Procedimiento para diseñar bordes de ataque y estructura sustentadora provista de dicho borde
La invención concierne un procedimiento de fabricación o diseño de un borde de ataque de una estructura sustentadora donde, comenzando en el punto medio de la base (0,0), se aplica una curva al perfil de la estructura, cuya longitud "Li" es función del grosor máximo de la sección NACA en l...
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creator | DIEZ DIEZ, Guzmán GABINA IRIBAR, Gorka |
description | La invención concierne un procedimiento de fabricación o diseño de un borde de ataque de una estructura sustentadora donde, comenzando en el punto medio de la base (0,0), se aplica una curva al perfil de la estructura, cuya longitud "Li" es función del grosor máximo de la sección NACA en la base del perfil "Ho" en la base y viene definida por la ecuación L1 = 0,051 OHo2 - 0,0790Ho + 15,5790, y cuya cota máxima en el eje "x" se sitúa en el punto "L1/2" y se define mediante la relación x = 0.0137(L1)1 4944, estando la forma de dicha curva definida mediante la ecuación: (y- yo) = 0.0000000107x6 + 0.0000016382x5 - 0.0000794412x4 + 0.0010194142x3 + 0.0097205322x2 + 0.0136993913x y calculando el resto de la curva mediante un proceso iterativo según lo anteriormente indicado.
The invention relates to a method for producing or designing a leading edge of a lifting structure, wherein starting at the midpoint of the base (0,0), a curve is applied to the profile of the structure, the length "L 1 " of which is according to the maximum thickness of the NACA section in the base of the profile "Ho" in the base and is defined by the equation L 1 = 0.0510H 0 2 - 0.0790H 0 + 15.5790, and the maximum height of which on the "x"-axis is located at point "L 1 /2" and defined by means of the relationship x = 0.0137(L 1 ) 1.4944 , the shape of said curve being defined by means of the equation: (y-yo) = 0.0000000107x 6 + 0.0000016382x 5 - 0.0000794412x 4 + 0.0010194142x 3 + 0.0097205322x 2 + 0.0136993913x, and the rest of the curve being calculated by means of an iterative process according to the above. |
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fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_ES2906635TT3</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>ES2906635TT3</sourcerecordid><originalsourceid>FETCH-epo_espacenet_ES2906635TT33</originalsourceid><addsrcrecordid>eNqNy8EJAjEQheFcPIjaw1iAIAYXPMuKR8GcXcZkxIDuxMxEsCxrsDEjWoCnx4PvH5rDLrOnEK-RemVImBFCFHo9McORcyCBQICKt0LwABLNxWupTIpojTBwPSnzPYriB4foz_yNx2ZwwovQ5LcjM920br2dUeKOJKGnnrRr94vVvGns0jlr_zFv8MQ-LA</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Procedimiento para diseñar bordes de ataque y estructura sustentadora provista de dicho borde</title><source>esp@cenet</source><creator>DIEZ DIEZ, Guzmán ; GABINA IRIBAR, Gorka</creator><creatorcontrib>DIEZ DIEZ, Guzmán ; GABINA IRIBAR, Gorka</creatorcontrib><description>La invención concierne un procedimiento de fabricación o diseño de un borde de ataque de una estructura sustentadora donde, comenzando en el punto medio de la base (0,0), se aplica una curva al perfil de la estructura, cuya longitud "Li" es función del grosor máximo de la sección NACA en la base del perfil "Ho" en la base y viene definida por la ecuación L1 = 0,051 OHo2 - 0,0790Ho + 15,5790, y cuya cota máxima en el eje "x" se sitúa en el punto "L1/2" y se define mediante la relación x = 0.0137(L1)1 4944, estando la forma de dicha curva definida mediante la ecuación: (y- yo) = 0.0000000107x6 + 0.0000016382x5 - 0.0000794412x4 + 0.0010194142x3 + 0.0097205322x2 + 0.0136993913x y calculando el resto de la curva mediante un proceso iterativo según lo anteriormente indicado.
