An integrated polishing method for compressor blade surfaces
The surface quality and profile precision of compressor blades affect the performance and security of aircraft engines. Components with complex design specifications are difficult to manufacture, especially when polishing processes are needed to enable compliance with tight industrial standards. Bel...
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| Veröffentlicht in: | International journal of advanced manufacturing technology 2017-02, Vol.88 (5-8), p.1723-1733 |
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| container_issue | 5-8 |
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| container_title | International journal of advanced manufacturing technology |
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| creator | Xiao, Guijian Huang, Yun Yin, Jiachao |
| description | The surface quality and profile precision of compressor blades affect the performance and security of aircraft engines. Components with complex design specifications are difficult to manufacture, especially when polishing processes are needed to enable compliance with tight industrial standards. Belt polishing and bob polishing are commonly used in the precision manufacturing of components of gas turbine engines for aerospace and energy applications. These methods are used to polish different parts of the compressor blade. Information on integrated methods with belt polishing and bob polishing processes for full-area compressor blade (FACB) surfaces is scarce. In the present study, an integrated polishing method that combines bob polishing and seven-axis linkage belt polishing was used to improve the surface quality and profile precision of a FACB surface. The surfaces of three compressor blades were analyzed after polishing with each individual method and the integrated method. The surface roughness was less than 0.35 μm; the profile precision was higher than 0.05 mm; and the precision consistency was substantially improved. This proves that this polishing method, which integrates belt and bob polishing, can be used for automated polishing of compressor blade surfaces. |
| doi_str_mv | 10.1007/s00170-016-8891-y |
| format | Article |
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Components with complex design specifications are difficult to manufacture, especially when polishing processes are needed to enable compliance with tight industrial standards. Belt polishing and bob polishing are commonly used in the precision manufacturing of components of gas turbine engines for aerospace and energy applications. These methods are used to polish different parts of the compressor blade. Information on integrated methods with belt polishing and bob polishing processes for full-area compressor blade (FACB) surfaces is scarce. In the present study, an integrated polishing method that combines bob polishing and seven-axis linkage belt polishing was used to improve the surface quality and profile precision of a FACB surface. The surfaces of three compressor blades were analyzed after polishing with each individual method and the integrated method. The surface roughness was less than 0.35 μm; the profile precision was higher than 0.05 mm; and the precision consistency was substantially improved. 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The surface roughness was less than 0.35 μm; the profile precision was higher than 0.05 mm; and the precision consistency was substantially improved. This proves that this polishing method, which integrates belt and bob polishing, can be used for automated polishing of compressor blade surfaces.</description><subject>Aerospace engines</subject><subject>Aircraft engines</subject><subject>Belts</subject><subject>CAE) and Design</subject><subject>Compressor blades</subject><subject>Computer-Aided Engineering (CAD</subject><subject>Design specifications</subject><subject>Engineering</subject><subject>Gas turbine engines</subject><subject>Industrial and Production Engineering</subject><subject>Mechanical Engineering</subject><subject>Media Management</subject><subject>Original Article</subject><subject>Polishes</subject><subject>Polishing</subject><subject>Rapid prototyping</subject><subject>Surface properties</subject><subject>Surface roughness</subject><issn>0268-3768</issn><issn>1433-3015</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2017</creationdate><recordtype>article</recordtype><sourceid>BENPR</sourceid><recordid>eNp9kE1LAzEQhoMoWKs_wNuC52gmySZZ8FKKX1DwoueQbJJ2S7tZk-2h_96U9eBFYWDm8LzvwIPQLZB7IEQ-ZEJAEkxAYKUawMczNAPOGGYE6nM0I1QozKRQl-gq522hBQg1Q4-Lvur60a-TGb2rhrjr8qbr19Xej5voqhBT1cb9kHzO5bQ743yVDymY1udrdBHMLvubnz1Hn89PH8tXvHp_eVsuVrhlnI84gOQCQmiEdc4RYYFQJ4WVDLxn3LiWWm7aUAOHxtZcCeHqwA1T3vKmIWyO7qbeIcWvg8-j3sZD6stLTako0wCX_1GgFJEN5ZwWCiaqTTHn5IMeUrc36aiB6JNKPanUxZA-qdTHkqFTJhe2X_v0q_nP0Ddje3Xk</recordid><startdate>20170201</startdate><enddate>20170201</enddate><creator>Xiao, Guijian</creator><creator>Huang, Yun</creator><creator>Yin, Jiachao</creator><general>Springer