JP2015137592A5 - - Google Patents
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- Publication number
- JP2015137592A5 JP2015137592A5 JP2014009680A JP2014009680A JP2015137592A5 JP 2015137592 A5 JP2015137592 A5 JP 2015137592A5 JP 2014009680 A JP2014009680 A JP 2014009680A JP 2014009680 A JP2014009680 A JP 2014009680A JP 2015137592 A5 JP2015137592 A5 JP 2015137592A5
- Authority
- JP
- Japan
- Prior art keywords
- pressure surface
- hole
- impeller according
- surface side
- blade
- 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
- 239000012530 fluid Substances 0.000 claims description 2
- 238000007599 discharging Methods 0.000 claims 1
- 238000002347 injection Methods 0.000 claims 1
- 239000007924 injection Substances 0.000 claims 1
- 230000002093 peripheral Effects 0.000 claims 1
Description
上記課題を解決するため、本発明の第一の態様に係るインペラ、及び遠心圧縮機では、以下の手段を採用している。
本発明の一態様に係るインペラは、軸線回りに回転するディスクと、該ディスクの軸線方向一方側の面に、周方向に間隔をあけて複数設けられて軸線方向一方側から流入する流体を径方向外側に向かって排出する流路を画成するブレードと、を備え、前記ブレードは、径方向内側から外側に向かうに従って、軸線方向の寸法が減少するように形成され、前記ブレードに、回転方向前方側を向く圧力面と回転方向後方側を向く負圧面とを連通する孔部が形成され、前記孔部が前記ブレードを貫通する方向は、前記ディスクを基準とする前記ブレードの高さ方向における中間位置を前記軸線方向に結んだ線に沿うように設定されている。
In order to solve the above problems, the following means are employed in the impeller and the centrifugal compressor according to the first aspect of the present invention.
An impeller according to an aspect of the present invention has a disk that rotates around an axis, and a plurality of fluids that are provided on the surface on one side in the axial direction of the disk at intervals in the circumferential direction and flow from one side in the axial direction A blade that defines a flow path that discharges toward the outside in the direction, and the blade is formed such that its axial dimension decreases from the radially inner side toward the outer side, and the blade has a rotational direction. are holes for communicating the negative pressure surface facing the pressure surface and rotationally trailing side facing the front side is formed, and the direction of the hole passes through the blade, in the height direction of the blade relative to the said disc The intermediate position is set along a line connecting in the axial direction .
Claims (8)
該ディスクの軸線方向一方側の面に、周方向に間隔をあけて複数設けられて軸線方向一方側から流入する流体を径方向外側に向かって排出する流路を画成するブレードと、
を備え、
前記ブレードは、径方向内側から外側に向かうに従って、軸線方向の寸法が減少するように形成され、
前記ブレードに、回転方向前方側を向く圧力面と回転方向後方側を向く負圧面とを連通する孔部が形成され、
前記孔部が前記ブレードを貫通する方向は、前記ディスクを基準とする前記ブレードの高さ方向における中間位置を前記軸線方向に結んだ線に沿うように設定されているインペラ。 A disc that rotates about its axis;
A plurality of blades which are provided on the surface on one side in the axial direction of the disk at intervals in the circumferential direction and define a flow path for discharging fluid flowing in from the one side in the axial direction toward the outside in the radial direction;
With
The blade is formed such that its axial dimension decreases from the radially inner side to the outer side,
Said blade hole for communicating the suction side of the pressure surface facing the rotational direction of the front side and oriented in the direction of rotation rear side is formed,
The impeller that is set so that a direction in which the hole passes through the blade is along a line that connects an intermediate position in the height direction of the blade with respect to the disk in the axial direction .
