sistema de sensor acústico para uma aeronave, método para controlar a diretividade de sinais acústicos de um sistema de sensor acústico, e, protetor de eco fixo
sistema de sensor acústico para uma aeronave, método para controlar a diretividade de sinais acústicos de um sistema de sensor acústico, e, protetor de eco fixo um sistema de sensor acústico para uma aeronave inclui um transmissor configurado para emitir sinais acústicos externos à aeronave, e pelo...
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| creator | JAIME SLY JOSHUA BOELMAN |
| description | sistema de sensor acústico para uma aeronave, método para controlar a diretividade de sinais acústicos de um sistema de sensor acústico, e, protetor de eco fixo um sistema de sensor acústico para uma aeronave inclui um transmissor configurado para emitir sinais acústicos externos à aeronave, e pelo menos um microfone posicionado num exterior da aeronave e configurado para captar os sinais acústicos como dados captados. o sistema de sensor acústico é configurado para dirigir os sinais acústicos para o pelo menos um microfone de modo que um nível de pressão sonora seja atenuado perpendicular à aeronave.
An acoustic sensor system (10) for an aircraft (52) includes a transmitter (12) configured to emit acoustic signals external to the aircraft (52), and at least one microphone (14a-14n) positioned on an exterior of the aircraft (52) and configured to sense the acoustic signals as sensed data. The acoustic sensor system (10) is configured to direct the acoustic signals to the at least one microphone (14a-14n) such that a sound pressure level is attenuated perpendicular to the aircraft (52). |
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An acoustic sensor system (10) for an aircraft (52) includes a transmitter (12) configured to emit acoustic signals external to the aircraft (52), and at least one microphone (14a-14n) positioned on an exterior of the aircraft (52) and configured to sense the acoustic signals as sensed data. The acoustic sensor system (10) is configured to direct the acoustic signals to the at least one microphone (14a-14n) such that a sound pressure level is attenuated perpendicular to the aircraft (52).</description><language>por</language><subject>AIRCRAFT ; ANALOGOUS ARRANGEMENTS USING OTHER WAVES ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; COSMONAUTICS ; DEAF-AID SETS ; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES ; ELECTRIC COMMUNICATION TECHNIQUE ; ELECTRICITY ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT ; INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIRCHEMICAL OR PHYSICAL PROPERTIES ; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION ORRERADIATION OF RADIO WAVES ; LOUDSPEAKERS, MICROPHONES, GRAMOPHONE PICK-UPS OR LIKEACOUSTIC ELECTROMECHANICAL TRANSDUCERS ; MEASURING ; MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION,OR SHOCK ; PARACHUTES ; PERFORMING OPERATIONS ; PHYSICS ; PUBLIC ADDRESS SYSTEMS ; RADIO DIRECTION-FINDING ; RADIO NAVIGATION ; TESTING ; TRANSPORTING</subject><creationdate>2020</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&date=20200407&DB=EPODOC&CC=BR&NR=102019013615A2$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20200407&DB=EPODOC&CC=BR&NR=102019013615A2$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>JAIME SLY</creatorcontrib><creatorcontrib>JOSHUA BOELMAN</creatorcontrib><title>sistema de sensor acústico para uma aeronave, método para controlar a diretividade de sinais acústicos de um sistema de sensor acústico, e, protetor de eco fixo</title><description>sistema de sensor acústico para uma aeronave, método para controlar a diretividade de sinais acústicos de um sistema de sensor acústico, e, protetor de eco fixo um sistema de sensor acústico para uma aeronave inclui um transmissor configurado para emitir sinais acústicos externos à aeronave, e pelo menos um microfone posicionado num exterior da aeronave e configurado para captar os sinais acústicos como dados captados. o sistema de sensor acústico é configurado para dirigir os sinais acústicos para o pelo menos um microfone de modo que um nível de pressão sonora seja atenuado perpendicular à aeronave.
