JP5037171B2 - 低レイノルズ数領域で低損失を可能とする軸流型圧縮機用翼型 - Google Patents
低レイノルズ数領域で低損失を可能とする軸流型圧縮機用翼型 Download PDFInfo
- Publication number
- JP5037171B2 JP5037171B2 JP2007047160A JP2007047160A JP5037171B2 JP 5037171 B2 JP5037171 B2 JP 5037171B2 JP 2007047160 A JP2007047160 A JP 2007047160A JP 2007047160 A JP2007047160 A JP 2007047160A JP 5037171 B2 JP5037171 B2 JP 5037171B2
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- JP
- Japan
- Prior art keywords
- airfoil
- reynolds number
- cord
- leading edge
- low
- 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 - Fee Related
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/38—Blades
- F04D29/384—Blades characterised by form
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
- F04D29/68—Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers
- F04D29/681—Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers especially adapted for elastic fluid pumps
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S415/00—Rotary kinetic fluid motors or pumps
- Y10S415/914—Device to control boundary layer
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S416/00—Fluid reaction surfaces, i.e. impellers
- Y10S416/02—Formulas of curves
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S416/00—Fluid reaction surfaces, i.e. impellers
- Y10S416/05—Variable camber or chord length
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Description
12 後縁
13 腹面
14 背面
Claims (5)
- 前縁(11)および後縁(12)間に正圧を発生する腹面(13)および負圧を発生する背面(14)を備えた翼型であって、
背面(14)側の流速分布が、前縁(11)の位置を0%とし、後縁(12)の位置を100%としたコード上に超音速の極大値を一つだけ有するとともに、前記極大値は前縁(11)から6%以内にあり、かつ翼型の前縁部の翼厚分布が変曲点を有することを特徴とする、低レイノルズ数領域で低損失を可能とする軸流型圧縮機用翼型。 - 背面(14)側の流速分布における超音速領域がコード上で前縁(11)から15%以内に限られることを特徴とする、請求項1に記載の軸流型圧縮機用翼型。
- 前記変曲点はコード上で前縁(11)から3%〜20%の範囲に在ることを特徴とする、請求項1に記載の低レイノルズ数領域で低損失を可能とする軸流型圧縮機用翼型。
- 前記超音速の極大値はマッハ1.3以下であることを特徴とする、請求項1に記載の低レイノルズ数領域で低損失を可能とする軸流型圧縮機用翼型。
- 前記翼型は圧縮機のアウトレットガイドベーンあるいは静翼あるいは動翼のスパン方向の少なくとも一部において採用されることを特徴とする、請求項1〜請求項4の何れか1項に記載の低レイノルズ数領域で低損失を可能とする軸流型圧縮機用翼型。
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102006019946.4A DE102006019946B4 (de) | 2006-04-28 | 2006-04-28 | Flügelprofil für einen Axialströmungskompressor, das die Verluste im Bereich niedriger Reynolds-Zahlen verringern kann |
DE102006019946.4 | 2006-04-28 |
Related Child Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2011274257A Division JP5342637B2 (ja) | 2006-04-28 | 2011-12-15 | 低レイノルズ数領域で低損失を可能とする軸流型圧縮機用翼型 |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2007298025A JP2007298025A (ja) | 2007-11-15 |
JP5037171B2 true JP5037171B2 (ja) | 2012-09-26 |
Family
ID=38564725
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2007047160A Expired - Fee Related JP5037171B2 (ja) | 2006-04-28 | 2007-02-27 | 低レイノルズ数領域で低損失を可能とする軸流型圧縮機用翼型 |
JP2011274257A Expired - Fee Related JP5342637B2 (ja) | 2006-04-28 | 2011-12-15 | 低レイノルズ数領域で低損失を可能とする軸流型圧縮機用翼型 |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2011274257A Expired - Fee Related JP5342637B2 (ja) | 2006-04-28 | 2011-12-15 | 低レイノルズ数領域で低損失を可能とする軸流型圧縮機用翼型 |
