DELTA FUSELAGE FOR VERTICAL TAKE-OFF AND LANDING (VTOL) AIRCRAFT
A vertical take-off and landing (VTOL) aircraft is provided. The aircraft includes a wing, nacelles supportively disposed at opposite ends of the wing, proprotors respectively attached to each of the nacelles with each of the proprotors being rotatable to generate lift in vertical flight and thrust...
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creator | Alber Mark R Gayagoy Charles |
description | A vertical take-off and landing (VTOL) aircraft is provided. The aircraft includes a wing, nacelles supportively disposed at opposite ends of the wing, proprotors respectively attached to each of the nacelles with each of the proprotors being rotatable to generate lift in vertical flight and thrust in horizontal flight and a delta-wing shaped fuselage disposed along the wing between the nacelles. |
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The aircraft includes a wing, nacelles supportively disposed at opposite ends of the wing, proprotors respectively attached to each of the nacelles with each of the proprotors being rotatable to generate lift in vertical flight and thrust in horizontal flight and a delta-wing shaped fuselage disposed along the wing between the nacelles.</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>HELICOPTERS</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2017</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZHBwcfUJcVRwCw129XF0d1Vw8w9SCHMNCvF0dvRRCHH0dtX1d3NTcPRzUfABEp5-7goaYSH-PpoKjp5BzkGObiE8DKxpiTnFqbxQmptB2c01xNlDN7UgPz61uCAxOTUvtSQ-NNjIwNDc2NjE1NTc0dCYOFUACbUq-w</recordid><startdate>20171123</startdate><enddate>20171123</enddate><creator>Alber Mark R</creator><creator>Gayagoy Charles</creator><scope>EVB</scope></search><sort><creationdate>20171123</creationdate><title>DELTA FUSELAGE FOR VERTICAL TAKE-OFF AND LANDING (VTOL) AIRCRAFT</title><author>Alber Mark R ; Gayagoy Charles</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US2017334557A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2017</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>Alber Mark R</creatorcontrib><creatorcontrib>Gayagoy Charles</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Alber Mark R</au><au>Gayagoy Charles</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>DELTA FUSELAGE FOR VERTICAL TAKE-OFF AND LANDING (VTOL) AIRCRAFT</title><date>2017-11-23</date><risdate>2017</risdate><abstract>A vertical take-off and landing (VTOL) aircraft is provided. The aircraft includes a wing, nacelles supportively disposed at opposite ends of the wing, proprotors respectively attached to each of the nacelles with each of the proprotors being rotatable to generate lift in vertical flight and thrust in horizontal flight and a delta-wing shaped fuselage disposed along the wing between the nacelles.</abstract><oa>free_for_read</oa></addata></record> |
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subjects | AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING |
title | DELTA FUSELAGE FOR VERTICAL TAKE-OFF AND LANDING (VTOL) AIRCRAFT |
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