The invention relates to a method for producing or designing a leading edge of a lifting structure, wherein starting at the midpoint of the base (0,0), a curve is applied to the profile of the structure, the length "L 1 " of which is according to the maximum thickness of the NACA section in the base of the profile "Ho" in the base and is defined by the equation L 1 = 0.0510H 0 2 - 0.0790H 0 + 15.5790, and the maximum height of which on the "x"-axis is located at point "L 1 /2" and defined by means of the relationship x = 0.0137(L 1 ) 1.4944 , the shape of said curve being defined by means of the equation: (y-yo) = 0.0000000107x 6 + 0.0000016382x 5 - 0.0000794412x 4 + 0.0010194142x 3 + 0.0097205322x 2 + 0.0136993913x, and the rest of the curve being calculated by means of an iterative process according to the above.</description><language>spa</language><subject>BLASTING ; EQUIPMENT FOR SHIPPING ; HEATING ; LIGHTING ; MACHINES OR ENGINES FOR LIQUIDS ; MECHANICAL ENGINEERING ; OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR ; PERFORMING OPERATIONS ; PRODUCING MECHANICAL POWER ; RELATED EQUIPMENT ; SHIPS OR OTHER WATERBORNE VESSELS ; TRANSPORTING ; WEAPONS ; WIND MOTORS ; WIND, SPRING WEIGHT AND MISCELLANEOUS MOTORS</subject><creationdate>2022</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20220419&DB=EPODOC&CC=ES&NR=2906635T3$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20220419&DB=EPODOC&CC=ES&NR=2906635T3$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>DIEZ DIEZ, Guzmán</creatorcontrib><creatorcontrib>GABINA IRIBAR, Gorka</creatorcontrib><title>Procedimiento para diseñar bordes de ataque y estructura sustentadora provista de dicho borde</title><description>La invención concierne un procedimiento de fabricación o diseño de un borde de ataque de una estructura sustentadora donde, comenzando en el punto medio de la base (0,0), se aplica una curva al perfil de la estructura, cuya longitud "Li" es función del grosor máximo de la sección NACA en la base del perfil "Ho" en la base y viene definida por la ecuación L1 = 0,051 OHo2 - 0,0790Ho + 15,5790, y cuya cota máxima en el eje "x" se sitúa en el punto "L1/2" y se define mediante la relación x = 0.0137(L1)1 4944, estando la forma de dicha curva definida mediante la ecuación: (y- yo) = 0.0000000107x6 + 0.0000016382x5 - 0.0000794412x4 + 0.0010194142x3 + 0.0097205322x2 + 0.0136993913x y calculando el resto de la curva mediante un proceso iterativo según lo anteriormente indicado.
The invention relates to a method for producing or designing a leading edge of a lifting structure, wherein starting at the midpoint of the base (0,0), a curve is applied to the profile of the structure, the length "L 1 " of which is according to the maximum thickness of the NACA section in the base of the profile "Ho" in the base and is defined by the equation L 1 = 0.0510H 0 2 - 0.0790H 0 + 15.5790, and the maximum height of which on the "x"-axis is located at point "L 1 /2" and defined by means of the relationship x = 0.0137(L 1 ) 1.4944 , the shape of said curve being defined by means of the equation: (y-yo) = 0.0000000107x 6 + 0.0000016382x 5 - 0.0000794412x 4 + 0.0010194142x 3 + 0.0097205322x 2 + 0.0136993913x, and the rest of the curve being calculated by means of an iterative process according to the above.</description><subject>BLASTING</subject><subject>EQUIPMENT FOR SHIPPING</subject><subject>HEATING</subject><subject>LIGHTING</subject><subject>MACHINES OR ENGINES FOR LIQUIDS</subject><subject>MECHANICAL ENGINEERING</subject><subject>OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR</subject><subject>PERFORMING OPERATIONS</subject><subject>PRODUCING MECHANICAL POWER</subject><subject>RELATED EQUIPMENT</subject><subject>SHIPS OR OTHER WATERBORNE VESSELS</subject><subject>TRANSPORTING</subject><subject>WEAPONS</subject><subject>WIND MOTORS</subject><subject>WIND, SPRING WEIGHT AND MISCELLANEOUS