention, FIG. 2 is a side cross-sectional view showing thermal deformation of the wheel, and FIG. 3 is a side cross-sectional view showing a modified embodiment of a ring body. FIG. 4 is a side sectional view of a conventional impeller of a centrifugal compressor. 2: shaft, 4: impeller, 5: blade, 16: ring, 17: empty, 18: suction port, 19: discharge port
Claims (1)
端の径外方吐出口へ円弧状に湾曲する溝通路が区画され
る翼車の後端部軸心側に円錐状空部を形成し、後端部外
周面に翼車よりも熱膨張率の小さく高強度の材料からな
る環体を嵌着したことを特徴とする遠心型圧縮機の翼
車。1. A blade-shaped conical cavity at the rear end of the impeller, wherein a groove passage curved in an arc shape is defined from the axial suction port at the front end of the shaft to the radially outward discharge port at the rear end of the shaft. A centrifugal compressor impeller characterized in that an annular body made of a high-strength material having a smaller coefficient of thermal expansion than the impeller is fitted to the outer peripheral surface of the rear end portion.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP28112689A JP2760095B2 (en) | 1989-10-27 | 1989-10-27 | Centrifugal compressor impeller |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP28112689A JP2760095B2 (en) | 1989-10-27 | 1989-10-27 | Centrifugal compressor impeller |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH03141898A JPH03141898A (en) | 1991-06-17 |
| JP2760095B2 true JP2760095B2 (en) | 1998-05-28 |
Family
ID=17634727
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP28112689A Expired - Lifetime JP2760095B2 (en) | 1989-10-27 | 1989-10-27 | Centrifugal compressor impeller |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JP2760095B2 (en) |
Families Citing this family (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| IT1394295B1 (en) | 2009-05-08 | 2012-06-06 | Nuovo Pignone Spa | CENTRIFUGAL IMPELLER OF THE CLOSED TYPE FOR TURBOMACCHINE, COMPONENT FOR SUCH A IMPELLER, TURBOMACCHINA PROVIDED WITH THAT IMPELLER AND METHOD OF REALIZING SUCH A IMPELLER |
| IT1397058B1 (en) | 2009-11-23 | 2012-12-28 | Nuovo Pignone Spa | CENTRIFUGAL IMPELLER MOLD, MOLD INSERTS AND METHOD TO BUILD A CENTRIFUGAL IMPELLER |
| IT1397057B1 (en) | 2009-11-23 | 2012-12-28 | Nuovo Pignone Spa | CENTRIFUGAL AND TURBOMACHINE IMPELLER |
| ITCO20110064A1 (en) | 2011-12-14 | 2013-06-15 | Nuovo Pignone Spa | ROTARY MACHINE INCLUDING A ROTOR WITH A COMPOSITE IMPELLER AND A METAL SHAFT |
| ITCO20130067A1 (en) | 2013-12-17 | 2015-06-18 | Nuovo Pignone Srl | IMPELLER WITH PROTECTION ELEMENTS AND CENTRIFUGAL COMPRESSOR |
| CN109312661B (en) * | 2016-09-02 | 2020-12-25 | 株式会社Ihi | Impeller for supercharger |
| DE112018003072T5 (en) * | 2017-06-16 | 2020-02-27 | Ihi Corporation | Impeller made of FK for vehicle turbochargers |
| FR3081944B1 (en) * | 2018-05-31 | 2020-06-19 | Safran Electrical & Power | AIR COMPRESSOR THERMAL ARCHITECTURE |
| JP2022130751A (en) * | 2019-07-18 | 2022-09-07 | パナソニックIpマネジメント株式会社 | Impeller and centrifugal compressor using the same |
| US11408434B2 (en) | 2019-12-10 | 2022-08-09 | Ingersoll-Rand Industrial U.S., Inc. | Centrifugal compressor impeller with nonlinear backwall |
-
1989
- 1989-10-27 JP JP28112689A patent/JP2760095B2/en not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| JPH03141898A (en) | 1991-06-17 |
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