PASSIVE ROTOR PITCH CONTROL SYSTEM
One example includes a passive rotor pitch control system. The system includes a counterweights that are each associated with one of a respective plurality of rotors and can be arranged to have a center of mass configured to provide a pitch torque about a pitch axis associated with the respective on...
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creator | GALLMAN, JUDITH MARIE FLEMING, JONATHAN LEE LOOS, ERIC STEPHEN TALBERT, ROBERT FRANCIS |
description | One example includes a passive rotor pitch control system. The system includes a counterweights that are each associated with one of a respective plurality of rotors and can be arranged to have a center of mass configured to provide a pitch torque about a pitch axis associated with the respective one of the rotors in response to rotation of the rotors about a rotation axis. The system also includes a spring forcer comprising a pitch rod and a spring configured to provide a spring force on the pitch rod. The system further includes a pitch change assembly coupled to the counterweights and the pitch rod. The pitch change assembly can be configured to rotate a pitch of each of the rotors from a first pitch state to a second pitch state in response to a sum of pitch torques associated with the counterweights being greater than the spring force. |
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The system includes a counterweights that are each associated with one of a respective plurality of rotors and can be arranged to have a center of mass configured to provide a pitch torque about a pitch axis associated with the respective one of the rotors in response to rotation of the rotors about a rotation axis. The system also includes a spring forcer comprising a pitch rod and a spring configured to provide a spring force on the pitch rod. The system further includes a pitch change assembly coupled to the counterweights and the pitch rod. The pitch change assembly can be configured to rotate a pitch of each of the rotors from a first pitch state to a second pitch state in response to a sum of pitch torques associated with the counterweights being greater than the spring force.</description><language>eng</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; COSMONAUTICS ; HELICOPTERS ; PERFORMING OPERATIONS ; TRANSPORTING</subject><creationdate>2024</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=20240919&DB=EPODOC&CC=US&NR=2024308646A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25555,76308</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20240919&DB=EPODOC&CC=US&NR=2024308646A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>GALLMAN, JUDITH MARIE</creatorcontrib><creatorcontrib>FLEMING, JONATHAN LEE</creatorcontrib><creatorcontrib>LOOS, ERIC STEPHEN</creatorcontrib><creatorcontrib>TALBERT, ROBERT FRANCIS</creatorcontrib><title>PASSIVE ROTOR PITCH CONTROL SYSTEM</title><description>One example includes a passive rotor pitch control system. The system includes a counterweights that are each associated with one of a respective plurality of rotors and can be arranged to have a center of mass configured to provide a pitch torque about a pitch axis associated with the respective one of the rotors in response to rotation of the rotors about a rotation axis. The system also includes a spring forcer comprising a pitch rod and a spring configured to provide a spring force on the pitch rod. The system further includes a pitch change assembly coupled to the counterweights and the pitch rod. The pitch change assembly can be configured to rotate a pitch of each of the rotors from a first pitch state to a second pitch state in response to a sum of pitch torques associated with the counterweights being greater than the spring force.</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>2024</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZFAKcAwO9gxzVQjyD_EPUgjwDHH2UHD29wsJ8vdRCI4MDnH15WFgTUvMKU7lhdLcDMpurkBluqkF-fGpxQWJyal5qSXxocFGBkYmxgYWZiZmjobGxKkCAOIyI7I</recordid><startdate>20240919</startdate><enddate>20240919</enddate><creator>GALLMAN, JUDITH MARIE</creator><creator>FLEMING, JONATHAN LEE</creator><creator>LOOS, ERIC STEPHEN</creator><creator>TALBERT, ROBERT FRANCIS</creator><scope>EVB</scope></search><sort><creationdate>20240919</creationdate><title>PASSIVE ROTOR PITCH CONTROL SYSTEM</title><author>GALLMAN, JUDITH MARIE ; FLEMING, JONATHAN LEE ; LOOS, ERIC STEPHEN ; TALBERT, ROBERT FRANCIS</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US2024308646A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2024</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>GALLMAN, JUDITH MARIE</creatorcontrib><creatorcontrib>FLEMING, JONATHAN LEE</creatorcontrib><creatorcontrib>LOOS, ERIC STEPHEN</creatorcontrib><creatorcontrib>TALBERT, ROBERT FRANCIS</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>GALLMAN, JUDITH MARIE</au><au>FLEMING, JONATHAN LEE</au><au>LOOS, ERIC STEPHEN</au><au>TALBERT, ROBERT FRANCIS</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>PASSIVE ROTOR PITCH CONTROL SYSTEM</title><date>2024-09-19</date><risdate>2024</risdate><abstract>One example includes a passive rotor pitch control system. The system includes a counterweights that are each associated with one of a respective plurality of rotors and can be arranged to have a center of mass configured to provide a pitch torque about a pitch axis associated with the respective one of the rotors in response to rotation of the rotors about a rotation axis. The system also includes a spring forcer comprising a pitch rod and a spring configured to provide a spring force on the pitch rod. The system further includes a pitch change assembly coupled to the counterweights and the pitch rod. The pitch change assembly can be configured to rotate a pitch of each of the rotors from a first pitch state to a second pitch state in response to a sum of pitch torques associated with the counterweights being greater than the spring force.</abstract><oa>free_for_read</oa></addata></record> |
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subjects | AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING |
title | PASSIVE ROTOR PITCH CONTROL SYSTEM |
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