SYSTEM AND METHOD FOR LINKAGE LENGTH ADJUSTMENT
A rotor system has a rotor (302), an axis of rotation about which the rotor (302) may be rotated, a linkage system (310) having a first adjustable length portion (210) and a second adjustable length portion (212), wherein the second adjustable length portion (212) is configured to provide a relative...
Gespeichert in:
| 1. Verfasser: | |
|---|---|
| Format: | Patent |
| Sprache: | eng ; fre |
| Schlagworte: | |
| Online-Zugang: | Volltext bestellen |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| container_end_page | |
|---|---|
| container_issue | |
| container_start_page | |
| container_title | |
| container_volume | |
| creator | WIINIKKA, MARK A |
| description | A rotor system has a rotor (302), an axis of rotation about which the rotor (302) may be rotated, a linkage system (310) having a first adjustable length portion (210) and a second adjustable length portion (212), wherein the second adjustable length portion (212) is configured to provide a relatively finer adjustment of an overall effective length of the linkage system (310) as compared to the first adjustable length portion (210) and wherein the rotor (302) is configured to rotate about the axis in response to changing the overall effective length of the linkage system (310).
Système de rotor possédant un rotor (302), un axe de rotation autour duquel le rotor (302) peut tourner, un système de tringlerie (310) possédant une première partie à longueur réglable (210) et une seconde partie à longueur réglable (212), la seconde partie à longueur réglable (212) étant configurée pour permettre un réglage relativement plus précis d'une longueur réelle générale du système de tringlerie (310) que la première partie à longueur réglable (210) et le rotor (302) étant configuré pour tourner autour de l'axe en réaction au changement de la longueur réelle générale du système de tringlerie (310). |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_WO2014100655A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>WO2014100655A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_WO2014100655A13</originalsourceid><addsrcrecordid>eNrjZNAPjgwOcfVVcPRzUfB1DfHwd1Fw8w9S8PH083Z0d1XwcfVzD_FQcHTxCg0O8XX1C-FhYE1LzClO5YXS3AzKbq4hzh66qQX58anFBYnJqXmpJfHh_kYGhiaGBgZmpqaOhsbEqQIAlp4m0g</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>SYSTEM AND METHOD FOR LINKAGE LENGTH ADJUSTMENT</title><source>esp@cenet</source><creator>WIINIKKA, MARK A</creator><creatorcontrib>WIINIKKA, MARK A</creatorcontrib><description>A rotor system has a rotor (302), an axis of rotation about which the rotor (302) may be rotated, a linkage system (310) having a first adjustable length portion (210) and a second adjustable length portion (212), wherein the second adjustable length portion (212) is configured to provide a relatively finer adjustment of an overall effective length of the linkage system (310) as compared to the first adjustable length portion (210) and wherein the rotor (302) is configured to rotate about the axis in response to changing the overall effective length of the linkage system (310).
Système de rotor possédant un rotor (302), un axe de rotation autour duquel le rotor (302) peut tourner, un système de tringlerie (310) possédant une première partie à longueur réglable (210) et une seconde partie à longueur réglable (212), la seconde partie à longueur réglable (212) étant configurée pour permettre un réglage relativement plus précis d'une longueur réelle générale du système de tringlerie (310) que la première partie à longueur réglable (210) et le rotor (302) étant configuré pour tourner autour de l'axe en réaction au changement de la longueur réelle générale du système de tringlerie (310).</description><language>eng ; fre</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; BEARINGS ; BLASTING ; COSMONAUTICS ; ELEMENTS OR CRANKSHAFT MECHANISMS ; ENGINEERING ELEMENTS AND UNITS ; FLEXIBLE SHAFTS ; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS ; HEATING ; HELICOPTERS ; LIGHTING ; MECHANICAL ENGINEERING ; PERFORMING OPERATIONS ; ROTARY BODIES OTHER THAN GEARING ELEMENTS ; SHAFTS ; THERMAL INSULATION IN GENERAL ; TRANSPORTING ; WEAPONS</subject><creationdate>2014</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=20140626&DB=EPODOC&CC=WO&NR=2014100655A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20140626&DB=EPODOC&CC=WO&NR=2014100655A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>WIINIKKA, MARK A</creatorcontrib><title>SYSTEM AND METHOD FOR LINKAGE LENGTH ADJUSTMENT</title><description>A rotor system has a rotor (302), an axis of rotation about which the rotor (302) may be rotated, a linkage system (310) having a first adjustable length portion (210) and a second adjustable length portion (212), wherein the second adjustable length portion (212) is configured to provide a relatively finer adjustment of an overall effective length of the linkage system (310) as compared to the first adjustable length portion (210) and wherein the rotor (302) is configured to rotate about the axis in response to changing the overall effective length of the linkage system (310).
