IMPLIFIED METHOD FOR PARAMETRIC SURFACE GENERATION, FOR DESIGNING THE EXTERNAL GEOMETRY OF AN AIRCRAFT AIRFOIL
The present disclosure belongs to the field of configuring the shape or geometry of an aircraft airfoil (1.1 - 1.7). In particular, the present invention provides a method to design the external geometry of an aircraft airfoil.
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creator | LLAMAS SANDIN, Raúl Carlos BAILEY NOVAL, Nicolás |
description | The present disclosure belongs to the field of configuring the shape or geometry of an aircraft airfoil (1.1 - 1.7). In particular, the present invention provides a method to design the external geometry of an aircraft airfoil. |
format | Patent |
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In particular, the present invention provides a method to design the external geometry of an aircraft airfoil.</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>CALCULATING</subject><subject>COMPUTING</subject><subject>COSMONAUTICS</subject><subject>COUNTING</subject><subject>ELECTRIC DIGITAL DATA PROCESSING</subject><subject>HELICOPTERS</subject><subject>PERFORMING OPERATIONS</subject><subject>PHYSICS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2023</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNy8EKgkAQBmAvHaJ6h3mAOkhBeRzWmXVAd2VcoU4isZ3CBHt_0ugBOv3_D9-_Tgap6lJYKIeKQuFzYK9Qo-I8VQw0rTIaAkuOFIN4t_-SnBqxTpyFUBDQNZA6LGfml-MNPAM6QFGjyGEp7KXcJqtH_5zi7pebBJiCKQ5xfHVxGvt7HOK7o_qUZpdzlmF6_IN8AN_vNsQ</recordid><startdate>20230621</startdate><enddate>20230621</enddate><creator>LLAMAS SANDIN, Raúl Carlos</creator><creator>BAILEY NOVAL, Nicolás</creator><scope>EVB</scope></search><sort><creationdate>20230621</creationdate><title>IMPLIFIED METHOD FOR PARAMETRIC SURFACE GENERATION, FOR DESIGNING THE EXTERNAL GEOMETRY OF AN AIRCRAFT AIRFOIL</title><author>LLAMAS SANDIN, Raúl Carlos ; BAILEY NOVAL, Nicolás</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP4198799A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2023</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>CALCULATING</topic><topic>COMPUTING</topic><topic>COSMONAUTICS</topic><topic>COUNTING</topic><topic>ELECTRIC DIGITAL DATA PROCESSING</topic><topic>HELICOPTERS</topic><topic>PERFORMING OPERATIONS</topic><topic>PHYSICS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>LLAMAS SANDIN, Raúl Carlos</creatorcontrib><creatorcontrib>BAILEY NOVAL, Nicolás</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>LLAMAS SANDIN, Raúl Carlos</au><au>BAILEY NOVAL, Nicolás</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>IMPLIFIED METHOD FOR PARAMETRIC SURFACE GENERATION, FOR DESIGNING THE EXTERNAL GEOMETRY OF AN AIRCRAFT AIRFOIL</title><date>2023-06-21</date><risdate>2023</risdate><abstract>The present disclosure belongs to the field of configuring the shape or geometry of an aircraft airfoil (1.1 - 1.7). 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language | eng ; fre ; ger |
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subjects | AEROPLANES AIRCRAFT AVIATION CALCULATING COMPUTING COSMONAUTICS COUNTING ELECTRIC DIGITAL DATA PROCESSING HELICOPTERS PERFORMING OPERATIONS PHYSICS TRANSPORTING |
title | IMPLIFIED METHOD FOR PARAMETRIC SURFACE GENERATION, FOR DESIGNING THE EXTERNAL GEOMETRY OF AN AIRCRAFT AIRFOIL |
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