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
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JP
Japan
Prior art keywords
pressure surface
hole
impeller according
surface side
blade
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JP2014009680A
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Japanese (ja)
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JP2015137592A (en
JP6249219B2 (en
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Priority claimed from JP2014009680A external-priority patent/JP6249219B2/en
Priority to JP2014009680A priority Critical patent/JP6249219B2/en
Priority to CN201480062326.5A priority patent/CN105723096A/en
Priority to US15/039,312 priority patent/US20170167501A1/en
Priority to PCT/JP2014/069451 priority patent/WO2015111243A1/en
Priority to EP14879801.0A priority patent/EP3098454A4/en
Publication of JP2015137592A publication Critical patent/JP2015137592A/en
Publication of JP2015137592A5 publication Critical patent/JP2015137592A5/ja
Publication of JP6249219B2 publication Critical patent/JP6249219B2/en
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Expired - Fee Related legal-status Critical Current
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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)

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 .
前記孔部は、圧力面側から負圧面側に向かうにしたがって、前記流路の下流側に向かって延びている請求項1に記載のインペラ。   2. The impeller according to claim 1, wherein the hole extends toward the downstream side of the flow path from the pressure surface side toward the negative pressure surface side. 複数の前記孔部が、前記径方向内側から外側に向かって互いに離間して配列されている請求項1又は2に記載のインペラ。   The impeller according to claim 1 or 2, wherein the plurality of holes are arranged to be spaced apart from each other from the radially inner side toward the outer side. 前記孔部は、前記圧力面側から前記負圧面側に向かうにしたがって開孔面積が拡大する請求項1から3のいずれか一項に記載のインペラ。   The impeller according to any one of claims 1 to 3, wherein an opening area of the hole portion increases from the pressure surface side toward the negative pressure surface side. 前記孔部は、前記圧力面側から前記負圧面側に向かうにしたがって開孔面積が縮小する請求項1から4のいずれか一項に記載のインペラ。   The impeller according to any one of claims 1 to 4, wherein an aperture area of the hole portion decreases from the pressure surface side toward the negative pressure surface side. 前記孔部は、該孔部の内周面に螺旋状に形成された溝を有する請求項1から5のいずれか一項に記載のインペラ。   The impeller according to any one of claims 1 to 5, wherein the hole includes a groove formed in a spiral shape on an inner peripheral surface of the hole. 前記孔部は、前記圧力面側に設けられた1つの流入口を有し、前記流入口にそれぞれ連通するとともに前記負圧面側に設けられた複数の噴射口を有する請求項1から5のいずれか一項に記載のインペラ。   The said hole part has one inflow port provided in the said pressure surface side, and has each of the said inflow port, and has a several injection port provided in the said negative pressure surface side. The impeller according to claim 1. 請求項1から7のいずれか一項に記載のインペラを備える遠心圧縮機。   A centrifugal compressor comprising the impeller according to any one of claims 1 to 7.
JP2014009680A 2014-01-22 2014-01-22 Impeller and centrifugal compressor Expired - Fee Related JP6249219B2 (en)

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)

* Cited by examiner, † Cited by third party
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

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