Structure and properties of АА7075-SiC composite parts produced by cold spray additive manufacturing
In this work, the cold spray additive manufacturing technology was applied for producing composite AA7075 deposits reinforced by silicon carbide particles. It was found that ceramic content in the composite did not exceed 21–25 %vol. Different heat treatments and capsule-free hot isostatic pressing...
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| Veröffentlicht in: | International journal of advanced manufacturing technology 2021-09, Vol.116 (3-4), p.847-861 |
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| creator | Khomutov, Maxim Spasenko, Anastasia Sova, Alexey Petrovskiy, Pavel Cheverikin, Vladimir Travyanov, Andrey Smurov, Igor |
| description | In this work, the cold spray additive manufacturing technology was applied for producing composite AA7075 deposits reinforced by silicon carbide particles. It was found that ceramic content in the composite did not exceed 21–25 %vol. Different heat treatments and capsule-free hot isostatic pressing (HIP) were performed to homogenise the structure of the AA7075-SiC composite. The microstructure of the composite before and after heat treatments was analysed using SEM and TEM analysis and compared with bulk AA7075. The analysis showed that the presence of SiC in the composite influenced the distribution of hardening phases in AA7075 during heat treatment. The presence of uniformly distributed SiC particles accelerated the decomposition of the supersaturated aluminium solid solution during ageing. The decomposition process blocked the formation of large hardening precipitates at the grain boundaries generally observed at the bulk metallic alloy AA7075. The compressive strength tests revealed the improvement of the strain at failure of the composite deposits after heat treatment and HIP. At the same time, the compressive strength slightly decreased. The thermal expansion coefficient (TEC) of AA7075-SiC20% composite was lower than for the base bulk AA7075. The dilatation behaviour of the composite during TEC tests could be approximated using the simple rule of mixture. |
| doi_str_mv | 10.1007/s00170-021-07457-w |
| format | Article |
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It was found that ceramic content in the composite did not exceed 21–25 %vol. Different heat treatments and capsule-free hot isostatic pressing (HIP) were performed to homogenise the structure of the AA7075-SiC composite. The microstructure of the composite before and after heat treatments was analysed using SEM and TEM analysis and compared with bulk AA7075. The analysis showed that the presence of SiC in the composite influenced the distribution of hardening phases in AA7075 during heat treatment. The presence of uniformly distributed SiC particles accelerated the decomposition of the supersaturated aluminium solid solution during ageing. The decomposition process blocked the formation of large hardening precipitates at the grain boundaries generally observed at the bulk metallic alloy AA7075. The compressive strength tests revealed the improvement of the strain at failure of the composite deposits after heat treatment and HIP. At the same time, the compressive strength slightly decreased. The thermal expansion coefficient (TEC) of AA7075-SiC20% composite was lower than for the base bulk AA7075. 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It was found that ceramic content in the composite did not exceed 21–25 %vol. Different heat treatments and capsule-free hot isostatic pressing (HIP) were performed to homogenise the structure of the AA7075-SiC composite. The microstructure of the composite before and after heat treatments was analysed using SEM and TEM analysis and compared with bulk AA7075. The analysis showed that the presence of SiC in the composite influenced the distribution of hardening phases in AA7075 during heat treatment. The presence of uniformly distributed SiC particles accelerated the decomposition of the supersaturated aluminium solid solution during ageing. The decomposition process blocked the formation of large hardening precipitates at the grain boundaries generally observed at the bulk metallic alloy AA7075. The compressive strength tests revealed the improvement of the strain at failure of the composite deposits after heat treatment and HIP. At the same time, the compressive strength slightly decreased. The thermal expansion coefficient (TEC) of AA7075-SiC20% composite was lower than for the base bulk AA7075. The dilatation behaviour of the composite during TEC tests could be approximated using the simple rule of mixture.