MOTORS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2022</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNy8EJAjEQheFcPIjaw1iAIAYXPMuKR8GcXcZkxIDuxMxEsCxrsDEjWoCnx4PvH5rDLrOnEK-RemVImBFCFHo9McORcyCBQICKt0LwABLNxWupTIpojTBwPSnzPYriB4foz_yNx2ZwwovQ5LcjM920br2dUeKOJKGnnrRr94vVvGns0jlr_zFv8MQ-LA</recordid><startdate>20220419</startdate><enddate>20220419</enddate><creator>DIEZ DIEZ, Guzmán</creator><creator>GABINA IRIBAR, Gorka</creator><scope>EVB</scope></search><sort><creationdate>20220419</creationdate><title>Procedimiento para diseñar bordes de ataque y estructura sustentadora provista de dicho borde</title><author>DIEZ DIEZ, Guzmán ; GABINA IRIBAR, Gorka</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_ES2906635TT33</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>spa</language><creationdate>2022</creationdate><topic>BLASTING</topic><topic>EQUIPMENT FOR SHIPPING</topic><topic>HEATING</topic><topic>LIGHTING</topic><topic>MACHINES OR ENGINES FOR LIQUIDS</topic><topic>MECHANICAL ENGINEERING</topic><topic>OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR</topic><topic>PERFORMING OPERATIONS</topic><topic>PRODUCING MECHANICAL POWER</topic><topic>RELATED EQUIPMENT</topic><topic>SHIPS OR OTHER WATERBORNE VESSELS</topic><topic>TRANSPORTING</topic><topic>WEAPONS</topic><topic>WIND MOTORS</topic><topic>WIND, SPRING WEIGHT AND MISCELLANEOUS MOTORS</topic><toplevel>online_resources</toplevel><creatorcontrib>DIEZ DIEZ, Guzmán</creatorcontrib><creatorcontrib>GABINA IRIBAR, Gorka</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>DIEZ DIEZ, Guzmán</au><au>GABINA IRIBAR, Gorka</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Procedimiento para diseñar bordes de ataque y estructura sustentadora provista de dicho borde</title><date>2022-04-19</date><risdate>2022</risdate><abstract>La invención concierne un procedimiento de fabricación o diseño de un borde de ataque de una estructura sustentadora donde, comenzando en el punto medio de la base (0,0), se aplica una curva al perfil de la estructura, cuya longitud "Li" es función del grosor máximo de la sección NACA en la base del perfil "Ho" en la base y viene definida por la ecuación L1 = 0,051 OHo2 - 0,0790Ho + 15,5790, y cuya cota máxima en el eje "x" se sitúa en el punto "L1/2" y se define mediante la relación x = 0.0137(L1)1 4944, estando la forma de dicha curva definida mediante la ecuación: (y- yo) = 0.0000000107x6 + 0.0000016382x5 - 0.0000794412x4 + 0.0010194142x3 + 0.0097205322x2 + 0.0136993913x y calculando el resto de la curva mediante un proceso iterativo según lo anteriormente indicado.
The invention relates to a method for producing or designing a leading edge of a lifting structure, wherein starting at the midpoint of the base (0,0), a curve is applied to the profile of the structure, the length "L 1 " of which is according to the maximum thickness of the NACA section in the base of the profile "Ho" in the base and is defined by the equation L 1 = 0.0510H 0 2 - 0.0790H 0 + 15.5790, and the maximum height of which on the "x"-axis is located at point "L 1 /2" and defined by means of the relationship x = 0.0137(L 1 ) 1.4944 , the shape of said curve being defined by means of the equation: (y-yo) = 0.0000000107x 6 + 0.0000016382x 5 - 0.0000794412x 4 + 0.0010194142x 3 + 0.0097205322x 2 + 0.0136993913x, and the rest of the curve being calculated by means of an iterative process according to the above.</abstract><oa>free_for_read</oa></addata></record> |
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subjects | BLASTING EQUIPMENT FOR SHIPPING HEATING LIGHTING MACHINES OR ENGINES FOR LIQUIDS MECHANICAL ENGINEERING OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR PERFORMING OPERATIONS PRODUCING MECHANICAL POWER RELATED EQUIPMENT SHIPS OR OTHER WATERBORNE VESSELS TRANSPORTING WEAPONS WIND MOTORS WIND, SPRING WEIGHT AND MISCELLANEOUS MOTORS |
title | Procedimiento para diseñar bordes de ataque y estructura sustentadora provista de dicho borde |
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