SPLIT-AILERON CONTROL
The present invention provides methods and system for controlling the operation of an aircraft aileron which comprises an inboard portion and an outboard portion. A velocity of the aircraft is determined. Then, based on the velocity of the aircraft, the aileron is caused to move in certain ways. Whe...
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| creator | MOKHTARIAN FARZAD DE KOK GERARDUS HERBERTUS AHN THOMAS VIGNERON SEBASTIEN ERIC BENOIT TANG GRACE SHWU JEN |
| description | The present invention provides methods and system for controlling the operation of an aircraft aileron which comprises an inboard portion and an outboard portion. A velocity of the aircraft is determined. Then, based on the velocity of the aircraft, the aileron is caused to move in certain ways. When the velocity is below a first velocity threshold, the inboard aileron portion and the outboard aileron portion are caused to move substantially in unison. When the velocity is between the first velocity threshold and a second, greater, velocity threshold, the outboard portion of the aileron is caused to lock and the inboard portion of the aileron is caused to move independently from the outboard portion. When the velocity is above the second velocity threshold, the inboard portion is caused tomove substantially opposite from the outboard portion.
本公开提供了用于控制飞机副翼的操作的方法和系统，该飞机副翼包括内侧部分和外侧部分。确定飞机的速度。然后，根据飞机的速度，使副翼以某种方式移动。在低于第一速度阈值时，使内侧副翼部分和外侧副翼部分基本上一致地移动。在第一速度阈值和更大的第二速度阈值之间，使副翼的外侧部分锁定，并且使副翼的内侧部分独立于外侧部分移动。在高于第二速度阈值时，使内 |
| format | Patent |
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本公开提供了用于控制飞机副翼的操作的方法和系统，该飞机副翼包括内侧部分和外侧部分。确定飞机的速度。然后，根据飞机的速度，使副翼以某种方式移动。在低于第一速度阈值时，使内侧副翼部分和外侧副翼部分基本上一致地移动。在第一速度阈值和更大的第二速度阈值之间，使副翼的外侧部分锁定，并且使副翼的内侧部分独立于外侧部分移动。在高于第二速度阈值时，使内</description><language>chi ; eng</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; COSMONAUTICS ; HELICOPTERS ; PERFORMING OPERATIONS ; TRANSPORTING</subject><creationdate>2019</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=20190806&DB=EPODOC&CC=CN&NR=110099847A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20190806&DB=EPODOC&CC=CN&NR=110099847A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>MOKHTARIAN FARZAD</creatorcontrib><creatorcontrib>DE KOK GERARDUS HERBERTUS</creatorcontrib><creatorcontrib>AHN THOMAS</creatorcontrib><creatorcontrib>VIGNERON SEBASTIEN ERIC BENOIT</creatorcontrib><creatorcontrib>TANG GRACE SHWU JEN</creatorcontrib><title>SPLIT-AILERON CONTROL</title><description>The present invention provides methods and system for controlling the operation of an aircraft aileron which comprises an inboard portion and an outboard portion. A velocity of the aircraft is determined. Then, based on the velocity of the aircraft, the aileron is caused to move in certain ways. When the velocity is below a first velocity threshold, the inboard aileron portion and the outboard aileron portion are caused to move substantially in unison. When the velocity is between the first velocity threshold and a second, greater, velocity threshold, the outboard portion of the aileron is caused to lock and the inboard portion of the aileron is caused to move independently from the outboard portion. When the velocity is above the second velocity threshold, the inboard portion is caused tomove substantially opposite from the outboard portion.
本公开提供了用于控制飞机副翼的操作的方法和系统，该飞机副翼包括内侧部分和外侧部分。确定飞机的速度。然后，根据飞机的速度，使副翼以某种方式移动。在低于第一速度阈值时，使内侧副翼部分和外侧副翼部分基本上一致地移动。在第一速度阈值和更大的第二速度阈值之间，使副翼的外侧部分锁定，并且使副翼的内侧部分独立于外侧部分移动。在高于第二速度阈值时，使内</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>2019</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZBANDvDxDNF19PRxDfL3U3D29wsJ8vfhYWBNS8wpTuWF0twMim6uIc4euqkF-fGpxQWJyal5qSXxzn6GhgYGlpYWJuaOxsSoAQCk3R8O</recordid><startdate>20190806</startdate><enddate>20190806</enddate><creator>MOKHTARIAN FARZAD</creator><creator>DE KOK GERARDUS HERBERTUS</creator><creator>AHN THOMAS</creator><creator>VIGNERON SEBASTIEN ERIC BENOIT</creator><creator>TANG GRACE SHWU JEN</creator><scope>EVB</scope></search><sort><creationdate>20190806</creationdate><title>SPLIT-AILERON CONTROL</title><author>MOKHTARIAN FARZAD ; DE KOK GERARDUS HERBERTUS ; AHN THOMAS ; VIGNERON SEBASTIEN ERIC BENOIT ; TANG GRACE SHWU JEN</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN110099847A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2019</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>MOKHTARIAN FARZAD</creatorcontrib><creatorcontrib>DE KOK GERARDUS HERBERTUS</creatorcontrib><creatorcontrib>AHN THOMAS</creatorcontrib><creatorcontrib>VIGNERON SEBASTIEN ERIC BENOIT</creatorcontrib><creatorcontrib>TANG GRACE SHWU JEN</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>MOKHTARIAN FARZAD</au><au>DE KOK GERARDUS HERBERTUS</au><au>AHN THOMAS</au><au>VIGNERON SEBASTIEN ERIC BENOIT</au><au>TANG GRACE SHWU JEN</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>SPLIT-AILERON CONTROL</title><date>2019-08-06</date><risdate>2019</risdate><abstract>The present invention provides methods and system for controlling the operation of an aircraft aileron which comprises an inboard portion and an outboard portion. A velocity of the aircraft is determined. Then, based on the velocity of the aircraft, the aileron is caused to move in certain ways. When the velocity is below a first velocity threshold, the inboard aileron portion and the outboard aileron portion are caused to move substantially in unison. When the velocity is between the first velocity threshold and a second, greater, velocity threshold, the outboard portion of the aileron is caused to lock and the inboard portion of the aileron is caused to move independently from the outboard portion. When the velocity is above the second velocity threshold, the inboard portion is caused tomove substantially opposite from the outboard portion.
本公开提供了用于控制飞机副翼的操作的方法和系统，该飞机副翼包括内侧部分和外侧部分。确定飞机的速度。然后，根据飞机的速度，使副翼以某种方式移动。在低于第一速度阈值时，使内侧副翼部分和外侧副翼部分基本上一致地移动。在第一速度阈值和更大的第二速度阈值之间，使副翼的外侧部分锁定，并且使副翼的内侧部分独立于外侧部分移动。在高于第二速度阈值时，使内</abstract><oa>free_for_read</oa></addata></record> |
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| language | chi ; eng |
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| subjects | AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING |
| title | SPLIT-AILERON CONTROL |
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