Sealing structure used between flaps of airplane
The invention relates to a sealing arrangement for use between flaps of an aircraft, the sealing arrangement comprising a first sealing portion and a second sealing portion, the first and second sealing portions interfacing one another between the flaps, where the first sealing portion comprises a p...
Gespeichert in:
| Hauptverfasser: | , , , , |
|---|---|
| Format: | Patent |
| Sprache: | chi ; eng |
| 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 | YANG YINGHAO ZHANG JIASEN CHEN YIN YUAN XIUQI LI CHENXI |
| description | The invention relates to a sealing arrangement for use between flaps of an aircraft, the sealing arrangement comprising a first sealing portion and a second sealing portion, the first and second sealing portions interfacing one another between the flaps, where the first sealing portion comprises a plurality of discrete first seals, and the second sealing portion comprises a plurality of discrete second seals. And the second sealing portion includes a plurality of discrete second seals. The sealing structure with the separated design is more suitable for the situation of scissors difference between the inner flap and the outer flap.
本发明涉及一种用于飞机的襟翼之间的密封结构，这种密封结构包括第一密封部分和第二密封部分，第一密封部分和第二密封部分在襟翼之间彼此对接，其中，第一密封部分包括多个离散的第一密封件，并且第二密封部分包括多个离散的第二密封件。这种分离式设计的密封结构更适用于内外襟翼间剪刀差的情形。 |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN117184409A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN117184409A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN117184409A3</originalsourceid><addsrcrecordid>eNrjZDAITk3MycxLVyguKSpNLiktSlUoLU5NUUhKLSlPTc1TSMtJLChWyE9TSMwsKshJzEvlYWBNS8wpTuWF0twMim6uIc4euqkF-fGpxQWJyal5qSXxzn6GhuaGFiYmBpaOxsSoAQBtiCtj</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Sealing structure used between flaps of airplane</title><source>esp@cenet</source><creator>YANG YINGHAO ; ZHANG JIASEN ; CHEN YIN ; YUAN XIUQI ; LI CHENXI</creator><creatorcontrib>YANG YINGHAO ; ZHANG JIASEN ; CHEN YIN ; YUAN XIUQI ; LI CHENXI</creatorcontrib><description>The invention relates to a sealing arrangement for use between flaps of an aircraft, the sealing arrangement comprising a first sealing portion and a second sealing portion, the first and second sealing portions interfacing one another between the flaps, where the first sealing portion comprises a plurality of discrete first seals, and the second sealing portion comprises a plurality of discrete second seals. And the second sealing portion includes a plurality of discrete second seals. The sealing structure with the separated design is more suitable for the situation of scissors difference between the inner flap and the outer flap.
本发明涉及一种用于飞机的襟翼之间的密封结构，这种密封结构包括第一密封部分和第二密封部分，第一密封部分和第二密封部分在襟翼之间彼此对接，其中，第一密封部分包括多个离散的第一密封件，并且第二密封部分包括多个离散的第二密封件。这种分离式设计的密封结构更适用于内外襟翼间剪刀差的情形。</description><language>chi ; eng</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; COSMONAUTICS ; HELICOPTERS ; PERFORMING OPERATIONS ; TRANSPORTING</subject><creationdate>2023</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=20231208&DB=EPODOC&CC=CN&NR=117184409A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25543,76293</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20231208&DB=EPODOC&CC=CN&NR=117184409A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>YANG YINGHAO</creatorcontrib><creatorcontrib>ZHANG JIASEN</creatorcontrib><creatorcontrib>CHEN YIN</creatorcontrib><creatorcontrib>YUAN XIUQI</creatorcontrib><creatorcontrib>LI CHENXI</creatorcontrib><title>Sealing structure used between flaps of airplane</title><description>The invention relates to a sealing arrangement for use between flaps of an aircraft, the sealing arrangement comprising a first sealing portion and a second sealing portion, the first and second sealing portions interfacing one another between the flaps, where the first sealing portion comprises a plurality of discrete first seals, and the second sealing portion comprises a plurality of discrete second seals. And the second sealing portion includes a plurality of discrete second seals. The sealing structure with the separated design is more suitable for the situation of scissors difference between the inner flap and the outer flap.
本发明涉及一种用于飞机的襟翼之间的密封结构，这种密封结构包括第一密封部分和第二密封部分，第一密封部分和第二密封部分在襟翼之间彼此对接，其中，第一密封部分包括多个离散的第一密封件，并且第二密封部分包括多个离散的第二密封件。这种分离式设计的密封结构更适用于内外襟翼间剪刀差的情形。</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>HELICOPTERS</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2023</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZDAITk3MycxLVyguKSpNLiktSlUoLU5NUUhKLSlPTc1TSMtJLChWyE9TSMwsKshJzEvlYWBNS8wpTuWF0twMim6uIc4euqkF-fGpxQWJyal5qSXxzn6GhuaGFiYmBpaOxsSoAQBtiCtj</recordid><startdate>20231208</startdate><enddate>20231208</enddate><creator>YANG YINGHAO</creator><creator>ZHANG JIASEN</creator><creator>CHEN YIN</creator><creator>YUAN XIUQI</creator><creator>LI CHENXI</creator><scope>EVB</scope></search><sort><creationdate>20231208</creationdate><title>Sealing structure used between flaps of airplane</title><author>YANG YINGHAO ; ZHANG JIASEN ; CHEN YIN ; YUAN XIUQI ; LI CHENXI</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN117184409A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2023</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>HELICOPTERS</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>YANG YINGHAO</creatorcontrib><creatorcontrib>ZHANG JIASEN</creatorcontrib><creatorcontrib>CHEN YIN</creatorcontrib><creatorcontrib>YUAN XIUQI</creatorcontrib><creatorcontrib>LI CHENXI</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>YANG YINGHAO</au><au>ZHANG JIASEN</au><au>CHEN YIN</au><au>YUAN XIUQI</au><au>LI CHENXI</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Sealing structure used between flaps of airplane</title><date>2023-12-08</date><risdate>2023</risdate><abstract>The invention relates to a sealing arrangement for use between flaps of an aircraft, the sealing arrangement comprising a first sealing portion and a second sealing portion, the first and second sealing portions interfacing one another between the flaps, where the first sealing portion comprises a plurality of discrete first seals, and the second sealing portion comprises a plurality of discrete second seals. And the second sealing portion includes a plurality of discrete second seals. The sealing structure with the separated design is more suitable for the situation of scissors difference between the inner flap and the outer flap.
本发明涉及一种用于飞机的襟翼之间的密封结构，这种密封结构包括第一密封部分和第二密封部分，第一密封部分和第二密封部分在襟翼之间彼此对接，其中，第一密封部分包括多个离散的第一密封件，并且第二密封部分包括多个离散的第二密封件。这种分离式设计的密封结构更适用于内外襟翼间剪刀差的情形。</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | chi ; eng |
| recordid | cdi_epo_espacenet_CN117184409A |
| source | esp@cenet |
| subjects | AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING |
| title | Sealing structure used between flaps of airplane |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-25T11%3A13%3A05IST&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=YANG%20YINGHAO&rft.date=2023-12-08&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN117184409A%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 |