Skin panel of composite material having an internal grid

A skin panel configured for attachment to an aircraft structure is constructed of a composite material and has a continuous, smooth outer surface; a continuous, smooth inner surface that is configured for attachment to an aircraft structure; a peripheral edge that extends entirely around the skin pa...

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Hauptverfasser:	Santini, Gregory M, Stickler, Patrick B, Oakes, Gary D, Walker, Steven P
Format:	Patent
Sprache:	eng
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS LAYERED PRODUCTS LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM PERFORMING OPERATIONS TRANSPORTING
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creator	Santini, Gregory M Stickler, Patrick B Oakes, Gary D Walker, Steven P
description	A skin panel configured for attachment to an aircraft structure is constructed of a composite material and has a continuous, smooth outer surface; a continuous, smooth inner surface that is configured for attachment to an aircraft structure; a peripheral edge that extends entirely around the skin panel and has a continuous, smooth surface and a plurality of cavities inside the material of the skin panel. The cavities reduce the weight of the skin panel without significantly detracting from the compression strength and tensile strength of the skin panel.
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The cavities reduce the weight of the skin panel without significantly detracting from the compression strength and tensile strength of the skin panel.</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>HELICOPTERS</subject><subject>LAYERED PRODUCTS</subject><subject>LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2022</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZLAIzs7MUyhIzEvNUchPU0jOzy3IL84sSVXITSxJLcpMzFHISCzLzEtXSMxTyMwDCuUBhdKLMlN4GFjTEnOKU3mhNDeDoptriLOHbmpBfnxqcUFicmpeakl8aLChoamhoYWJuZORMTFqAO_kLjY</recordid><startdate>20221129</startdate><enddate>20221129</enddate><creator>Santini, Gregory M</creator><creator>Stickler, Patrick B</creator><creator>Oakes, Gary D</creator><creator>Walker, Steven P</creator><scope>EVB</scope></search><sort><creationdate>20221129</creationdate><title>Skin panel of composite material having an internal grid</title><author>Santini, Gregory M ; Stickler, Patrick B ; Oakes, Gary D ; Walker, Steven P</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US11511847B23</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2022</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>HELICOPTERS</topic><topic>LAYERED PRODUCTS</topic><topic>LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>Santini, Gregory M</creatorcontrib><creatorcontrib>Stickler, Patrick B</creatorcontrib><creatorcontrib>Oakes, Gary D</creatorcontrib><creatorcontrib>Walker, Steven P</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Santini, Gregory M</au><au>Stickler, Patrick B</au><au>Oakes, Gary D</au><au>Walker, Steven P</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Skin panel of composite material having an internal grid</title><date>2022-11-29</date><risdate>2022</risdate><abstract>A skin panel configured for attachment to an aircraft structure is constructed of a composite material and has a continuous, smooth outer surface; a continuous, smooth inner surface that is configured for attachment to an aircraft structure; a peripheral edge that extends entirely around the skin panel and has a continuous, smooth surface and a plurality of cavities inside the material of the skin panel. 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subjects	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS LAYERED PRODUCTS LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM PERFORMING OPERATIONS TRANSPORTING
title	Skin panel of composite material having an internal grid
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