Composite part design based on numerical simulation of the manufacturing process

Abstract In aeronautics, the decreased density of structural components is a major factor to consider in order to satisfy economic, environmental, and technical requirements. Using composite materials is justifying good weight to mechanical strength compromise. Mechanical strength depends on shapes,...
Ausführliche Beschreibung

Gespeichert in:

Autor*in:	Mouton, Serge [verfasserIn] Ledoux, Yann Teissandier, Denis Sébastian, Patrick

Format:	E-Artikel
Sprache:	Englisch

Erschienen:	2010

Schlagwörter:	Resin transfer molding (RTM) Numerical simulations Failure risk Design for manufacturing and assembly (DFMA)

Anmerkung:	© Springer-Verlag London Limited 2010

Übergeordnetes Werk:	Enthalten in: The international journal of advanced manufacturing technology - London : Springer, 1985, 55(2010), 5-8 vom: 31. Dez., Seite 421-431
Übergeordnetes Werk:	volume:55 ; year:2010 ; number:5-8 ; day:31 ; month:12 ; pages:421-431

Links:	Volltext

DOI / URN:	10.1007/s00170-010-3107-3

Katalog-ID:	SPR001677985

Internformat


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650		4	\|a Numerical simulations \|7 (dpeaa)DE-He213
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700	1		\|a Sébastian, Patrick \|4 aut
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allfields	10.1007/s00170-010-3107-3 doi (DE-627)SPR001677985 (SPR)s00170-010-3107-3-e DE-627 ger DE-627 rakwb eng Mouton, Serge verfasserin aut Composite part design based on numerical simulation of the manufacturing process 2010 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © Springer-Verlag London Limited 2010 Abstract In aeronautics, the decreased density of structural components is a major factor to consider in order to satisfy economic, environmental, and technical requirements. Using composite materials is justifying good weight to mechanical strength compromise. Mechanical strength depends on shapes, dimensions, and materials defined at the design stage and in manufacturing and assembling process of the part. In this article, a general method is proposed to evaluate the performance of the design choices based on the failure risk of an assembled part. This evaluation integrates manufacturing deviations from the shaping operation (resin transfer molding). Three criteria are derived from numerical simulations of RTM process and assembly phase. These criteria assist the designer early in the design cycle to appreciate the consequences of manufacturing choices on the mechanical strength of an assembled part. The approach will be applied to an airplane component. Resin transfer molding (RTM) (dpeaa)DE-He213 Numerical simulations (dpeaa)DE-He213 Failure risk (dpeaa)DE-He213 Design for manufacturing and assembly (DFMA) (dpeaa)DE-He213 Ledoux, Yann aut Teissandier, Denis aut Sébastian, Patrick aut Enthalten in The international journal of advanced manufacturing technology London : Springer, 1985 55(2010), 5-8 vom: 31. Dez., Seite 421-431 (DE-627)270127712 (DE-600)1476510-X 1433-3015 nnns volume:55 year:2010 number:5-8 day:31 month:12 pages:421-431 https://dx.doi.org/10.1007/s00170-010-3107-3 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_206 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2070 GBV_ILN_2086 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2116 GBV_ILN_2118 GBV_ILN_2119 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4012 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 55 2010 5-8 31 12 421-431
spelling	10.1007/s00170-010-3107-3 doi (DE-627)SPR001677985 (SPR)s00170-010-3107-3-e DE-627 ger DE-627 rakwb eng Mouton, Serge verfasserin aut Composite part design based on numerical simulation of the manufacturing process 2010 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © Springer-Verlag London Limited 2010 Abstract In aeronautics, the decreased density of structural components is a major factor to consider in order to satisfy economic, environmental, and technical requirements. Using composite materials is justifying good weight to mechanical strength compromise. Mechanical strength depends on shapes, dimensions, and materials defined at the design stage and in manufacturing and assembling process of the part. In this article, a general method is proposed to evaluate the performance of the design choices based on the failure risk of an assembled part. This evaluation integrates manufacturing deviations from the shaping operation (resin transfer molding). Three criteria are derived from numerical