Aircraft wing structure profiled suspension pylon
According to the invention, the suspension pylon ( 3 ) comprises a fairing for reducing the local loss in lift ( 8 ) and its maximum-width section ( 7 ) is located at the front of the concave and set-back rear part ( 4 R) of the pressure face ( 4 ) of the wing structure ( 1 ). The fairing for reduci...
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| creator | Cambon, Jean-Louis |
| description | According to the invention, the suspension pylon (
3
) comprises a fairing for reducing the local loss in lift (
8
) and its maximum-width section (
7
) is located at the front of the concave and set-back rear part (
4
R) of the pressure face (
4
) of the wing structure (
1
). The fairing for reducing the local loss in lift (
8
):
is housed, at least over most of its height, in the concavity of said rear part (
4
R) of the pressure face (
4
) of the wing structure (
1
), and widens laterally toward the rear; and
comprises a projecting rear part (
12
) that tapers toward the rear and ends in an aerodynamic trailing edge (
16
) the length of which is very long by comparison with said maximum width of the fairing. |
| format | Patent |
| fullrecord | <record><control><sourceid>uspatents_EFI</sourceid><recordid>TN_cdi_uspatents_applications_20010028019</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>20010028019</sourcerecordid><originalsourceid>FETCH-uspatents_applications_200100280193</originalsourceid><addsrcrecordid>eNrjZDB0zCxKLkpMK1Eoz8xLVyguKSpNLiktSlUoKMpPy8xJTVEoLi0uSM0rzszPUyiozMnP42FgTUvMKU7lhdLcDJpuriHOHrpAdYklqXklxfGJBQU5mcmJJUA9xfFGBgaGBgZGFgaGlsakqAUAR3wzZg</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Aircraft wing structure profiled suspension pylon</title><source>USPTO Published Applications</source><creator>Cambon, Jean-Louis</creator><creatorcontrib>Cambon, Jean-Louis</creatorcontrib><description>According to the invention, the suspension pylon (
3
) comprises a fairing for reducing the local loss in lift (
8
) and its maximum-width section (
7
) is located at the front of the concave and set-back rear part (
4
R) of the pressure face (
4
) of the wing structure (
1
). The fairing for reducing the local loss in lift (
8
):
is housed, at least over most of its height, in the concavity of said rear part (
4
R) of the pressure face (
4
) of the wing structure (
1
), and widens laterally toward the rear; and
comprises a projecting rear part (
12
) that tapers toward the rear and ends in an aerodynamic trailing edge (
16
) the length of which is very long by comparison with said maximum width of the fairing.</description><language>eng</language><creationdate>2001</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20010028019$$EPDF$$P50$$Guspatents$$Hfree_for_read</linktopdf><link.rule.ids>230,308,776,869,881,64032</link.rule.ids><linktorsrc>$$Uhttps://patentcenter.uspto.gov/applications/09798918$$EView_record_in_USPTO$$FView_record_in_$$GUSPTO$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Cambon, Jean-Louis</creatorcontrib><title>Aircraft wing structure profiled suspension pylon</title><description>According to the invention, the suspension pylon (
3
) comprises a fairing for reducing the local loss in lift (
8
) and its maximum-width section (
7
) is located at the front of the concave and set-back rear part (
4
R) of the pressure face (
4
) of the wing structure (
1
). The fairing for reducing the local loss in lift (
8
):
is housed, at least over most of its height, in the concavity of said rear part (
4
R) of the pressure face (
4
) of the wing structure (
1
), and widens laterally toward the rear; and
comprises a projecting rear part (
12
) that tapers toward the rear and ends in an aerodynamic trailing edge (
16
) the length of which is very long by comparison with said maximum width of the fairing.</description><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2001</creationdate><recordtype>patent</recordtype><sourceid>EFI</sourceid><recordid>eNrjZDB0zCxKLkpMK1Eoz8xLVyguKSpNLiktSlUoKMpPy8xJTVEoLi0uSM0rzszPUyiozMnP42FgTUvMKU7lhdLcDJpuriHOHrpAdYklqXklxfGJBQU5mcmJJUA9xfFGBgaGBgZGFgaGlsakqAUAR3wzZg</recordid><startdate>20011011</startdate><enddate>20011011</enddate><creator>Cambon, Jean-Louis</creator><scope>EFI</scope></search><sort><creationdate>20011011</creationdate><title>Aircraft wing structure profiled suspension pylon</title><author>Cambon, Jean-Louis</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-uspatents_applications_200100280193</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2001</creationdate><toplevel>online_resources</toplevel><creatorcontrib>Cambon, Jean-Louis</creatorcontrib><collection>USPTO Published Applications</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Cambon, Jean-Louis</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Aircraft wing structure profiled suspension pylon</title><date>2001-10-11</date><risdate>2001</risdate><abstract>According to the invention, the suspension pylon (
3
) comprises a fairing for reducing the local loss in lift (
8
) and its maximum-width section (
7
) is located at the front of the concave and set-back rear part (
4
R) of the pressure face (
4
) of the wing structure (
1
). The fairing for reducing the local loss in lift (
8
):
is housed, at least over most of its height, in the concavity of said rear part (
4
R) of the pressure face (
4
) of the wing structure (
1
), and widens laterally toward the rear; and
comprises a projecting rear part (
12
) that tapers toward the rear and ends in an aerodynamic trailing edge (
16
) the length of which is very long by comparison with said maximum width of the fairing.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng |
| recordid | cdi_uspatents_applications_20010028019 |
| source | USPTO Published Applications |
| title | Aircraft wing structure profiled suspension pylon |
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