aparelho de voo camuflado

APARELHO DE VOO CAMUFLADO. A presente invenção refere-se a um aparelho de voo (10) com assinatura de radar pequena apresenta um primeiro lado (12), sobre o qual estão dispostos a abertura de turbina (14,16) e compartimentos de carga útil ou de mecanismo de rolamento (20,24,26). Um segundo lado (30)...

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Hauptverfasser: JOCHEN DORNWALD, BARTHOLOMAEUS BICHLER
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creator JOCHEN DORNWALD
BARTHOLOMAEUS BICHLER
description APARELHO DE VOO CAMUFLADO. A presente invenção refere-se a um aparelho de voo (10) com assinatura de radar pequena apresenta um primeiro lado (12), sobre o qual estão dispostos a abertura de turbina (14,16) e compartimentos de carga útil ou de mecanismo de rolamento (20,24,26). Um segundo lado (30) do aparelho de voo está realizado de tal modo que ele apresenta uma assinatura de radar menor do que o primeiro lado (12). The aircraft (10) has a turbine (18) that is provided with apertures (14,16). The aircraft components are moved inside an aircraft main portion by a payload shaft (20) and landing gear shafts (24,26). The turbine apertures and the shafts are arranged on a top surface (12) of the aircraft main portion. The radar signature of a bottom surface (30) of the aircraft main portion is set smaller than the radar signature of the top surface of the aircraft main portion. The bottom surface is provided with an uninterrupted surface. An independent claim is included for a method for operating aircraft.
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A presente invenção refere-se a um aparelho de voo (10) com assinatura de radar pequena apresenta um primeiro lado (12), sobre o qual estão dispostos a abertura de turbina (14,16) e compartimentos de carga útil ou de mecanismo de rolamento (20,24,26). Um segundo lado (30) do aparelho de voo está realizado de tal modo que ele apresenta uma assinatura de radar menor do que o primeiro lado (12). The aircraft (10) has a turbine (18) that is provided with apertures (14,16). The aircraft components are moved inside an aircraft main portion by a payload shaft (20) and landing gear shafts (24,26). The turbine apertures and the shafts are arranged on a top surface (12) of the aircraft main portion. The radar signature of a bottom surface (30) of the aircraft main portion is set smaller than the radar signature of the top surface of the aircraft main portion. The bottom surface is provided with an uninterrupted surface. An independent claim is included for a method for operating aircraft.</description><language>por</language><subject>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</subject><creationdate>2013</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20130702&amp;DB=EPODOC&amp;CC=BR&amp;NR=102012013764A2$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,778,883,25551,76302</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20130702&amp;DB=EPODOC&amp;CC=BR&amp;NR=102012013764A2$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>JOCHEN DORNWALD</creatorcontrib><creatorcontrib>BARTHOLOMAEUS BICHLER</creatorcontrib><title>aparelho de voo camuflado</title><description>APARELHO DE VOO CAMUFLADO. A presente invenção refere-se a um aparelho de voo (10) com assinatura de radar pequena apresenta um primeiro lado (12), sobre o qual estão dispostos a abertura de turbina (14,16) e compartimentos de carga útil ou de mecanismo de rolamento (20,24,26). Um segundo lado (30) do aparelho de voo está realizado de tal modo que ele apresenta uma assinatura de radar menor do que o primeiro lado (12). The aircraft (10) has a turbine (18) that is provided with apertures (14,16). The aircraft components are moved inside an aircraft main portion by a payload shaft (20) and landing gear shafts (24,26). The turbine apertures and the shafts are arranged on a top surface (12) of the aircraft main portion. The radar signature of a bottom surface (30) of the aircraft main portion is set smaller than the radar signature of the top surface of the aircraft main portion. The bottom surface is provided with an uninterrupted surface. 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A presente invenção refere-se a um aparelho de voo (10) com assinatura de radar pequena apresenta um primeiro lado (12), sobre o qual estão dispostos a abertura de turbina (14,16) e compartimentos de carga útil ou de mecanismo de rolamento (20,24,26). Um segundo lado (30) do aparelho de voo está realizado de tal modo que ele apresenta uma assinatura de radar menor do que o primeiro lado (12). The aircraft (10) has a turbine (18) that is provided with apertures (14,16). The aircraft components are moved inside an aircraft main portion by a payload shaft (20) and landing gear shafts (24,26). The turbine apertures and the shafts are arranged on a top surface (12) of the aircraft main portion. The radar signature of a bottom surface (30) of the aircraft main portion is set smaller than the radar signature of the top surface of the aircraft main portion. The bottom surface is provided with an uninterrupted surface. An independent claim is included for a method for operating aircraft.</abstract><oa>free_for_read</oa></addata></record>
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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 aparelho de voo camuflado
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