</description><subject>Additive manufacturing</subject><subject>Aluminum base alloys</subject><subject>CAE) and Design</subject><subject>Cold working</subject><subject>Compressive strength</subject><subject>Computer-Aided Engineering (CAD</subject><subject>Decomposition</subject><subject>Engineering</subject><subject>Engineering Sciences</subject><subject>Grain boundaries</subject><subject>Heat treating</subject><subject>Heat treatment</subject><subject>Hot isostatic pressing</subject><subject>Industrial and Production Engineering</subject><subject>Mechanical Engineering</subject><subject>Media Management</subject><subject>Original Article</subject><subject>Precipitates</subject><subject>Silicon carbide</subject><subject>Solid solutions</subject><subject>Thermal expansion</subject><issn>0268-3768</issn><issn>1433-3015</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2021</creationdate><recordtype>article</recordtype><sourceid>AFKRA</sourceid><sourceid>BENPR</sourceid><sourceid>CCPQU</sourceid><sourceid>DWQXO</sourceid><recordid>eNp9kM1KAzEUhYMoWKsv4CrgykX05mcm02UpaoWCi-o6pPnRKW1nTGZa-hZ9tD6SGUd0J3cRuPnO4dyD0DWFOwog7yMAlUCAUQJSZJLsTtCACs4JB5qdogGwvCBc5sU5uohxmfCc5sUA-XkTWtO0wWG9sbgOVe1CU7qIK4-Ph-NBgszIvJxgU63rKpaNw7UOTexQ2xpn8WKf_lYWxzroPdbWlk25dXitN63XnXW5eb9EZ16vorv6eYfo7fHhdTIls5en58l4RkzKtyOiMCPHjJMMpOfUWsu8FsynSdEpXeQ5zUyu9YJqzbX0JvfFwhaFkGzkheBDdNv7fuiVqkO51mGvKl2q6Ximuh0IKAQA39LE3vRsuuSzdbFRy6oNmxRPsSyTHEYw6ijWUyZUMQbnf20pqK571XevUvfqu3u1SyLei1In6XoX_qz_UX0Bj3mI0w</recordid><startdate>20210901</startdate><enddate>20210901</enddate><creator>Khomutov, Maxim</creator><creator>Spasenko, Anastasia</creator><creator>Sova, Alexey</creator><creator>Petrovskiy, Pavel</creator><creator>Cheverikin, Vladimir</creator><creator>Travyanov, Andrey</creator><creator>Smurov, Igor</creator><general>Springer London</general><general>Springer Nature B.V</general><general>Springer Verlag</general><scope>AAYXX</scope><scope>CITATION</scope><scope>8FE</scope><scope>8FG</scope><scope>ABJCF</scope><scope>AFKRA</scope><scope>BENPR</scope><scope>BGLVJ</scope><scope>CCPQU</scope><scope>DWQXO</scope><scope>HCIFZ</scope><scope>L6V</scope><scope>M7S</scope><scope>PQEST</scope><scope>PQQKQ</scope><scope>PQUKI</scope><scope>PTHSS</scope><scope>1XC</scope><orcidid>https://orcid.org/0000-0002-7701-1600</orcidid></search><sort><creationdate>20210901</creationdate><title>Structure and properties of АА7075-SiC composite parts produced by cold spray additive manufacturing</title><author>Khomutov, Maxim ; 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It was found that ceramic content in the composite did not exceed 21–25 %vol. Different heat treatments and capsule-free hot isostatic pressing (HIP) were performed to homogenise the structure of the AA7075-SiC composite. The microstructure of the composite before and after heat treatments was analysed using SEM and TEM analysis and compared with bulk AA7075. The analysis showed that the presence of SiC in the composite influenced the distribution of hardening phases in AA7075 during heat treatment. The presence of uniformly distributed SiC particles accelerated the decomposition of the supersaturated aluminium solid solution during ageing. The decomposition process blocked the formation of large hardening precipitates at the grain boundaries generally observed at the bulk metallic alloy AA7075. The compressive strength tests revealed the improvement of the strain at failure of the composite deposits after heat treatment and HIP. 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| subjects | Additive manufacturing Aluminum base alloys CAE) and Design Cold working Compressive strength Computer-Aided Engineering (CAD Decomposition Engineering Engineering Sciences Grain boundaries Heat treating Heat treatment Hot isostatic pressing Industrial and Production Engineering Mechanical Engineering Media Management Original Article Precipitates Silicon carbide Solid solutions Thermal expansion |
| title | Structure and properties of АА7075-SiC composite parts produced by cold spray additive manufacturing |
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