APPARATUS FOR INTEGRATED NOISE CONTROL AND FLOW CONTROL IN AN AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM

Aircraft, environmental control systems, and air diffusers that may be used to create a quiet, comfortable environment within an aircraft cabin are disclosed. The air diffusers include a duct (30), a grille (50), and a porous flow conditioner (60) positioned at least partially within an outlet plenu...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: BULTEMEIER, ERIC JAMES, JONES, RODERICK M, HLAVKA, BRIAN DALE, BARKER, GAIL MARY
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page
container_issue
container_start_page
container_title
container_volume
creator BULTEMEIER, ERIC JAMES
JONES, RODERICK M
HLAVKA, BRIAN DALE
BARKER, GAIL MARY
description Aircraft, environmental control systems, and air diffusers that may be used to create a quiet, comfortable environment within an aircraft cabin are disclosed. The air diffusers include a duct (30), a grille (50), and a porous flow conditioner (60) positioned at least partially within an outlet plenum (36) of the duct. The porous flow conditioner is configured to create backpressure and to reduce a velocity of air flowing out of the porous flow conditioner, relative to air flow unaffected by the porous flow conditioner. The porous flow conditioner may be configured to reduce noise generated by air flow through the air diffuser assembly, relative to air flow unaffected by the porous flow conditioner. The porous flow conditioner may be configured to reduce noise generated by air flow downstream of the porous flow conditioner.
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP3088303A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP3088303A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP3088303A13</originalsourceid><addsrcrecordid>eNqNirEKwjAQQLM4iPoP9wNCJUvXI71oIL2E5FQ6lVLiJFqo_48dpLPT4z3eVo0YIyaUawYbEjgWOi9KDXBwmcAElhQ8IDdgfbivwfHSAF0yCa0A8c2lwC2xoF-n3GWhdq82j-E5l8OPOwWWxFyOZXr3ZZ6GsbzKp6eoq7rWlcaT_mP5AtfrNCg</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>APPARATUS FOR INTEGRATED NOISE CONTROL AND FLOW CONTROL IN AN AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM</title><source>esp@cenet</source><creator>BULTEMEIER, ERIC JAMES ; JONES, RODERICK M ; HLAVKA, BRIAN DALE ; BARKER, GAIL MARY</creator><creatorcontrib>BULTEMEIER, ERIC JAMES ; JONES, RODERICK M ; HLAVKA, BRIAN DALE ; BARKER, GAIL MARY</creatorcontrib><description>Aircraft, environmental control systems, and air diffusers that may be used to create a quiet, comfortable environment within an aircraft cabin are disclosed. The air diffusers include a duct (30), a grille (50), and a porous flow conditioner (60) positioned at least partially within an outlet plenum (36) of the duct. The porous flow conditioner is configured to create backpressure and to reduce a velocity of air flowing out of the porous flow conditioner, relative to air flow unaffected by the porous flow conditioner. The porous flow conditioner may be configured to reduce noise generated by air flow through the air diffuser assembly, relative to air flow unaffected by the porous flow conditioner. The porous flow conditioner may be configured to reduce noise generated by air flow downstream of the porous flow conditioner.</description><language>eng ; fre ; ger</language><subject>AIR-CONDITIONING, AIR-HUMIDIFICATION, VENTILATION, USE OF AIRCURRENTS FOR SCREENING ; AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; BLASTING ; COSMONAUTICS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; HEATING ; LIGHTING ; MECHANICAL ENGINEERING ; PARACHUTES ; PERFORMING OPERATIONS ; RANGES ; TRANSPORTING ; VENTILATING ; WEAPONS</subject><creationdate>2016</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=20161102&amp;DB=EPODOC&amp;CC=EP&amp;NR=3088303A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20161102&amp;DB=EPODOC&amp;CC=EP&amp;NR=3088303A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>BULTEMEIER, ERIC JAMES</creatorcontrib><creatorcontrib>JONES, RODERICK M</creatorcontrib><creatorcontrib>HLAVKA, BRIAN DALE</creatorcontrib><creatorcontrib>BARKER, GAIL MARY</creatorcontrib><title>APPARATUS FOR INTEGRATED NOISE CONTROL AND FLOW CONTROL IN AN AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM</title><description>Aircraft, environmental control systems, and air diffusers that may be used to create a quiet, comfortable environment within an aircraft cabin are disclosed. The air diffusers include a duct (30), a grille (50), and a porous flow conditioner (60) positioned at least partially within an outlet plenum (36) of the duct. The porous flow conditioner is configured to create backpressure and to reduce a velocity of air flowing out of the porous flow conditioner, relative to air flow unaffected by the porous flow conditioner. The porous flow conditioner may be configured to reduce noise generated by air flow through the air diffuser assembly, relative to air flow unaffected by the porous flow conditioner. The porous flow conditioner may be configured to reduce noise generated by air flow downstream of the porous flow conditioner.