London</general><general>Springer Nature B.V</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>PRINS</scope><scope>PTHSS</scope></search><sort><creationdate>20170201</creationdate><title>An integrated polishing method for compressor blade surfaces</title><author>Xiao, Guijian ; Huang, Yun ; Yin, Jiachao</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c344t-f17461ff96bddd06b102d76b731ee34adc2b4acf51419b54866d5f4a38eb49903</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2017</creationdate><topic>Aerospace engines</topic><topic>Aircraft engines</topic><topic>Belts</topic><topic>CAE) and Design</topic><topic>Compressor blades</topic><topic>Computer-Aided Engineering (CAD</topic><topic>Design specifications</topic><topic>Engineering</topic><topic>Gas turbine engines</topic><topic>Industrial and Production Engineering</topic><topic>Mechanical Engineering</topic><topic>Media Management</topic><topic>Original Article</topic><topic>Polishes</topic><topic>Polishing</topic><topic>Rapid prototyping</topic><topic>Surface properties</topic><topic>Surface roughness</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Xiao, Guijian</creatorcontrib><creatorcontrib>Huang, Yun</creatorcontrib><creatorcontrib>Yin, Jiachao</creatorcontrib><collection>CrossRef</collection><collection>ProQuest SciTech Collection</collection><collection>ProQuest Technology Collection</collection><collection>Materials Science & Engineering Collection</collection><collection>ProQuest Central UK/Ireland</collection><collection>ProQuest Central</collection><collection>Technology Collection</collection><collection>ProQuest One Community College</collection><collection>ProQuest Central Korea</collection><collection>SciTech Premium Collection</collection><collection>ProQuest Engineering Collection</collection><collection>Engineering Database</collection><collection>ProQuest One Academic Eastern Edition (DO NOT USE)</collection><collection>ProQuest One Academic</collection><collection>ProQuest One Academic UKI Edition</collection><collection>ProQuest Central China</collection><collection>Engineering Collection</collection><jtitle>International journal of advanced manufacturing technology</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Xiao, Guijian</au><au>Huang, Yun</au><au>Yin, Jiachao</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>An integrated polishing method for compressor blade surfaces</atitle><jtitle>International journal of advanced manufacturing technology</jtitle><stitle>Int J Adv Manuf Technol</stitle><date>2017-02-01</date><risdate>2017</risdate><volume>88</volume><issue>5-8</issue><spage>1723</spage><epage>1733</epage><pages>1723-1733</pages><issn>0268-3768</issn><eissn>1433-3015</eissn><abstract>The surface quality and profile precision of compressor blades affect the performance and security of aircraft engines. Components with complex design specifications are difficult to manufacture, especially when polishing processes are needed to enable compliance with tight industrial standards. Belt polishing and bob polishing are commonly used in the precision manufacturing of components of gas turbine engines for aerospace and energy applications. These methods are used to polish different parts of the compressor blade. Information on integrated methods with belt polishing and bob polishing processes for full-area compressor blade (FACB) surfaces is scarce. In the present study, an integrated polishing method that combines bob polishing and seven-axis linkage belt polishing was used to improve the surface quality and profile precision of a FACB surface. The surfaces of three compressor blades were analyzed after polishing with each individual method and the integrated method. The surface roughness was less than 0.35 μm; the profile precision was higher than 0.05 mm; and the precision consistency was substantially improved. This proves that this polishing method, which integrates belt and bob polishing, can be used for automated polishing of compressor blade surfaces.</abstract><cop>London</cop><pub>Springer London</pub><doi>10.1007/s00170-016-8891-y</doi><tpages>11</tpages></addata></record> |
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| ispartof | International journal of advanced manufacturing technology, 2017-02, Vol.88 (5-8), p.1723-1733 |
| issn | 0268-3768 1433-3015 |
| language | eng |
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| source | Springer Nature - Complete Springer Journals |
| subjects | Aerospace engines Aircraft engines Belts CAE) and Design Compressor blades Computer-Aided Engineering (CAD Design specifications Engineering Gas turbine engines Industrial and Production Engineering Mechanical Engineering Media Management Original Article Polishes Polishing Rapid prototyping Surface properties Surface roughness |
| title | An integrated polishing method for compressor blade surfaces |
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