JPH08284884A - Fluid machinery - Google Patents

Fluid machinery

Info

Publication number
JPH08284884A
JPH08284884A JP11504795A JP11504795A JPH08284884A JP H08284884 A JPH08284884 A JP H08284884A JP 11504795 A JP11504795 A JP 11504795A JP 11504795 A JP11504795 A JP 11504795A JP H08284884 A JPH08284884 A JP H08284884A
Authority
JP
Japan
Prior art keywords
moving blade
tip
chip
height
backside
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.)
Withdrawn
Application number
JP11504795A
Other languages
Japanese (ja)
Inventor
Toshikazu Owaki
敏和 大脇
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.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries 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 Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP11504795A priority Critical patent/JPH08284884A/en
Publication of JPH08284884A publication Critical patent/JPH08284884A/en
Withdrawn legal-status Critical Current

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  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

PURPOSE: To improve performance in fluid machinery by chipping the backside of a moving blade by fixed height from the tip end, and forming a thin wall part at the web side. CONSTITUTION: A backside 1b of a moving blade 1 is chipped as far as constant height from the chip end 4, and ship thinning work to chip a cut part 2 is carried out, whereby a thin wall part 3 consisting in height (a) and thickness (b) along the profile is being formed. Accordingly, since a camber angle at a tip part of the moving blade 1 is not increased at all, any pressure rise based on this chip thinning work is thus restrained. In consequence, since the occurrence of any pressure grade in the height direction of the moving blade 1 is checkable, a mixing loss in a secondary flow on the basis of this pressure grade and any increase of fluid quantity to be leaked to the backside 1b from the web side 1a by way of a chip clearance are all preventable. With this constitution, fluid machinery (for example, a fan, a compressor and the like) is well improved in terms of performance.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【産業上の利用分野】本発明は軸流又は斜流型のフア
ン、ブロア、圧縮機、ポンプ等の流体機械に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an axial or mixed flow type fan, blower, compressor, pump or other fluid machine.

【0002】[0002]

【従来の技術】図2には従来の軸流送風機のチップシン
ニング加工を施した動翼の1例が示されている。翼形の
輪郭を有する動翼1の腹側1aをそのチップ端4から一定
高さ削り込んでカット部2を削除することによって背側
1bに背側曲線に沿って一定厚さの薄肉部3が形成されて
いる。5はケーシング、cはチップ端4とケーシング5
の内面との間のチップクリアランスを示す。
2. Description of the Related Art FIG. 2 shows an example of a rotor blade of a conventional axial blower, which has been subjected to tip thinning processing. The ventral side 1a of the rotor blade 1 having the contour of the airfoil is cut from the tip end 4 of the tip end 4 by a certain height and the cut portion 2 is removed so that the back side is removed.
A thin portion 3 having a constant thickness is formed on 1b along the back curve. 5 is a casing, c is a tip end 4 and a casing 5
2 shows the tip clearance with the inner surface of the.

【0003】上記チップシンニング加工はチップラブに
よるトラブル防止及びチップクリアランスcを狭くする
ことによって動翼1の腹側1aから背側1bへ漏れる流体を
少なくして送風機の効率を向上するために施工される。
The tip thinning process is carried out to prevent troubles due to the tip rub and to reduce the tip clearance c to reduce the fluid leaking from the ventral side 1a to the back side 1b of the moving blade 1 to improve the efficiency of the blower. It

【0004】[0004]

【発明が解決しようとする課題】チップシンニング加工
を施した場合には、図3に示すように、動翼1の先端部
の反り角θO 、即ち、翼のキャンバー線6と翼弦7、即
ち、翼前縁1cと翼後縁1dを結ぶ直線とのなす角がチップ
シンニング加工を施さない場合の反り角θより大きくな
る。
When subjected to INVENTION Problems to be Solved] chip thinning processing, as shown in FIG. 3, the warp angle theta O of the tip portion of the blade 1, i.e., blade camber line 6 and chord 7, That is, the angle formed by the straight line connecting the blade leading edge 1c and the blade trailing edge 1d is larger than the warp angle θ when the chip thinning process is not performed.

【0005】この結果、チップシンニング加工を施した
部分は施さない部分よりかなり大きな圧力上昇を発生さ
せて翼高さ方向に大きな圧力勾配を惹起する。これに伴
って、二次流れによる混合損失が増大するとともにチッ
プクリアランスcを通って腹側1aから背側1bへ漏れる流
体の量が増大するので、送風機の効率が低下するという
問題がっあった。
As a result, the portion subjected to the tip thinning process causes a considerably larger pressure rise than the portion not subjected to the tip thinning process, and causes a large pressure gradient in the blade height direction. Along with this, the mixing loss due to the secondary flow increases and the amount of fluid leaking from the ventral side 1a to the back side 1b through the tip clearance c increases, so that there is a problem that the efficiency of the blower decreases. .

