estrutura da zona de introdução de carga na extremidade traseira de uma aeronave

Load introduction zone in the rear end of an aircraft comprising receiving elements (3, 4) of the loads of the horizontal and vertical tail stabilizers connected to structural elements (2, 8, 9) wherein: a) said structural elements are the cladding (8), two contiguous load-bearing frames (2) with a...

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Hauptverfasser:	ELENA ARÉVALO RODRÍGUEZ, FRANCISCO JOSÉ CRUZ DOMÍNGUEZ, MANUEL ARIZA MARTÍN
Format:	Patent
Sprache:	por
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
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creator	ELENA ARÉVALO RODRÍGUEZ FRANCISCO JOSÉ CRUZ DOMÍNGUEZ MANUEL ARIZA MARTÍN
description	Load introduction zone in the rear end of an aircraft comprising receiving elements (3, 4) of the loads of the horizontal and vertical tail stabilizers connected to structural elements (2, 8, 9) wherein: a) said structural elements are the cladding (8), two contiguous load-bearing frames (2) with a or omega cross-section and, at least, a third frame (9); b) the receiving element of the horizontal tail stabilizer load is a first fitting (3) structured as a torque box, transversely arranged between said load-bearing frames (2) and connected to them, and the receiving elements of the vertical tail stabilizer loads are some second fittings (4) coupled to these frames (2, 9); c) said frames (2, 9) and said first and second fittings (3, 4) are entirely made of composite material.
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FRANCISCO JOSÉ CRUZ DOMÍNGUEZ ; MANUEL ARIZA MARTÍN</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_BRPI0923172A23</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>por</language><creationdate>2016</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>HELICOPTERS</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>ELENA ARÉVALO RODRÍGUEZ</creatorcontrib><creatorcontrib>FRANCISCO JOSÉ CRUZ DOMÍNGUEZ</creatorcontrib><creatorcontrib>MANUEL ARIZA MARTÍN</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>ELENA ARÉVALO RODRÍGUEZ</au><au>FRANCISCO JOSÉ CRUZ DOMÍNGUEZ</au><au>MANUEL ARIZA MARTÍN</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>estrutura da zona de introdução de carga na extremidade traseira de uma aeronave</title><date>2016-02-16</date><risdate>2016</risdate><abstract>Load introduction zone in the rear end of an aircraft comprising receiving elements (3, 4) of the loads of the horizontal and vertical tail stabilizers connected to structural elements (2, 8, 9) wherein: a) said structural elements are the cladding (8), two contiguous load-bearing frames (2) with a or omega cross-section and, at least, a third frame (9); 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subjects	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
title	estrutura da zona de introdução de carga na extremidade traseira de uma aeronave
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