CN105378735B - 用于对非轴对称表面进行建模的方法 - Google Patents

用于对非轴对称表面进行建模的方法 Download PDF

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CN105378735B
CN105378735B CN201480040598.5A CN201480040598A CN105378735B CN 105378735 B CN105378735 B CN 105378735B CN 201480040598 A CN201480040598 A CN 201480040598A CN 105378735 B CN105378735 B CN 105378735B
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CN105378735A (zh
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达米恩·约瑟夫·塞利尔
文森特·佩洛特
马修·让·卢克·沃勒布雷特
尼古拉斯·让·费尔南多·皮格尼尔
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Safran Aircraft Engines SAS
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SNECMA SAS
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    • G—PHYSICS
    • G06—COMPUTING OR CALCULATING; COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F30/00—Computer-aided design [CAD]
    • G—PHYSICS
    • G06—COMPUTING OR CALCULATING; COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F17/00—Digital computing or data processing equipment or methods, specially adapted for specific functions
    • G—PHYSICS
    • G06—COMPUTING OR CALCULATING; COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F30/00—Computer-aided design [CAD]
    • G06F30/20—Design optimisation, verification or simulation
    • G—PHYSICS
    • G06—COMPUTING OR CALCULATING; COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F30/00—Computer-aided design [CAD]
    • G06F30/10—Geometric CAD
    • G06F30/17—Mechanical parametric or variational design

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Theoretical Computer Science (AREA)
  • Geometry (AREA)
  • General Physics & Mathematics (AREA)
  • General Engineering & Computer Science (AREA)
  • Computer Hardware Design (AREA)
  • Evolutionary Computation (AREA)
  • Mathematical Optimization (AREA)
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  • Databases & Information Systems (AREA)
  • Mathematical Physics (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Architecture (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
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CN201480040598.5A 2013-07-09 2014-07-07 用于对非轴对称表面进行建模的方法 Active CN105378735B (zh)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1356732A FR3008507B1 (fr) 2013-07-09 2013-07-09 Procede de modelisation d'une surface non-axisymetrique
FR1356732 2013-07-09
PCT/FR2014/051744 WO2015004377A1 (fr) 2013-07-09 2014-07-07 Procédé de modélisation d'une surface non-axisymétrique

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CN105378735A CN105378735A (zh) 2016-03-02
CN105378735B true CN105378735B (zh) 2018-08-28

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US (1) US10216867B2 (enExample)
EP (1) EP3019989B1 (enExample)
JP (1) JP6471154B2 (enExample)
CN (1) CN105378735B (enExample)
BR (1) BR112016000393B1 (enExample)
CA (1) CA2917225C (enExample)
FR (1) FR3008507B1 (enExample)
RU (1) RU2670380C2 (enExample)
WO (1) WO2015004377A1 (enExample)

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JP6518526B2 (ja) * 2015-06-18 2019-05-22 三菱日立パワーシステムズ株式会社 軸流タービン
CN106202674B (zh) * 2016-07-01 2019-06-18 中航空天发动机研究院有限公司 一种非轴对称元件的二维数值计算方法
CN108038259B (zh) * 2017-11-06 2021-05-28 中国商用飞机有限责任公司 基于曲率生成气动部件外形的方法
US10962021B2 (en) 2018-08-17 2021-03-30 Rolls-Royce Corporation Non-axisymmetric impeller hub flowpath
CN111435399B (zh) 2018-12-25 2023-05-23 中国航发商用航空发动机有限责任公司 风扇组件的造型方法
CN111460571B (zh) * 2019-01-02 2023-07-21 中国航发商用航空发动机有限责任公司 中介机匣部件的型线的构造方法、构造装置以及计算机可读存储介质
CN110362929B (zh) * 2019-07-17 2020-12-15 重庆大学 一种组合结合面的装配误差传递属性分析方法
CN112419502A (zh) * 2020-11-23 2021-02-26 苏州千机智能技术有限公司 发动机叶盘的叶片曲面重建方法
US11480073B2 (en) * 2020-11-24 2022-10-25 Rolls-Royce Plc Gas turbine engine nacelle and method of designing same

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CN1858801A (zh) * 2006-06-08 2006-11-08 东南大学 三维扫描的点云孔洞填补方法
WO2007011355A1 (en) * 2005-07-19 2007-01-25 Honeywell International Inc. Variable nozzle turbocharger
WO2012107677A1 (fr) * 2011-02-10 2012-08-16 Snecma Ensemble pale-plateforme pour ecoulement supersonique.

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RU2137286C1 (ru) * 1998-06-29 1999-09-10 Харьковский государственный технический университет радиоэлектроники Пазонный способ моделирования электрических машин и устройство для его осуществления
WO2004095322A2 (en) * 2003-04-21 2004-11-04 Ugs Plm Solutions Inc. System and method for multiple-sided surface matching with curvature continuity
US7465155B2 (en) * 2006-02-27 2008-12-16 Honeywell International Inc. Non-axisymmetric end wall contouring for a turbomachine blade row
JP5283855B2 (ja) * 2007-03-29 2013-09-04 株式会社Ｉｈｉ ターボ機械の壁、及びターボ機械
EP2165167B1 (en) * 2007-04-30 2016-03-16 Nuovo Pignone S.p.A. Method and system for turbine blade characterization
FR2928172B1 (fr) * 2008-02-28 2015-07-17 Snecma Aube avec plateforme non axisymetrique lineaire.
US8439643B2 (en) * 2009-08-20 2013-05-14 General Electric Company Biformal platform turbine blade

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Publication number Priority date Publication date Assignee Title
WO2007011355A1 (en) * 2005-07-19 2007-01-25 Honeywell International Inc. Variable nozzle turbocharger
CN1858801A (zh) * 2006-06-08 2006-11-08 东南大学 三维扫描的点云孔洞填补方法
WO2012107677A1 (fr) * 2011-02-10 2012-08-16 Snecma Ensemble pale-plateforme pour ecoulement supersonique.

Non-Patent Citations (3)

* Cited by examiner, † Cited by third party
Title
"A Design Method For Turbine Blades Using Genetic Algorithms On Parallel Computers";K.C. Giannakoglou;《Computational Fluid Dynamics》;19980101;第2-5页 *
"Analysis and optimization of transonic centrifugal compressor impellers using the design of experiments technique";D Bonaiuti,et al.;《Journal of turbomachinery》;20060101;第128卷(第04期);第786-796页 *
"Rapid Meshing of Turbomachinery Rows Using Semi-Unstructured Conformal Grids";Manuel A. Burgos.et al;《Engineering with Computers》;20091215;第26卷(第04期);第351-360页 *

Also Published As

Publication number Publication date
BR112016000393B1 (pt) 2022-07-19
JP6471154B2 (ja) 2019-02-13
FR3008507B1 (fr) 2017-04-14
CN105378735A (zh) 2016-03-02
JP2016524260A (ja) 2016-08-12
RU2016104022A (ru) 2017-08-14
RU2016104022A3 (enExample) 2018-05-29
EP3019989B1 (fr) 2024-10-30
BR112016000393A2 (enExample) 2017-07-25
EP3019989A1 (fr) 2016-05-18
US20160154901A1 (en) 2016-06-02
CA2917225A1 (fr) 2015-01-15
FR3008507A1 (fr) 2015-01-16
RU2670380C2 (ru) 2018-10-22
US10216867B2 (en) 2019-02-26
CA2917225C (fr) 2021-03-16
WO2015004377A1 (fr) 2015-01-15

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