【0006】[0006]

【課題を解決するための手段】本発明は上記課題を解決
するために発明されたものであって、この要旨とすると
ころは、翼形の輪郭を有する動翼を具え、この動翼のチ
ップ端とケーシングの内面との間にチップクリアランス
を存置せしめてなる流体機械において、上記動翼の背側
をそのチップ端から一定高さ削除することによって腹側
に薄肉部を形成したことを特徴とする流体機械にある。
SUMMARY OF THE INVENTION The present invention has been invented to solve the above-mentioned problems, and the gist of the present invention is to provide a blade having a wing-shaped contour, and a tip of the blade. In a fluid machine in which a tip clearance is kept between the end and the inner surface of the casing, a thin portion is formed on the ventral side by removing the back side of the moving blade from the tip end by a certain height. It is in fluid machinery.

【0007】[0007]

【作用】本発明においては、上記構成を具えているた
め、動翼先端部の反り角が増大しないので、チップシン
ニング加工に基づく圧力上昇が抑制される。
In the present invention, because of the above-mentioned structure, the warp angle of the tip of the moving blade does not increase, so that the pressure increase due to the tip thinning process is suppressed.

【0008】[0008]

【実施例】本発明の1実施例が図1に示されている。動
翼1の背側1bをそのチップ端4から一定高さa削り込み
カット部分2を削除するチップシンニング加工を施すこ
とによって腹側1aにその輪郭に沿う高さa、厚さbの薄
肉部3が形成されている。
DESCRIPTION OF THE PREFERRED EMBODIMENT One embodiment of the present invention is shown in FIG. By thinning the back side 1b of the rotor blade 1 from the tip end 4 of the tip end 4 and removing the cut portion 2, a thin portion having a height a and thickness b along the contour of the ventral side 1a 3 is formed.

【0009】この動翼1の先端部の反り角はチップシン
ニング加工を施さない場合と同じとなり、従って、図2
に示す従来のもののように動翼先端部における圧力上昇
を抑制し、この圧力上昇に基づく動翼高さ方向の圧力勾
配の発生を阻止しうる。
The warp angle of the tip portion of the moving blade 1 is the same as that when the tip thinning process is not applied, and therefore, as shown in FIG.
It is possible to suppress the pressure rise at the tip of the moving blade as in the case of the conventional one shown in FIG. 1 and prevent the generation of the pressure gradient in the height direction of the moving blade due to this pressure increase.

【0010】以上本発明を軸流送風機に適用した場合に
ついて説明したが、本発明は圧縮機、ポンプ等に適用す
ることができ、また、軸流型に限らず斜流型の流体機械
に適用しうるのは勿論である。
The case where the present invention is applied to an axial blower has been described above. However, the present invention can be applied to a compressor, a pump, etc., and is not limited to an axial flow type fluid machine. Of course it is possible.

【0011】[0011]

【発明の効果】本発明においては、動翼の背側をそのチ
ップ端から一定高さ削除することによって薄肉部を腹側
に形成したため、動翼先端部の反り角が増大しないの
で、チップシンニング加工に基づく圧力上昇を抑制しう
る。この結果、動翼の高さ方向の圧力勾配の発生を阻止
しうるので、この圧力勾配に基づく二次流れの混合損失
及びチップクリアランスを通って腹側から背側に漏れる
流体量の増大を防止しうる。
According to the present invention, since the thin portion is formed on the ventral side by removing the back side of the moving blade from the tip end by a certain height, the warp angle of the tip of the moving blade does not increase. The pressure increase due to processing can be suppressed. As a result, it is possible to prevent the generation of a pressure gradient in the height direction of the moving blade, and thus prevent an increase in the amount of fluid leaking from the ventral side to the dorsal side through the mixing loss of the secondary flow and the tip clearance due to this pressure gradient. You can.

【0012】かくして、チップシンニング加工による利
点、即ち、チップラブによるトラブル防止及びチップク
リアランスを通って動翼の腹側から背側に漏れる流体量
を少なくするという利点を損なうことなく従来のチップ
シンニング加工の不具合を解消して流体機械の性能を向
上できる。
Thus, the conventional tip thinning processing is carried out without impairing the advantages of the tip thinning processing, that is, the advantages of preventing troubles due to the tip rub and reducing the amount of fluid leaking from the ventral side of the moving blade to the back side through the tip clearance. The problem of can be solved and the performance of the fluid machine can be improved.

【図面の簡単な説明】[Brief description of drawings]

【図1】本発明の実施例に係わる軸流送風機の動翼の1
例を示し、(A) は動翼の先端部の斜視図、(B) は (A)の
B−B線に沿う断面図である。
FIG. 1 is one of rotor blades of an axial flow fan according to an embodiment of the present invention.
An example is shown, (A) is a perspective view of the tip portion of the moving blade, and (B) is a sectional view taken along the line BB of (A).

