dispositivo de suspensão de um turborreator
A turbojet is suspended by attachments including hinged links. An attachment includes a support including three branches with passages through which a pin passes, the pin being oriented generally parallel to a direction that is tangential to a casing and being hinged to a central branch of the suppo...
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creator | WOUTER BALK THOMAS ALAIN CHRISTIAN VINCENT |
description | A turbojet is suspended by attachments including hinged links. An attachment includes a support including three branches with passages through which a pin passes, the pin being oriented generally parallel to a direction that is tangential to a casing and being hinged to a central branch of the support by a ball joint. |
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An attachment includes a support including three branches with passages through which a pin passes, the pin being oriented generally parallel to a direction that is tangential to a casing and being hinged to a central branch of the support by a ball joint.</description><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2016</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZNBJySwuyC_OLMksy1dISVUoLi0uSM0rPrwYzCvNVSgpLUrKLypKTSzJL-JhYE1LzClO5YXS3Ayqbq4hzh66qQX58anFBYnJqXmpJfFOQYaGRgaGxgaGpoaWZo5GxsSqAwBo1yyD</recordid><startdate>20160913</startdate><enddate>20160913</enddate><creator>WOUTER BALK</creator><creator>THOMAS ALAIN CHRISTIAN VINCENT</creator><scope>EVB</scope></search><sort><creationdate>20160913</creationdate><title>dispositivo de suspensão de um turborreator</title><author>WOUTER BALK ; THOMAS ALAIN CHRISTIAN VINCENT</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_BR112013015196A23</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>por</language><creationdate>2016</creationdate><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>WOUTER BALK</creatorcontrib><creatorcontrib>THOMAS ALAIN CHRISTIAN VINCENT</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>WOUTER BALK</au><au>THOMAS ALAIN CHRISTIAN VINCENT</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>dispositivo de suspensão de um turborreator</title><date>2016-09-13</date><risdate>2016</risdate><abstract>A turbojet is suspended by attachments including hinged links. 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subjects | AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS TRANSPORTING |
title | dispositivo de suspensão de um turborreator |
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