simulations of RTM process and assembly phase. These criteria assist the designer early in the design cycle to appreciate the consequences of manufacturing choices on the mechanical strength of an assembled part. The approach will be applied to an airplane component. Resin transfer molding (RTM) (dpeaa)DE-He213 Numerical simulations (dpeaa)DE-He213 Failure risk (dpeaa)DE-He213 Design for manufacturing and assembly (DFMA) (dpeaa)DE-He213 Ledoux, Yann aut Teissandier, Denis aut Sébastian, Patrick aut Enthalten in The international journal of advanced manufacturing technology London : Springer, 1985 55(2010), 5-8 vom: 31. Dez., Seite 421-431 (DE-627)270127712 (DE-600)1476510-X 1433-3015 nnns volume:55 year:2010 number:5-8 day:31 month:12 pages:421-431 https://dx.doi.org/10.1007/s00170-010-3107-3 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_206 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2070 GBV_ILN_2086 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2116 GBV_ILN_2118 GBV_ILN_2119 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4012 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 55 2010 5-8 31 12 421-431
allfields_unstemmed	10.1007/s00170-010-3107-3 doi (DE-627)SPR001677985 (SPR)s00170-010-3107-3-e DE-627 ger DE-627 rakwb eng Mouton, Serge verfasserin aut Composite part design based on numerical simulation of the manufacturing process 2010 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © Springer-Verlag London Limited 2010 Abstract In aeronautics, the decreased density of structural components is a major factor to consider in order to satisfy economic, environmental, and technical requirements. Using composite materials is justifying good weight to mechanical strength compromise. Mechanical strength depends on shapes, dimensions, and materials defined at the design stage and in manufacturing and assembling process of the part. In this article, a general method is proposed to evaluate the performance of the design choices based on the failure risk of an assembled part. This evaluation integrates manufacturing deviations from the shaping operation (resin transfer molding). Three criteria are derived from numerical simulations of RTM process and assembly phase. These criteria assist the designer early in the design cycle to appreciate the consequences of manufacturing choices on the mechanical strength of an assembled part. The approach will be applied to an airplane component. Resin transfer molding (RTM) (dpeaa)DE-He213 Numerical simulations (dpeaa)DE-He213 Failure risk (dpeaa)DE-He213 Design for manufacturing and assembly (DFMA) (dpeaa)DE-He213 Ledoux, Yann aut Teissandier, Denis aut Sébastian, Patrick aut Enthalten in The international journal of advanced manufacturing technology London : Springer, 1985 55(2010), 5-8 vom: 31. Dez., Seite 421-431 (DE-627)270127712 (DE-600)1476510-X 1433-3015 nnns volume:55 year:2010 number:5-8 day:31 month:12 pages:421-431 https://dx.doi.org/10.1007/s00170-010-3107-3 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_206 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2070 GBV_ILN_2086 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2116 GBV_ILN_2118 GBV_ILN_2119 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4012 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 55 2010 5-8 31 12 421-431
allfieldsGer	10.1007/s00170-010-3107-3 doi (DE-627)SPR001677985 (SPR)s00170-010-3107-3-e DE-627 ger DE-627 rakwb eng Mouton, Serge verfasserin aut Composite part design based on numerical simulation of the manufacturing process 2010 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © Springer-Verlag London Limited 2010 Abstract In aeronautics, the decreased density of structural components is a major factor to consider in order to satisfy economic, environmental, and technical requirements. Using composite materials is justifying good weight to mechanical strength compromise. Mechanical strength depends on shapes, dimensions, and materials defined at the design stage and in manufacturing and assembling process of the part. In this article, a general method is proposed to evaluate the performance of the design choices based on the failure risk of an assembled part. This evaluation integrates manufacturing deviations from the shaping operation (resin transfer molding). Three criteria are derived from numerical simulations of RTM process and assembly phase. These criteria assist the designer early in the design cycle to appreciate the consequences of manufacturing choices on the mechanical strength of an