An acoustic sensor system (10) for an aircraft (52) includes a transmitter (12) configured to emit acoustic signals external to the aircraft (52), and at least one microphone (14a-14n) positioned on an exterior of the aircraft (52) and configured to sense the acoustic signals as sensed data. The acoustic sensor system (10) is configured to direct the acoustic signals to the at least one microphone (14a-14n) such that a sound pressure level is attenuated perpendicular to the aircraft (52).</description><subject>AIRCRAFT</subject><subject>ANALOGOUS ARRANGEMENTS USING OTHER WAVES</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>DEAF-AID SETS</subject><subject>DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES</subject><subject>ELECTRIC COMMUNICATION TECHNIQUE</subject><subject>ELECTRICITY</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT</subject><subject>INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIRCHEMICAL OR PHYSICAL PROPERTIES</subject><subject>LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION ORRERADIATION OF RADIO WAVES</subject><subject>LOUDSPEAKERS, MICROPHONES, GRAMOPHONE PICK-UPS OR LIKEACOUSTIC ELECTROMECHANICAL TRANSDUCERS</subject><subject>MEASURING</subject><subject>MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION,OR SHOCK</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>PHYSICS</subject><subject>PUBLIC ADDRESS SYSTEMS</subject><subject>RADIO DIRECTION-FINDING</subject><subject>RADIO NAVIGATION</subject><subject>TESTING</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2020</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNjrEKwkAQRNNYiPoP29hFyCUoWKoo1mIflssGDpLb4_YS_CAbf8E2P-YFAnZitTAz-2bmyVOMBGoRKgIhK-wB9fCWYDSDQ4_QRRPJs8WeUmiHV-BqsjTb4LnB-AOV8RRMbyqMpBFmLBr5wmQUuxZ-9KUQC5znQCHKMUBxQ20evExmNTZCq-kukvXlfD9dN-S4JHGoyVIojzeV5ZnaZ6rYqe0hL_7NfQDvfVos</recordid><startdate>20200407</startdate><enddate>20200407</enddate><creator>JAIME SLY</creator><creator>JOSHUA BOELMAN</creator><scope>EVB</scope></search><sort><creationdate>20200407</creationdate><title>sistema de sensor acústico para uma aeronave, método para controlar a diretividade de sinais acústicos de um sistema de sensor acústico, e, protetor de eco fixo</title><author>JAIME SLY ; JOSHUA BOELMAN</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_BR102019013615A23</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>por</language><creationdate>2020</creationdate><topic>AIRCRAFT</topic><topic>ANALOGOUS ARRANGEMENTS USING OTHER WAVES</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>DEAF-AID SETS</topic><topic>DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES</topic><topic>ELECTRIC COMMUNICATION TECHNIQUE</topic><topic>ELECTRICITY</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT</topic><topic>INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIRCHEMICAL OR PHYSICAL PROPERTIES</topic><topic>LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION ORRERADIATION OF RADIO WAVES</topic><topic>LOUDSPEAKERS, MICROPHONES, GRAMOPHONE PICK-UPS OR LIKEACOUSTIC ELECTROMECHANICAL TRANSDUCERS</topic><topic>MEASURING</topic><topic>MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION,OR SHOCK</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>PHYSICS</topic><topic>PUBLIC ADDRESS SYSTEMS</topic><topic>RADIO DIRECTION-FINDING</topic><topic>RADIO NAVIGATION</topic><topic>TESTING</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>JAIME SLY</creatorcontrib><creatorcontrib>JOSHUA BOELMAN</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>JAIME SLY</au><au>JOSHUA BOELMAN</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>sistema de sensor acústico para uma aeronave, método para controlar a diretividade de sinais acústicos de um sistema de sensor acústico, e, protetor de eco fixo</title><date>2020-04-07</date><risdate>2020</risdate><abstract>sistema de sensor acústico para uma aeronave, método para controlar a diretividade de sinais acústicos de um sistema de sensor acústico, e, protetor de eco fixo um sistema de sensor acústico para uma aeronave inclui um transmissor configurado para emitir sinais acústicos externos à aeronave, e pelo menos um microfone posicionado num exterior da aeronave e configurado para captar os sinais acústicos como dados captados. o sistema de sensor acústico é configurado para dirigir os sinais acústicos para o pelo menos um microfone de modo que um nível de pressão sonora seja atenuado perpendicular à aeronave.
An acoustic sensor system (10) for an aircraft (52) includes a transmitter (12) configured to emit acoustic signals external to the aircraft (52), and at least one microphone (14a-14n) positioned on an exterior of the aircraft (52) and configured to sense the acoustic signals as sensed data. The acoustic sensor system (10) is configured to direct the acoustic signals to the at least one microphone (14a-14n) such that a sound pressure level is attenuated perpendicular to the aircraft (52).</abstract><oa>free_for_read</oa></addata></record> |
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| language | por |
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| subjects | AIRCRAFT ANALOGOUS ARRANGEMENTS USING OTHER WAVES ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS DEAF-AID SETS DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES ELECTRIC COMMUNICATION TECHNIQUE ELECTRICITY EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIRCHEMICAL OR PHYSICAL PROPERTIES LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION ORRERADIATION OF RADIO WAVES LOUDSPEAKERS, MICROPHONES, GRAMOPHONE PICK-UPS OR LIKEACOUSTIC ELECTROMECHANICAL TRANSDUCERS MEASURING MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION,OR SHOCK PARACHUTES PERFORMING OPERATIONS PHYSICS PUBLIC ADDRESS SYSTEMS RADIO DIRECTION-FINDING RADIO NAVIGATION TESTING TRANSPORTING |
| title | sistema de sensor acústico para uma aeronave, método para controlar a diretividade de sinais acústicos de um sistema de sensor acústico, e, protetor de eco fixo |
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