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2014009680A JP6249219B2 (en) | 2014-01-22 | 2014-01-22 | Impeller and centrifugal compressor |
EP14879801.0A EP3098454A4 (en) | 2014-01-22 | 2014-07-23 | Impeller and centrifugal compressor |
US15/039,312 US20170167501A1 (en) | 2014-01-22 | 2014-07-23 | Impeller and centrifugal compressor |
PCT/JP2014/069451 WO2015111243A1 (en) | 2014-01-22 | 2014-07-23 | Impeller and centrifugal compressor |
CN201480062326.5A CN105723096A (en) | 2014-01-22 | 2014-07-23 | Impeller and centrifugal compressor |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2014009680A JP6249219B2 (en) | 2014-01-22 | 2014-01-22 | Impeller and centrifugal compressor |
Publications (3)
Publication Number | Publication Date |
---|---|
JP2015137592A JP2015137592A (en) | 2015-07-30 |
JP2015137592A5 true JP2015137592A5 (en) | 2017-02-16 |
JP6249219B2 JP6249219B2 (en) | 2017-12-20 |
Family
ID=53681066
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2014009680A Expired - Fee Related JP6249219B2 (en) | 2014-01-22 | 2014-01-22 | Impeller and centrifugal compressor |
Country Status (5)
Country | Link |
---|---|
US (1) | US20170167501A1 (en) |
EP (1) | EP3098454A4 (en) |
JP (1) | JP6249219B2 (en) |
CN (1) | CN105723096A (en) |
WO (1) | WO2015111243A1 (en) |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB256647A (en) * | 1925-08-08 | 1926-10-21 | Gen Electric | Improvements in or relating to centrifugal blowers and compressors |
US2161182A (en) * | 1937-01-22 | 1939-06-06 | Alfred N Massey | Supercharger for internal combustion engines |
DE860898C (en) * | 1944-02-29 | 1952-12-29 | Aeg | Impeller for centrifugal pumps |
CH398320A (en) * | 1961-06-27 | 1966-03-15 | Sulzer Ag | Centrifugal pump |
JPS53123506U (en) * | 1977-03-07 | 1978-10-02 | ||
DE4214753A1 (en) * | 1992-05-04 | 1993-11-11 | Asea Brown Boveri | Radial compressor impeller with axially spaced shroud disc - has series of holes across blade ends to give stable flow under part load conditions |
JP3948785B2 (en) * | 1996-05-17 | 2007-07-25 | カルソニックカンセイ株式会社 | Centrifugal multiblade fan |
DE69724868T2 (en) * | 1996-05-17 | 2004-05-06 | Calsonic Kansei Corp. | Multi-blade rotor for centrifugal fans |
US6860715B2 (en) * | 2003-04-24 | 2005-03-01 | Borgwarner Inc. | Centrifugal compressor wheel |
JP2006194238A (en) * | 2004-12-14 | 2006-07-27 | Toyota Industries Corp | Centrifugal compressor |
US7261513B2 (en) * | 2004-12-01 | 2007-08-28 | Kabushiki Kaisha Toyota Jidoshokki | Centrifugal compressor |
GB0910838D0 (en) | 2009-06-24 | 2009-08-05 | Rolls Royce Plc | A shroudless blade |
JP2012052439A (en) * | 2010-08-31 | 2012-03-15 | Mitsubishi Heavy Ind Ltd | Impeller |
CN202326441U (en) * | 2011-12-02 | 2012-07-11 | 杭州求是透平机制造有限公司 | Wedge-shaped blade for blade diffuser of centrifugal compressor |
-
2014
- 2014-01-22 JP JP2014009680A patent/JP6249219B2/en not_active Expired - Fee Related
- 2014-07-23 CN CN201480062326.5A patent/CN105723096A/en active Pending
- 2014-07-23 EP EP14879801.0A patent/EP3098454A4/en not_active Withdrawn
- 2014-07-23 US US15/039,312 patent/US20170167501A1/en not_active Abandoned
- 2014-07-23 WO PCT/JP2014/069451 patent/WO2015111243A1/en active Application Filing
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