AIRFRAME POSITION ADJUSTING STRUCTURE
Provided is an airframe position adjusting structure capable of adjusting the position of an airframe (A) inclined laterally. The airframe position adjusting structure (1) is made such that a component force (FV), as taken in the vertical directions of the airframe, of a ground reaction force (F) to...
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| creator | ITAKURA, EIJI |
| description | Provided is an airframe position adjusting structure capable of adjusting the position of an airframe (A) inclined laterally. The airframe position adjusting structure (1) is made such that a component force (FV), as taken in the vertical directions of the airframe, of a ground reaction force (F) to be received from the ground (G) may be the higher as the rolling angle (f) at the grounding time of the airframe (A) becomes the larger. The airframe vertical component force (FV) of the ground reaction force (F) acts as a force to return the airframe (A) to a horizontal position so that the laterally inclined position of the airframe (A) can be adjusted when the airframe (A) grounds.
L'invention concerne une structure d'ajustement de la position d'une cellule capable d'ajuster la position d'une cellule (A) inclinée latéralement. La structure d'ajustement de la position d'une cellule (1) est réalisée de telle sorte qu'une composante de force (FV), dans la direction verticale de la cellule, d'une force de réaction du sol (F) reçue du sol (G) puisse être supérieure quand l'angle de roulis (f) au moment de l'atterrissage de la cellule (A) augmente. La composante de force verticale de la cellule (FV) de la force de réaction du sol (F) sert de force pour remettre la cellule (A) dans une position horizontale de telle sorte que la position latéralement inclinée de la cellule (A) puisse être ajustée quand la cellule (A) atterrit. |
| format | Patent |
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L'invention concerne une structure d'ajustement de la position d'une cellule capable d'ajuster la position d'une cellule (A) inclinée latéralement. La structure d'ajustement de la position d'une cellule (1) est réalisée de telle sorte qu'une composante de force (FV), dans la direction verticale de la cellule, d'une force de réaction du sol (F) reçue du sol (G) puisse être supérieure quand l'angle de roulis (f) au moment de l'atterrissage de la cellule (A) augmente. La composante de force verticale de la cellule (FV) de la force de réaction du sol (F) sert de force pour remettre la cellule (A) dans une position horizontale de telle sorte que la position latéralement inclinée de la cellule (A) puisse être ajustée quand la cellule (A) atterrit.</description><language>eng ; fre ; jpn</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; COSMONAUTICS ; HELICOPTERS ; PERFORMING OPERATIONS ; TRANSPORTING</subject><creationdate>2010</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=20100826&DB=EPODOC&CC=WO&NR=2010095261A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20100826&DB=EPODOC&CC=WO&NR=2010095261A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>ITAKURA, EIJI</creatorcontrib><title>AIRFRAME POSITION ADJUSTING STRUCTURE</title><description>Provided is an airframe position adjusting structure capable of adjusting the position of an airframe (A) inclined laterally. The airframe position adjusting structure (1) is made such that a component force (FV), as taken in the vertical directions of the airframe, of a ground reaction force (F) to be received from the ground (G) may be the higher as the rolling angle (f) at the grounding time of the airframe (A) becomes the larger. The airframe vertical component force (FV) of the ground reaction force (F) acts as a force to return the airframe (A) to a horizontal position so that the laterally inclined position of the airframe (A) can be adjusted when the airframe (A) grounds.
L'invention concerne une structure d'ajustement de la position d'une cellule capable d'ajuster la position d'une cellule (A) inclinée latéralement. La structure d'ajustement de la position d'une cellule (1) est réalisée de telle sorte qu'une composante de force (FV), dans la direction verticale de la cellule, d'une force de réaction du sol (F) reçue du sol (G) puisse être supérieure quand l'angle de roulis (f) au moment de l'atterrissage de la cellule (A) augmente. La composante de force verticale de la cellule (FV) de la force de réaction du sol (F) sert de force pour remettre la cellule (A) dans une position horizontale de telle sorte que la position latéralement inclinée de la cellule (A) puisse être ajustée quand la cellule (A) atterrit.</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>2010</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZFB19AxyC3L0dVUI8A_2DPH091NwdPEKDQ7x9HNXCA4JCnUOCQ1y5WFgTUvMKU7lhdLcDMpuriHOHrqpBfnxqcUFicmpeakl8eH-RgaGBgaWpkZmho6GxsSpAgBSNCSG</recordid><startdate>20100826</startdate><enddate>20100826</enddate><creator>ITAKURA, EIJI</creator><scope>EVB</scope></search><sort><creationdate>20100826</creationdate><title>AIRFRAME POSITION ADJUSTING STRUCTURE</title><author>ITAKURA, EIJI</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_WO2010095261A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; jpn</language><creationdate>2010</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>ITAKURA, EIJI</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>ITAKURA, EIJI</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>AIRFRAME POSITION ADJUSTING STRUCTURE</title><date>2010-08-26</date><risdate>2010</risdate><abstract>Provided is an airframe position adjusting structure capable of adjusting the position of an airframe (A) inclined laterally. The airframe position adjusting structure (1) is made such that a component force (FV), as taken in the vertical directions of the airframe, of a ground reaction force (F) to be received from the ground (G) may be the higher as the rolling angle (f) at the grounding time of the airframe (A) becomes the larger. The airframe vertical component force (FV) of the ground reaction force (F) acts as a force to return the airframe (A) to a horizontal position so that the laterally inclined position of the airframe (A) can be adjusted when the airframe (A) grounds.
L'invention concerne une structure d'ajustement de la position d'une cellule capable d'ajuster la position d'une cellule (A) inclinée latéralement. La structure d'ajustement de la position d'une cellule (1) est réalisée de telle sorte qu'une composante de force (FV), dans la direction verticale de la cellule, d'une force de réaction du sol (F) reçue du sol (G) puisse être supérieure quand l'angle de roulis (f) au moment de l'atterrissage de la cellule (A) augmente. La composante de force verticale de la cellule (FV) de la force de réaction du sol (F) sert de force pour remettre la cellule (A) dans une position horizontale de telle sorte que la position latéralement inclinée de la cellule (A) puisse être ajustée quand la cellule (A) atterrit.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre ; jpn |
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| subjects | AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING |
| title | AIRFRAME POSITION ADJUSTING STRUCTURE |
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