【図2】従来の軸流送風機の動翼を示し、(A) は動翼の
先端部の斜視図、(B) は (A)のB−B線に沿う断面図で
ある。
FIG. 2 shows a moving blade of a conventional axial-flow blower, (A) is a perspective view of a tip portion of the moving blade, and (B) is a cross-sectional view taken along line BB of (A).

【図3】上記従来の動翼先端部の反り角を示す説明図で
ある。
FIG. 3 is an explanatory diagram showing a warp angle of the conventional blade tip portion.

【符号の説明】[Explanation of symbols]

1 動翼 1a 腹側 1b 背側 2 カット部 3 薄肉部 1 Blade 1a Ventral side 1b Dorsal side 2 Cut section 3 Thin section

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】 翼形の輪郭を有する動翼を具え、この動
翼のチップ端とケーシングの内面との間にチップクリア
ランスを存置せしめてなる流体機械において、上記動翼
の背側をそのチップ端から一定高さ削除することによっ
て腹側に薄肉部を形成したことを特徴とする流体機械。
1. A fluid machine comprising a moving blade having an airfoil profile, wherein a tip clearance is left between the tip end of the moving blade and the inner surface of the casing. A fluid machine characterized in that a thin portion is formed on the ventral side by removing a certain height from the end.
JP11504795A 1995-04-17 1995-04-17 Fluid machinery Withdrawn JPH08284884A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP11504795A JPH08284884A (en) 1995-04-17 1995-04-17 Fluid machinery

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP11504795A JPH08284884A (en) 1995-04-17 1995-04-17 Fluid machinery

Publications (1)

Publication Number Publication Date
JPH08284884A true JPH08284884A (en) 1996-10-29

Family

ID=14652875

Family Applications (1)

Application Number Title Priority Date Filing Date
JP11504795A Withdrawn JPH08284884A (en) 1995-04-17 1995-04-17 Fluid machinery

Country Status (1)

Country Link
JP (1) JPH08284884A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6132171A (en) * 1997-06-10 2000-10-17 Matsushita Electric Industrial Co., Ltd. Blower and method for molding housing thereof
JP2002520993A (en) * 1998-07-20 2002-07-09 エヌエムビー(ユーエスエイ)・インコーポレイテッド Axial fan
CN1323631C (en) * 2004-02-03 2007-07-04 Lg电子株式会社 Air-blowing apparatus of cleaner
JP2008128198A (en) * 2006-11-24 2008-06-05 Ihi Corp Rotor blade of compressor
WO2014099520A1 (en) * 2012-12-19 2014-06-26 Solar Turbines Incorporated Compressor blade for gas turbine engine
US9399918B2 (en) 2012-08-09 2016-07-26 Mtu Aero Engines Gmbh Blade for a continuous-flow machine and a continuous-flow machine

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6796768B2 (en) 1997-06-10 2004-09-28 Matsushita Electric Industrial Co., Ltd. Blower and method for molding housing thereof
US6132171A (en) * 1997-06-10 2000-10-17 Matsushita Electric Industrial Co., Ltd. Blower and method for molding housing thereof
JP4796691B2 (en) * 1998-07-20 2011-10-19 ミネベア株式会社 Axial fan
JP2002520993A (en) * 1998-07-20 2002-07-09 エヌエムビー(ユーエスエイ)・インコーポレイテッド Axial fan
CN1323631C (en) * 2004-02-03 2007-07-04 Lg电子株式会社 Air-blowing apparatus of cleaner
US8366400B2 (en) 2006-11-24 2013-02-05 Ihi Corporation Compressor rotor
JP2008128198A (en) * 2006-11-24 2008-06-05 Ihi Corp Rotor blade of compressor
US9399918B2 (en) 2012-08-09 2016-07-26 Mtu Aero Engines Gmbh Blade for a continuous-flow machine and a continuous-flow machine
WO2014099520A1 (en) * 2012-12-19 2014-06-26 Solar Turbines Incorporated Compressor blade for gas turbine engine
GB2523961A (en) * 2012-12-19 2015-09-09 Solar Turbines Inc Compressor blade for gas turbine engine
CN104956032A (en) * 2012-12-19 2015-09-30 索拉透平公司 Compressor blade for gas turbine engine
US9506347B2 (en) 2012-12-19 2016-11-29 Solar Turbines Incorporated Compressor blade for gas turbine engine
GB2523961B (en) * 2012-12-19 2020-02-19 Solar Turbines Inc Compressor blade for gas turbine engine

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Legal Events

Date Code Title Description
A300 Withdrawal of application because of no request for examination

Free format text: JAPANESE INTERMEDIATE CODE: A300

Effective date: 20020702