Système de rotor possédant un rotor (302), un axe de rotation autour duquel le rotor (302) peut tourner, un système de tringlerie (310) possédant une première partie à longueur réglable (210) et une seconde partie à longueur réglable (212), la seconde partie à longueur réglable (212) étant configurée pour permettre un réglage relativement plus précis d'une longueur réelle générale du système de tringlerie (310) que la première partie à longueur réglable (210) et le rotor (302) étant configuré pour tourner autour de l'axe en réaction au changement de la longueur réelle générale du système de tringlerie (310).</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>BEARINGS</subject><subject>BLASTING</subject><subject>COSMONAUTICS</subject><subject>ELEMENTS OR CRANKSHAFT MECHANISMS</subject><subject>ENGINEERING ELEMENTS AND UNITS</subject><subject>FLEXIBLE SHAFTS</subject><subject>GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS</subject><subject>HEATING</subject><subject>HELICOPTERS</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>PERFORMING OPERATIONS</subject><subject>ROTARY BODIES OTHER THAN GEARING ELEMENTS</subject><subject>SHAFTS</subject><subject>THERMAL INSULATION IN GENERAL</subject><subject>TRANSPORTING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2014</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZNAPjgwOcfVVcPRzUfB1DfHwd1Fw8w9S8PH083Z0d1XwcfVzD_FQcHTxCg0O8XX1C-FhYE1LzClO5YXS3AzKbq4hzh66qQX58anFBYnJqXmpJfHh_kYGhiaGBgZmpqaOhsbEqQIAlp4m0g</recordid><startdate>20140626</startdate><enddate>20140626</enddate><creator>WIINIKKA, MARK A</creator><scope>EVB</scope></search><sort><creationdate>20140626</creationdate><title>SYSTEM AND METHOD FOR LINKAGE LENGTH ADJUSTMENT</title><author>WIINIKKA, MARK A</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_WO2014100655A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre</language><creationdate>2014</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>BEARINGS</topic><topic>BLASTING</topic><topic>COSMONAUTICS</topic><topic>ELEMENTS OR CRANKSHAFT MECHANISMS</topic><topic>ENGINEERING ELEMENTS AND UNITS</topic><topic>FLEXIBLE SHAFTS</topic><topic>GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS</topic><topic>HEATING</topic><topic>HELICOPTERS</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>PERFORMING OPERATIONS</topic><topic>ROTARY BODIES OTHER THAN GEARING ELEMENTS</topic><topic>SHAFTS</topic><topic>THERMAL INSULATION IN GENERAL</topic><topic>TRANSPORTING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>WIINIKKA, MARK A</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>WIINIKKA, MARK A</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>SYSTEM AND METHOD FOR LINKAGE LENGTH ADJUSTMENT</title><date>2014-06-26</date><risdate>2014</risdate><abstract>A rotor system has a rotor (302), an axis of rotation about which the rotor (302) may be rotated, a linkage system (310) having a first adjustable length portion (210) and a second adjustable length portion (212), wherein the second adjustable length portion (212) is configured to provide a relatively finer adjustment of an overall effective length of the linkage system (310) as compared to the first adjustable length portion (210) and wherein the rotor (302) is configured to rotate about the axis in response to changing the overall effective length of the linkage system (310).
Système de rotor possédant un rotor (302), un axe de rotation autour duquel le rotor (302) peut tourner, un système de tringlerie (310) possédant une première partie à longueur réglable (210) et une seconde partie à longueur réglable (212), la seconde partie à longueur réglable (212) étant configurée pour permettre un réglage relativement plus précis d'une longueur réelle générale du système de tringlerie (310) que la première partie à longueur réglable (210) et le rotor (302) étant configuré pour tourner autour de l'axe en réaction au changement de la longueur réelle générale du système de tringlerie (310).</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | eng ; fre |
| recordid | cdi_epo_espacenet_WO2014100655A1 |
| source | esp@cenet |
| subjects | AEROPLANES AIRCRAFT AVIATION BEARINGS BLASTING COSMONAUTICS ELEMENTS OR CRANKSHAFT MECHANISMS ENGINEERING ELEMENTS AND UNITS FLEXIBLE SHAFTS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING HELICOPTERS LIGHTING MECHANICAL ENGINEERING PERFORMING OPERATIONS ROTARY BODIES OTHER THAN GEARING ELEMENTS SHAFTS THERMAL INSULATION IN GENERAL TRANSPORTING WEAPONS |
| title | SYSTEM AND METHOD FOR LINKAGE LENGTH ADJUSTMENT |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-28T20%3A21%3A35IST&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=WIINIKKA,%20MARK%20A&rft.date=2014-06-26&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EWO2014100655A1%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 |