assembled part. The approach will be applied to an airplane component. Resin transfer molding (RTM) (dpeaa)DE-He213 Numerical simulations (dpeaa)DE-He213 Failure risk (dpeaa)DE-He213 Design for manufacturing and assembly (DFMA) (dpeaa)DE-He213 Ledoux, Yann aut Teissandier, Denis aut Sébastian, Patrick aut Enthalten in The international journal of advanced manufacturing technology London : Springer, 1985 55(2010), 5-8 vom: 31. Dez., Seite 421-431 (DE-627)270127712 (DE-600)1476510-X 1433-3015 nnns volume:55 year:2010 number:5-8 day:31 month:12 pages:421-431 https://dx.doi.org/10.1007/s00170-010-3107-3 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_206 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2070 GBV_ILN_2086 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2116 GBV_ILN_2118 GBV_ILN_2119 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4012 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 55 2010 5-8 31 12 421-431
allfieldsSound	10.1007/s00170-010-3107-3 doi (DE-627)SPR001677985 (SPR)s00170-010-3107-3-e DE-627 ger DE-627 rakwb eng Mouton, Serge verfasserin aut Composite part design based on numerical simulation of the manufacturing process 2010 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © Springer-Verlag London Limited 2010 Abstract In aeronautics, the decreased density of structural components is a major factor to consider in order to satisfy economic, environmental, and technical requirements. Using composite materials is justifying good weight to mechanical strength compromise. Mechanical strength depends on shapes, dimensions, and materials defined at the design stage and in manufacturing and assembling process of the part. In this article, a general method is proposed to evaluate the performance of the design choices based on the failure risk of an assembled part. This evaluation integrates manufacturing deviations from the shaping operation (resin transfer molding). Three criteria are derived from numerical simulations of RTM process and assembly phase. These criteria assist the designer early in the design cycle to appreciate the consequences of manufacturing choices on the mechanical strength of an assembled part. The approach will be applied to an airplane component. Resin transfer molding (RTM) (dpeaa)DE-He213 Numerical simulations (dpeaa)DE-He213 Failure risk (dpeaa)DE-He213 Design for manufacturing and assembly (DFMA) (dpeaa)DE-He213 Ledoux, Yann aut Teissandier, Denis aut Sébastian, Patrick aut Enthalten in The international journal of advanced manufacturing technology London : Springer, 1985 55(2010), 5-8 vom: 31. Dez., Seite 421-431 (DE-627)270127712 (DE-600)1476510-X 1433-3015 nnns volume:55 year:2010 number:5-8 day:31 month:12 pages:421-431 https://dx.doi.org/10.1007/s00170-010-3107-3 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_206 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2070 GBV_ILN_2086 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2116 GBV_ILN_2118 GBV_ILN_2119 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4012 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 55 2010 5-8 31 12 421-431
language	English
source	Enthalten in The international journal of advanced manufacturing technology 55(2010), 5-8 vom: 31. Dez., Seite 421-431 volume:55 year:2010 number:5-8 day:31 month:12 pages:421-431
sourceStr	Enthalten in The international journal of advanced manufacturing technology 55(2010), 5-8 vom: 31. Dez., Seite 421-431 volume:55 year:2010 number:5-8 day:31 month:12 pages:421-431
format_phy_str_mv	Article
institution	findex.gbv.de
topic_facet	Resin transfer molding (RTM) Numerical simulations Failure risk Design for manufacturing and assembly (DFMA)
isfreeaccess_bool	false
container_title	The international journal of advanced manufacturing technology
authorswithroles_txt_mv	Mouton, Serge @@aut@@ Ledoux, Yann @@aut@@ Teissandier, Denis @@aut@@ Sébastian, Patrick @@aut@@
publishDateDaySort_date	2010-12-31T00:00:00Z
hierarchy_top_id	270127712
id	SPR001677985
language_de	englisch
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author	Mouton, Serge
spellingShingle	Mouton, Serge misc Resin transfer molding (RTM) misc Numerical simulations misc Failure risk misc Design for manufacturing and assembly (DFMA) Composite part design based on numerical simulation of the manufacturing process
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topic_title	Composite part design based on numerical simulation of the manufacturing process Resin transfer molding (RTM) (dpeaa)DE-He213 Numerical simulations (dpeaa)DE-He213 Failure risk (dpeaa)DE-He213 Design for manufacturing and assembly (DFMA) (dpeaa)DE-He213
