GUST COMPENSATION SYSTEM AND METHOD FOR AIRCRAFT
PROBLEM TO BE SOLVED: To provide a system and method for efficiently configuring an aircraft to compensate for gusts.SOLUTION: A gust compensation system is configured to adaptively reduce gust loads exerted into an aircraft 100. The gust compensation system may include a first sensor 110 proximate...
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| creator | CHRISTOPHER D DALLARA ALEXANDER C HO YAMASHIRO HISAKO RAFAEL E CAICEDO PAUL C STREFLING KIOUMARS NAJMABADI TZE L SIU KHALED ABDEL-MOTAGALY |
| description | PROBLEM TO BE SOLVED: To provide a system and method for efficiently configuring an aircraft to compensate for gusts.SOLUTION: A gust compensation system is configured to adaptively reduce gust loads exerted into an aircraft 100. The gust compensation system may include a first sensor 110 proximate to a front of the aircraft. The first sensor is configured to output a first signal. A second sensor 120 may be distally located from a front 113 of the aircraft. The second sensor is configured to output a second signal. A gust signal sub-system is configured to receive the first and second signals and generate a gust signal on the basis of analysis of the first and second signals. The gust signal sub-system outputs the gust signal and may modify a load parameter signal in response to the gust signal exceeding a load alleviation threshold.SELECTED DRAWING: Figure 1
【課題】突風を補償するように航空機を効率的に構成するためのシステムおよび方法を提供すること【解決手段】突風補償システムは、航空機１００に作用する突風負荷を適応的に削減するように構成される。突風補償システムが当該航空機の前面に近接する第１のセンサ１１０を含んでもよい。第１のセンサは、第１の信号を出力するように構成される。第２のセンサ１２０を当該航空機の前面１１３から遠位に配置してもよい。第２のセンサは、第２の信号を出力するように構成される。突風信号サブシステムは、第１の信号と第２の信号を受信し、第１の信号と第２の信号の分析に基づいて突風信号を生成するように構成される。突風信号サブシステムが当該突風信号を出力し、当該突風信号が負荷軽減閾値を超過したことに応答して負荷パラメータ信号を修正してもよい。【選択図】図１ |
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【課題】突風を補償するように航空機を効率的に構成するためのシステムおよび方法を提供すること【解決手段】突風補償システムは、航空機１００に作用する突風負荷を適応的に削減するように構成される。突風補償システムが当該航空機の前面に近接する第１のセンサ１１０を含んでもよい。第１のセンサは、第１の信号を出力するように構成される。第２のセンサ１２０を当該航空機の前面１１３から遠位に配置してもよい。第２のセンサは、第２の信号を出力するように構成される。突風信号サブシステムは、第１の信号と第２の信号を受信し、第１の信号と第２の信号の分析に基づいて突風信号を生成するように構成される。突風信号サブシステムが当該突風信号を出力し、当該突風信号が負荷軽減閾値を超過したことに応答して負荷パラメータ信号を修正してもよい。【選択図】図１</description><language>eng ; jpn</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; CONTROLLING ; COSMONAUTICS ; HELICOPTERS ; PERFORMING OPERATIONS ; PHYSICS ; REGULATING ; SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES ; TRANSPORTING</subject><creationdate>2017</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=20170105&DB=EPODOC&CC=JP&NR=2017001656A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76516</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20170105&DB=EPODOC&CC=JP&NR=2017001656A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>CHRISTOPHER D DALLARA</creatorcontrib><creatorcontrib>ALEXANDER C HO</creatorcontrib><creatorcontrib>YAMASHIRO HISAKO</creatorcontrib><creatorcontrib>RAFAEL E CAICEDO</creatorcontrib><creatorcontrib>PAUL C STREFLING</creatorcontrib><creatorcontrib>KIOUMARS NAJMABADI</creatorcontrib><creatorcontrib>TZE L SIU</creatorcontrib><creatorcontrib>KHALED ABDEL-MOTAGALY</creatorcontrib><title>GUST COMPENSATION SYSTEM AND METHOD FOR AIRCRAFT</title><description>PROBLEM TO BE SOLVED: To provide a system and method for efficiently configuring an aircraft to compensate for gusts.SOLUTION: A gust compensation system is configured to adaptively reduce gust loads exerted into an aircraft 100. The gust compensation system may include a first sensor 110 proximate to a front of the aircraft. The first sensor is configured to output a first signal. A second sensor 120 may be distally located from a front 113 of the aircraft. The second sensor is configured to output a second signal. A gust signal sub-system is configured to receive the first and second signals and generate a gust signal on the basis of analysis of the first and second signals. The gust signal sub-system outputs the gust signal and may modify a load parameter signal in response to the gust signal exceeding a load alleviation threshold.SELECTED DRAWING: Figure 1