Country Status (3)
Country | Link |
---|---|
US (1) | US8152459B2 (ja) |
JP (2) | JP5037171B2 (ja) |
DE (1) | DE102006019946B4 (ja) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102010027588A1 (de) * | 2010-07-19 | 2012-01-19 | Rolls-Royce Deutschland Ltd & Co Kg | Fan-Nachleitradschaufel eines Turbofantriebwerks |
EP2927427A1 (de) * | 2014-04-04 | 2015-10-07 | MTU Aero Engines GmbH | Gasturbinenschaufel |
US10508549B2 (en) | 2014-06-06 | 2019-12-17 | United Technologies Corporation | Gas turbine engine airfoil with large thickness properties |
JP6468414B2 (ja) | 2014-08-12 | 2019-02-13 | 株式会社Ihi | 圧縮機静翼、軸流圧縮機、及びガスタービン |
WO2018216255A1 (ja) | 2017-05-24 | 2018-11-29 | 株式会社Ihi | ファン及び圧縮機の翼 |
US10710705B2 (en) * | 2017-06-28 | 2020-07-14 | General Electric Company | Open rotor and airfoil therefor |
CN108799205A (zh) * | 2018-04-13 | 2018-11-13 | 哈尔滨工程大学 | 一种带自抽吸作用的高负荷氦气压气机叶栅结构 |
EP4130436A4 (en) | 2020-04-01 | 2024-04-24 | Ihi Corp | STATIC BLADE AND AIRCRAFT GAS TURBINE |
US11873730B1 (en) | 2022-11-28 | 2024-01-16 | Rtx Corporation | Gas turbine engine airfoil with extended laminar flow |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS6048602B2 (ja) * | 1978-07-14 | 1985-10-28 | 株式会社日立製作所 | タ−ビン翼形 |
US4519746A (en) * | 1981-07-24 | 1985-05-28 | United Technologies Corporation | Airfoil blade |
JP2906939B2 (ja) * | 1993-09-20 | 1999-06-21 | 株式会社日立製作所 | 軸流圧縮機 |
JPH09256998A (ja) * | 1996-03-25 | 1997-09-30 | Senshin Zairyo Riyou Gas Jienereeta Kenkyusho:Kk | 圧縮機の翼 |
JPH09256997A (ja) * | 1996-03-25 | 1997-09-30 | Senshin Zairyo Riyou Gas Jienereeta Kenkyusho:Kk | 軸流圧縮機の動翼 |
JP2001234893A (ja) * | 2000-02-23 | 2001-08-31 | Hitachi Ltd | 軸流送風機 |
KR100349930B1 (ko) * | 2000-08-30 | 2002-08-24 | 학교법인 선문학원 | 프로펠러 팬 |
JP4737579B2 (ja) * | 2001-04-19 | 2011-08-03 | 株式会社Ihi | 圧縮機翼 |
JP4318940B2 (ja) * | 2002-10-08 | 2009-08-26 | 本田技研工業株式会社 | 圧縮機翼型 |
JP4563653B2 (ja) * | 2003-03-25 | 2010-10-13 | 本田技研工業株式会社 | 高転向・高遷音速翼 |
US20080118362A1 (en) * | 2006-11-16 | 2008-05-22 | Siemens Power Generation, Inc. | Transonic compressor rotors with non-monotonic meanline angle distributions |
-
2006
- 2006-04-28 DE DE102006019946.4A patent/DE102006019946B4/de not_active Expired - Fee Related
-
2007
- 2007-02-27 JP JP2007047160A patent/JP5037171B2/ja not_active Expired - Fee Related
- 2007-04-27 US US11/790,865 patent/US8152459B2/en not_active Expired - Fee Related
-
2011
- 2011-12-15 JP JP2011274257A patent/JP5342637B2/ja not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
DE102006019946A1 (de) | 2007-11-08 |
JP5342637B2 (ja) | 2013-11-13 |
US8152459B2 (en) | 2012-04-10 |
US20080181780A1 (en) | 2008-07-31 |
DE102006019946B4 (de) | 2016-12-22 |
JP2007298025A (ja) | 2007-11-15 |
JP2012052557A (ja) | 2012-03-15 |
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