topic	misc Resin transfer molding (RTM) misc Numerical simulations misc Failure risk misc Design for manufacturing and assembly (DFMA)
topic_unstemmed	misc Resin transfer molding (RTM) misc Numerical simulations misc Failure risk misc Design for manufacturing and assembly (DFMA)
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title	Composite part design based on numerical simulation of the manufacturing process
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title_full	Composite part design based on numerical simulation of the manufacturing process
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author_browse	Mouton, Serge Ledoux, Yann Teissandier, Denis Sébastian, Patrick
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title_sort	composite part design based on numerical simulation of the manufacturing process
title_auth	Composite part design based on numerical simulation of the manufacturing process
abstract	Abstract In aeronautics, the decreased density of structural components is a major factor to consider in order to satisfy economic, environmental, and technical requirements. Using composite materials is justifying good weight to mechanical strength compromise. Mechanical strength depends on shapes, dimensions, and materials defined at the design stage and in manufacturing and assembling process of the part. In this article, a general method is proposed to evaluate the performance of the design choices based on the failure risk of an assembled part. This evaluation integrates manufacturing deviations from the shaping operation (resin transfer molding). Three criteria are derived from numerical simulations of RTM process and assembly phase. These criteria assist the designer early in the design cycle to appreciate the consequences of manufacturing choices on the mechanical strength of an assembled part. The approach will be applied to an airplane component. © Springer-Verlag London Limited 2010
abstractGer	Abstract In aeronautics, the decreased density of structural components is a major factor to consider in order to satisfy economic, environmental, and technical requirements. Using composite materials is justifying good weight to mechanical strength compromise. Mechanical strength depends on shapes, dimensions, and materials defined at the design stage and in manufacturing and assembling process of the part. In this article, a general method is proposed to evaluate the performance of the design choices based on the failure risk of an assembled part. This evaluation integrates manufacturing deviations from the shaping operation (resin transfer molding). Three criteria are derived from numerical simulations of RTM process and assembly phase. These criteria assist the designer early in the design cycle to appreciate the consequences of manufacturing choices on the mechanical strength of an assembled part. The approach will be applied to an airplane component. © Springer-Verlag London Limited 2010
abstract_unstemmed	Abstract In aeronautics, the decreased density of structural components is a major factor to consider in order to satisfy economic, environmental, and technical requirements. Using composite materials is justifying good weight to mechanical strength compromise. Mechanical strength depends on shapes, dimensions, and materials defined at the design stage and in manufacturing and assembling process of the part. In this article, a general method is proposed to evaluate the performance of the design choices based on the failure risk of an assembled part. This evaluation integrates manufacturing deviations from the shaping operation (resin transfer molding). Three criteria are derived from numerical simulations of RTM process and assembly phase. These criteria assist the designer early in the design cycle to appreciate the consequences of manufacturing choices on the mechanical strength of an assembled part. The approach will be applied to an airplane component. © Springer-Verlag London Limited 2010
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title_short	Composite part design based on numerical simulation of the manufacturing process
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doi_str	10.1007/s00170-010-3107-3
up_date	2024-07-03T23:51:56.567Z
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Composite part design based on numerical simulation of the manufacturing process

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