Arrangement for boundary layer suction of aircraft
The arrangement has a porous carrier layer (3) which is applied to a bearing structure of the aircraft (1) in the area of boundary layer removal (5). The layer is discretely connected to a suction channel (4). A layer of microfibre fabric (2), which conforms to the surface structure, is fastened to...
Gespeichert in:
Hauptverfasser: | , |
---|---|
Format: | Patent |
Sprache: | eng ; 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 | WALDENMAIER, THOMAS, 88677 MARKDORF, DE DITTRICH, KAY, 88090 IMMENSTAAD, DE |
description | The arrangement has a porous carrier layer (3) which is applied to a bearing structure of the aircraft (1) in the area of boundary layer removal (5). The layer is discretely connected to a suction channel (4). A layer of microfibre fabric (2), which conforms to the surface structure, is fastened to the porous carrier layer.The carrier layer is pref. glued to the aircraft structure. It consists of a material, which is a distancing fabric, or a syntactical foam with very low resin content, or a fibre-enforced synthetic with extremely low resin content, or a fibre-enforced ceramic with high number of pores. |
format | Patent |
fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_DE4414205A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>DE4414205A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_DE4414205A13</originalsourceid><addsrcrecordid>eNrjZDByLCpKzEtPzU3NK1FIyy9SSMovzUtJLKpUyEmsTC1SKC5NLsnMz1PIT1NIzCxKLkpMK-FhYE1LzClO5YXS3AwKbq4hzh66qQX58anFBYnJqXmpJfEuriYmhiZGBqaOhsZEKAEAh4crsw</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Arrangement for boundary layer suction of aircraft</title><source>esp@cenet</source><creator>WALDENMAIER, THOMAS, 88677 MARKDORF, DE ; DITTRICH, KAY, 88090 IMMENSTAAD, DE</creator><creatorcontrib>WALDENMAIER, THOMAS, 88677 MARKDORF, DE ; DITTRICH, KAY, 88090 IMMENSTAAD, DE</creatorcontrib><description>The arrangement has a porous carrier layer (3) which is applied to a bearing structure of the aircraft (1) in the area of boundary layer removal (5). The layer is discretely connected to a suction channel (4). A layer of microfibre fabric (2), which conforms to the surface structure, is fastened to the porous carrier layer.The carrier layer is pref. glued to the aircraft structure. It consists of a material, which is a distancing fabric, or a syntactical foam with very low resin content, or a fibre-enforced synthetic with extremely low resin content, or a fibre-enforced ceramic with high number of pores.</description><edition>6</edition><language>eng ; ger</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>1995</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=19951026&DB=EPODOC&CC=DE&NR=4414205A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25543,76293</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=19951026&DB=EPODOC&CC=DE&NR=4414205A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>WALDENMAIER, THOMAS, 88677 MARKDORF, DE</creatorcontrib><creatorcontrib>DITTRICH, KAY, 88090 IMMENSTAAD, DE</creatorcontrib><title>Arrangement for boundary layer suction of aircraft</title><description>The arrangement has a porous carrier layer (3) which is applied to a bearing structure of the aircraft (1) in the area of boundary layer removal (5). The layer is discretely connected to a suction channel (4). A layer of microfibre fabric (2), which conforms to the surface structure, is fastened to the porous carrier layer.The carrier layer is pref. glued to the aircraft structure. It consists of a material, which is a distancing fabric, or a syntactical foam with very low resin content, or a fibre-enforced synthetic with extremely low resin content, or a fibre-enforced ceramic with high number of pores.</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>HELICOPTERS</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>1995</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZDByLCpKzEtPzU3NK1FIyy9SSMovzUtJLKpUyEmsTC1SKC5NLsnMz1PIT1NIzCxKLkpMK-FhYE1LzClO5YXS3AwKbq4hzh66qQX58anFBYnJqXmpJfEuriYmhiZGBqaOhsZEKAEAh4crsw</recordid><startdate>19951026</startdate><enddate>19951026</enddate><creator>WALDENMAIER, THOMAS, 88677 MARKDORF, DE</creator><creator>DITTRICH, KAY, 88090 IMMENSTAAD, DE</creator><scope>EVB</scope></search><sort><creationdate>19951026</creationdate><title>Arrangement for boundary layer suction of aircraft</title><author>WALDENMAIER, THOMAS, 88677 MARKDORF, DE ; DITTRICH, KAY, 88090 IMMENSTAAD, DE</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_DE4414205A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; ger</language><creationdate>1995</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>WALDENMAIER, THOMAS, 88677 MARKDORF, DE</creatorcontrib><creatorcontrib>DITTRICH, KAY, 88090 IMMENSTAAD, DE</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>WALDENMAIER, THOMAS, 88677 MARKDORF, DE</au><au>DITTRICH, KAY, 88090 IMMENSTAAD, DE</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Arrangement for boundary layer suction of aircraft</title><date>1995-10-26</date><risdate>1995</risdate><abstract>The arrangement has a porous carrier layer (3) which is applied to a bearing structure of the aircraft (1) in the area of boundary layer removal (5). The layer is discretely connected to a suction channel (4). A layer of microfibre fabric (2), which conforms to the surface structure, is fastened to the porous carrier layer.The carrier layer is pref. glued to the aircraft structure. It consists of a material, which is a distancing fabric, or a syntactical foam with very low resin content, or a fibre-enforced synthetic with extremely low resin content, or a fibre-enforced ceramic with high number of pores.</abstract><edition>6</edition><oa>free_for_read</oa></addata></record> |
fulltext | fulltext_linktorsrc |
identifier | |
ispartof | |
issn | |
language | eng ; ger |
recordid | cdi_epo_espacenet_DE4414205A1 |
source | esp@cenet |
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 | Arrangement for boundary layer suction of aircraft |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-25T20%3A51%3A53IST&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=WALDENMAIER,%20THOMAS,%2088677%20MARKDORF,%20DE&rft.date=1995-10-26&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EDE4414205A1%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 |