</description><subject>AIR-CONDITIONING, AIR-HUMIDIFICATION, VENTILATION, USE OF AIRCURRENTS FOR SCREENING</subject><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>BLASTING</subject><subject>COSMONAUTICS</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>HEATING</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>RANGES</subject><subject>TRANSPORTING</subject><subject>VENTILATING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2016</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNirEKwjAQQLM4iPoP9wNCJUvXI71oIL2E5FQ6lVLiJFqo_48dpLPT4z3eVo0YIyaUawYbEjgWOi9KDXBwmcAElhQ8IDdgfbivwfHSAF0yCa0A8c2lwC2xoF-n3GWhdq82j-E5l8OPOwWWxFyOZXr3ZZ6GsbzKp6eoq7rWlcaT_mP5AtfrNCg</recordid><startdate>20161102</startdate><enddate>20161102</enddate><creator>BULTEMEIER, ERIC JAMES</creator><creator>JONES, RODERICK M</creator><creator>HLAVKA, BRIAN DALE</creator><creator>BARKER, GAIL MARY</creator><scope>EVB</scope></search><sort><creationdate>20161102</creationdate><title>APPARATUS FOR INTEGRATED NOISE CONTROL AND FLOW CONTROL IN AN AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM</title><author>BULTEMEIER, ERIC JAMES ; JONES, RODERICK M ; HLAVKA, BRIAN DALE ; BARKER, GAIL MARY</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3088303A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2016</creationdate><topic>AIR-CONDITIONING, AIR-HUMIDIFICATION, VENTILATION, USE OF AIRCURRENTS FOR SCREENING</topic><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>BLASTING</topic><topic>COSMONAUTICS</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>HEATING</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>RANGES</topic><topic>TRANSPORTING</topic><topic>VENTILATING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>BULTEMEIER, ERIC JAMES</creatorcontrib><creatorcontrib>JONES, RODERICK M</creatorcontrib><creatorcontrib>HLAVKA, BRIAN DALE</creatorcontrib><creatorcontrib>BARKER, GAIL MARY</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>BULTEMEIER, ERIC JAMES</au><au>JONES, RODERICK M</au><au>HLAVKA, BRIAN DALE</au><au>BARKER, GAIL MARY</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>APPARATUS FOR INTEGRATED NOISE CONTROL AND FLOW CONTROL IN AN AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM</title><date>2016-11-02</date><risdate>2016</risdate><abstract>Aircraft, environmental control systems, and air diffusers that may be used to create a quiet, comfortable environment within an aircraft cabin are disclosed. The air diffusers include a duct (30), a grille (50), and a porous flow conditioner (60) positioned at least partially within an outlet plenum (36) of the duct. The porous flow conditioner is configured to create backpressure and to reduce a velocity of air flowing out of the porous flow conditioner, relative to air flow unaffected by the porous flow conditioner. The porous flow conditioner may be configured to reduce noise generated by air flow through the air diffuser assembly, relative to air flow unaffected by the porous flow conditioner. The porous flow conditioner may be configured to reduce noise generated by air flow downstream of the porous flow conditioner.</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng ; fre ; ger
recordid cdi_epo_espacenet_EP3088303A1
source esp@cenet
subjects AIR-CONDITIONING, AIR-HUMIDIFICATION, VENTILATION, USE OF AIRCURRENTS FOR SCREENING
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
BLASTING
COSMONAUTICS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
HEATING
LIGHTING
MECHANICAL ENGINEERING
PARACHUTES
PERFORMING OPERATIONS
RANGES
TRANSPORTING
VENTILATING
WEAPONS
title APPARATUS FOR INTEGRATED NOISE CONTROL AND FLOW CONTROL IN AN AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-08T15%3A28%3A31IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-epo_EVB&rft_val_fmt=info:ofi/fmt:kev:mtx:patent&rft.genre=patent&rft.au=BULTEMEIER,%20ERIC%20JAMES&rft.date=2016-11-02&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EEP3088303A1%3C/epo_EVB%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true