JP6471154B2 - 非軸対称表面をモデル化する方法 - Google Patents

非軸対称表面をモデル化する方法 Download PDF

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JP6471154B2
JP6471154B2 JP2016524869A JP2016524869A JP6471154B2 JP 6471154 B2 JP6471154 B2 JP 6471154B2 JP 2016524869 A JP2016524869 A JP 2016524869A JP 2016524869 A JP2016524869 A JP 2016524869A JP 6471154 B2 JP6471154 B2 JP 6471154B2
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JP2016524260A5 (enExample
JP2016524260A (ja
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セリエ,ダミアン・ジョゼフ
ペロ,バンサン
ボルブレグト,マチュー・ジャン・リュック
ピニエ,ニコラ・ジャン・フェルナン
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サフラン・エアクラフト・エンジンズ
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    • GPHYSICS
    • G06COMPUTING OR CALCULATING; COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F30/00Computer-aided design [CAD]
    • GPHYSICS
    • G06COMPUTING OR CALCULATING; COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F17/00Digital computing or data processing equipment or methods, specially adapted for specific functions
    • GPHYSICS
    • G06COMPUTING OR CALCULATING; COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F30/00Computer-aided design [CAD]
    • G06F30/20Design optimisation, verification or simulation
    • GPHYSICS
    • G06COMPUTING OR CALCULATING; COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F30/00Computer-aided design [CAD]
    • G06F30/10Geometric CAD
    • G06F30/17Mechanical parametric or variational design

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  • Physics & Mathematics (AREA)
  • Theoretical Computer Science (AREA)
  • Geometry (AREA)
  • General Physics & Mathematics (AREA)
  • General Engineering & Computer Science (AREA)
  • Computer Hardware Design (AREA)
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  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Architecture (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
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JP2016524869A 2013-07-09 2014-07-07 非軸対称表面をモデル化する方法 Active JP6471154B2 (ja)

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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JP2016524260A JP2016524260A (ja) 2016-08-12
JP2016524260A5 JP2016524260A5 (enExample) 2017-07-27
JP6471154B2 true JP6471154B2 (ja) 2019-02-13

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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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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
DE602005011683D1 (de) * 2005-07-19 2009-01-22 Honeywell Int Inc Turbolader mit variabler düse
US7465155B2 (en) * 2006-02-27 2008-12-16 Honeywell International Inc. Non-axisymmetric end wall contouring for a turbomachine blade row
CN100383823C (zh) * 2006-06-08 2008-04-23 东南大学 三维扫描的点云孔洞填补方法
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
FR2971540B1 (fr) * 2011-02-10 2013-03-08 Snecma Ensemble pale-plateforme pour ecoulement supersonique

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Publication number Publication date
BR112016000393B1 (pt) 2022-07-19
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
CN105378735B (zh) 2018-08-28
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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