【課題】突風を補償するように航空機を効率的に構成するためのシステムおよび方法を提供すること【解決手段】突風補償システムは、航空機１００に作用する突風負荷を適応的に削減するように構成される。突風補償システムが当該航空機の前面に近接する第１のセンサ１１０を含んでもよい。第１のセンサは、第１の信号を出力するように構成される。第２のセンサ１２０を当該航空機の前面１１３から遠位に配置してもよい。第２のセンサは、第２の信号を出力するように構成される。突風信号サブシステムは、第１の信号と第２の信号を受信し、第１の信号と第２の信号の分析に基づいて突風信号を生成するように構成される。突風信号サブシステムが当該突風信号を出力し、当該突風信号が負荷軽減閾値を超過したことに応答して負荷パラメータ信号を修正してもよい。【選択図】図１</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>CONTROLLING</subject><subject>COSMONAUTICS</subject><subject>HELICOPTERS</subject><subject>PERFORMING OPERATIONS</subject><subject>PHYSICS</subject><subject>REGULATING</subject><subject>SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2017</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZDBwDw0OUXD29w1w9Qt2DPH091MIjgwOcfVVcPRzUfB1DfHwd1Fw8w9ScPQMcg5ydAvhYWBNS8wpTuWF0twMSm6uIc4euqkF-fGpxQWJyal5qSXxXgFGBobmBgaGZqZmjsZEKQIAhFMmwg</recordid><startdate>20170105</startdate><enddate>20170105</enddate><creator>CHRISTOPHER D DALLARA</creator><creator>ALEXANDER C HO</creator><creator>YAMASHIRO HISAKO</creator><creator>RAFAEL E CAICEDO</creator><creator>PAUL C STREFLING</creator><creator>KIOUMARS NAJMABADI</creator><creator>TZE L SIU</creator><creator>KHALED ABDEL-MOTAGALY</creator><scope>EVB</scope></search><sort><creationdate>20170105</creationdate><title>GUST COMPENSATION SYSTEM AND METHOD FOR AIRCRAFT</title><author>CHRISTOPHER D DALLARA ; ALEXANDER C HO ; YAMASHIRO HISAKO ; RAFAEL E CAICEDO ; PAUL C STREFLING ; KIOUMARS NAJMABADI ; TZE L SIU ; KHALED ABDEL-MOTAGALY</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_JP2017001656A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; jpn</language><creationdate>2017</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>CONTROLLING</topic><topic>COSMONAUTICS</topic><topic>HELICOPTERS</topic><topic>PERFORMING OPERATIONS</topic><topic>PHYSICS</topic><topic>REGULATING</topic><topic>SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>CHRISTOPHER D DALLARA</creatorcontrib><creatorcontrib>ALEXANDER C HO</creatorcontrib><creatorcontrib>YAMASHIRO HISAKO</creatorcontrib><creatorcontrib>RAFAEL E CAICEDO</creatorcontrib><creatorcontrib>PAUL C STREFLING</creatorcontrib><creatorcontrib>KIOUMARS NAJMABADI</creatorcontrib><creatorcontrib>TZE L SIU</creatorcontrib><creatorcontrib>KHALED ABDEL-MOTAGALY</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>CHRISTOPHER D DALLARA</au><au>ALEXANDER C HO</au><au>YAMASHIRO HISAKO</au><au>RAFAEL E CAICEDO</au><au>PAUL C STREFLING</au><au>KIOUMARS NAJMABADI</au><au>TZE L SIU</au><au>KHALED ABDEL-MOTAGALY</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>GUST COMPENSATION SYSTEM AND METHOD FOR AIRCRAFT</title><date>2017-01-05</date><risdate>2017</risdate><abstract>PROBLEM TO BE SOLVED: To provide a system and method for efficiently configuring an aircraft to compensate for gusts.SOLUTION: A gust compensation system is configured to adaptively reduce gust loads exerted into an aircraft 100. The gust compensation system may include a first sensor 110 proximate to a front of the aircraft. The first sensor is configured to output a first signal. A second sensor 120 may be distally located from a front 113 of the aircraft. The second sensor is configured to output a second signal. A gust signal sub-system is configured to receive the first and second signals and generate a gust signal on the basis of analysis of the first and second signals. The gust signal sub-system outputs the gust signal and may modify a load parameter signal in response to the gust signal exceeding a load alleviation threshold.SELECTED DRAWING: Figure 1
【課題】突風を補償するように航空機を効率的に構成するためのシステムおよび方法を提供すること【解決手段】突風補償システムは、航空機１００に作用する突風負荷を適応的に削減するように構成される。突風補償システムが当該航空機の前面に近接する第１のセンサ１１０を含んでもよい。第１のセンサは、第１の信号を出力するように構成される。第２のセンサ１２０を当該航空機の前面１１３から遠位に配置してもよい。第２のセンサは、第２の信号を出力するように構成される。突風信号サブシステムは、第１の信号と第２の信号を受信し、第１の信号と第２の信号の分析に基づいて突風信号を生成するように構成される。突風信号サブシステムが当該突風信号を出力し、当該突風信号が負荷軽減閾値を超過したことに応答して負荷パラメータ信号を修正してもよい。【選択図】図１</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | AEROPLANES AIRCRAFT AVIATION CONTROLLING COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS PHYSICS REGULATING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES TRANSPORTING |
| title | GUST COMPENSATION SYSTEM AND METHOD FOR AIRCRAFT |
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