A REAR END SECTION FOR AN AIRCRAFT
The invention refers to a rear end section (1) for an aircraft, having a fuselage (4), a v-tail (2), and a thruster assembly (3) comprising: at least one propulsion device (5) installed to ingest and consume air forming a fuselage boundary layer, a control surface (6) attached at the rearmost sectio...
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creator | LLAMAS SANDIN, Raul Carlos |
description | The invention refers to a rear end section (1) for an aircraft, having a fuselage (4), a v-tail (2), and a thruster assembly (3) comprising: at least one propulsion device (5) installed to ingest and consume air forming a fuselage boundary layer, a control surface (6) attached at the rearmost section of the rear end, and a casing (7) covering at least part of the propulsion device (5) such that an air inlet (8) and an air outlet (9) are defined between the casing (7) and the propulsion device (5), the air inlet (8) being designed for the passage of the fuselage boundary layer towards the propulsion device (5), and the air outlet (9) being designed for directing the airflow exhausted from the propulsion device (5) into the control surface (6), to divert said airflow and provide vectoring thrust for the aircraft. |
format | Patent |
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fre ; ger</language><creationdate>2023</creationdate><topic>AEROPLANES</topic><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>HELICOPTERS</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>LLAMAS SANDIN, Raul Carlos</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>LLAMAS SANDIN, Raul Carlos</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>A REAR END SECTION FOR AN AIRCRAFT</title><date>2023-06-07</date><risdate>2023</risdate><abstract>The invention refers to a rear end section (1) for an aircraft, having a fuselage (4), a v-tail (2), and a thruster assembly (3) comprising: at least one propulsion device (5) installed to ingest and consume air forming a fuselage boundary layer, a control surface (6) attached at the rearmost section of the rear end, and a casing (7) covering at least part of the propulsion device (5) such that an air inlet (8) and an air outlet (9) are defined between the casing (7) and the propulsion device (5), the air inlet (8) being designed for the passage of the fuselage boundary layer towards the propulsion device (5), and the air outlet (9) being designed for directing the airflow exhausted from the propulsion device (5) into the control surface (6), to divert said airflow and provide vectoring thrust for the aircraft.</abstract><oa>free_for_read</oa></addata></record> |
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language | eng ; fre ; ger |
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subjects | AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HELICOPTERS PARACHUTES PERFORMING OPERATIONS TRANSPORTING |
title | A REAR END SECTION FOR AN AIRCRAFT |
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