TRANSLATIONAL WING AIRCRAFT
PROBLEM TO BE SOLVED: To provide a translational wing aircraft simplifying mechanism, reducing weight, improving reliability, and reducing a manufacturing cost. SOLUTION: This translational wing aircraft employs a method for controlling output not by pitch angle control but by rotational speed contr...
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| creator | KUBOMURA KENJI UCHIDA TAKASHI |
| description | PROBLEM TO BE SOLVED: To provide a translational wing aircraft simplifying mechanism, reducing weight, improving reliability, and reducing a manufacturing cost. SOLUTION: This translational wing aircraft employs a method for controlling output not by pitch angle control but by rotational speed control, a method for positioning a blade by pinching the upper part of one guide plate by more than one roller, and a method for changing a pitch angle by changing the angles of two arms installed fixedly on a blade shaft when pitch angle control is unescapable. COPYRIGHT: (C)2007,JPO&INPIT |
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COPYRIGHT: (C)2007,JPO&INPIT</description><language>eng</language><subject>BLASTING ; HEATING ; LIGHTING ; MACHINES OR ENGINES FOR LIQUIDS ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT PUMPS ; OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR ; POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS ; PRODUCING MECHANICAL POWER ; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS ; WEAPONS ; WIND MOTORS ; WIND, SPRING WEIGHT AND MISCELLANEOUS MOTORS</subject><creationdate>2006</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=20061026&DB=EPODOC&CC=JP&NR=2006291796A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20061026&DB=EPODOC&CC=JP&NR=2006291796A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>KUBOMURA KENJI</creatorcontrib><creatorcontrib>UCHIDA TAKASHI</creatorcontrib><title>TRANSLATIONAL WING AIRCRAFT</title><description>PROBLEM TO BE SOLVED: To provide a translational wing aircraft simplifying mechanism, reducing weight, improving reliability, and reducing a manufacturing cost. 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SOLUTION: This translational wing aircraft employs a method for controlling output not by pitch angle control but by rotational speed control, a method for positioning a blade by pinching the upper part of one guide plate by more than one roller, and a method for changing a pitch angle by changing the angles of two arms installed fixedly on a blade shaft when pitch angle control is unescapable. COPYRIGHT: (C)2007,JPO&INPIT</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng |
| recordid | cdi_epo_espacenet_JP2006291796A |
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| subjects | BLASTING HEATING LIGHTING MACHINES OR ENGINES FOR LIQUIDS MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT PUMPS OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PRODUCING MECHANICAL POWER PUMPS FOR LIQUIDS OR ELASTIC FLUIDS WEAPONS WIND MOTORS WIND, SPRING WEIGHT AND MISCELLANEOUS MOTORS |
| title | TRANSLATIONAL WING AIRCRAFT |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-28T21%3A01%3A40IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-epo_EVB&rft_val_fmt=info:ofi/fmt:kev:mtx:patent&rft.genre=patent&rft.au=KUBOMURA%20KENJI&rft.date=2006-10-26&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EJP2006291796A%3C/epo_EVB%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true |