Turbofan engine and aircraft
The invention relates to a turbofan having a nacelle and an aircraft. The turbofan includes a slider translationally mobile to open a window between a duct and the exterior, a plurality of blades, each rotationally mobile on the slider, and a maneuvering system moving each blade and comprising for e...
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| creator | GARDES PASCAL BROCHARD WOLFGANG BOUDOU ANTOINE |
| description | The invention relates to a turbofan having a nacelle and an aircraft. The turbofan includes a slider translationally mobile to open a window between a duct and the exterior, a plurality of blades, each rotationally mobile on the slider, and a maneuvering system moving each blade and comprising for each blade, a shaft rotationally mobile on the slider and onto which the blade is fixed, an arm having a first end fixed to the shaft, an arc coaxial with the longitudinal axis, mounted rotationally mobile on the slider about the longitudinal axis, a rectilinear rod fixed by its base to the arc, therectilinear rod inserted into a through-bore of a stock, wherein the stock is mounted translationally free relative to the rectilinear rod, and the stock is mounted rotationally free on the arm at itssecond end about a rocking axis parallel to the rotational axis, and an actuation system producing arc rotation in two opposite directions.
涉及具有短舱的涡轮风扇发动机和飞行器，涡轮风扇发动机包括：在前进位置与缩回位置之间平移移动的滑动件，以在管道与外部之间开放窗口；多个叶片，每个叶片在滑动件上在收起位置与展 |
| format | Patent |
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涉及具有短舱的涡轮风扇发动机和飞行器，涡轮风扇发动机包括：在前进位置与缩回位置之间平移移动的滑动件，以在管道与外部之间开放窗口；多个叶片，每个叶片在滑动件上在收起位置与展</description><language>chi ; eng</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; BLASTING ; COMBUSTION ENGINES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; GAS-TURBINE PLANTS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; JET-PROPULSION PLANTS ; LIGHTING ; MECHANICAL ENGINEERING ; WEAPONS</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=20201027&DB=EPODOC&CC=CN&NR=111828199A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25543,76293</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20201027&DB=EPODOC&CC=CN&NR=111828199A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>GARDES PASCAL</creatorcontrib><creatorcontrib>BROCHARD WOLFGANG</creatorcontrib><creatorcontrib>BOUDOU ANTOINE</creatorcontrib><title>Turbofan engine and aircraft</title><description>The invention relates to a turbofan having a nacelle and an aircraft. The turbofan includes a slider translationally mobile to open a window between a duct and the exterior, a plurality of blades, each rotationally mobile on the slider, and a maneuvering system moving each blade and comprising for each blade, a shaft rotationally mobile on the slider and onto which the blade is fixed, an arm having a first end fixed to the shaft, an arc coaxial with the longitudinal axis, mounted rotationally mobile on the slider about the longitudinal axis, a rectilinear rod fixed by its base to the arc, therectilinear rod inserted into a through-bore of a stock, wherein the stock is mounted translationally free relative to the rectilinear rod, and the stock is mounted rotationally free on the arm at itssecond end about a rocking axis parallel to the rotational axis, and an actuation system producing arc rotation in two opposite directions.
涉及具有短舱的涡轮风扇发动机和飞行器，涡轮风扇发动机包括：在前进位置与缩回位置之间平移移动的滑动件，以在管道与外部之间开放窗口；多个叶片，每个叶片在滑动件上在收起位置与展</description><subject>AIR INTAKES FOR JET-PROPULSION PLANTS</subject><subject>BLASTING</subject><subject>COMBUSTION ENGINES</subject><subject>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</subject><subject>GAS-TURBINE PLANTS</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>JET-PROPULSION PLANTS</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2020</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZJAJKS1Kyk9LzFNIzUvPzEtVSMxLUUjMLEouSkwr4WFgTUvMKU7lhdLcDIpuriHOHrqpBfnxqcUFicmpeakl8c5-hoaGFkYWhpaWjsbEqAEAkuAjqQ</recordid><startdate>20201027</startdate><enddate>20201027</enddate><creator>GARDES PASCAL</creator><creator>BROCHARD WOLFGANG</creator><creator>BOUDOU ANTOINE</creator><scope>EVB</scope></search><sort><creationdate>20201027</creationdate><title>Turbofan engine and aircraft</title><author>GARDES PASCAL ; BROCHARD WOLFGANG ; BOUDOU ANTOINE</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN111828199A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2020</creationdate><topic>AIR INTAKES FOR JET-PROPULSION PLANTS</topic><topic>BLASTING</topic><topic>COMBUSTION ENGINES</topic><topic>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</topic><topic>GAS-TURBINE PLANTS</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>JET-PROPULSION PLANTS</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>GARDES PASCAL</creatorcontrib><creatorcontrib>BROCHARD WOLFGANG</creatorcontrib><creatorcontrib>BOUDOU ANTOINE</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>GARDES PASCAL</au><au>BROCHARD WOLFGANG</au><au>BOUDOU ANTOINE</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Turbofan engine and aircraft</title><date>2020-10-27</date><risdate>2020</risdate><abstract>The invention relates to a turbofan having a nacelle and an aircraft. The turbofan includes a slider translationally mobile to open a window between a duct and the exterior, a plurality of blades, each rotationally mobile on the slider, and a maneuvering system moving each blade and comprising for each blade, a shaft rotationally mobile on the slider and onto which the blade is fixed, an arm having a first end fixed to the shaft, an arc coaxial with the longitudinal axis, mounted rotationally mobile on the slider about the longitudinal axis, a rectilinear rod fixed by its base to the arc, therectilinear rod inserted into a through-bore of a stock, wherein the stock is mounted translationally free relative to the rectilinear rod, and the stock is mounted rotationally free on the arm at itssecond end about a rocking axis parallel to the rotational axis, and an actuation system producing arc rotation in two opposite directions.
涉及具有短舱的涡轮风扇发动机和飞行器，涡轮风扇发动机包括：在前进位置与缩回位置之间平移移动的滑动件，以在管道与外部之间开放窗口；多个叶片，每个叶片在滑动件上在收起位置与展</abstract><oa>free_for_read</oa></addata></record> |
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| language | chi ; eng |
| recordid | cdi_epo_espacenet_CN111828199A |
| source | esp@cenet |
| subjects | AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS |
| title | Turbofan engine and aircraft |
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