INDUCTIVE GUST SENSOR
Die Erfindung betrifft ein Windfahnenelement (10) mit einer Windfahne (12), das sich nach der Windrichtung ausrichtet, mit einem Drehwinkelaufnehmer (18), der eine Winkelstellung der Windfahne (12) als Messsignal bereitstellt, wobei der Drehwinkelaufnehmer (18) berührungslos arbeitet. The invention...
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| creator | STEIGENBERGER, JOSEF WILDSCHEK, ANDREAS |
| description | Die Erfindung betrifft ein Windfahnenelement (10) mit einer Windfahne (12), das sich nach der Windrichtung ausrichtet, mit einem Drehwinkelaufnehmer (18), der eine Winkelstellung der Windfahne (12) als Messsignal bereitstellt, wobei der Drehwinkelaufnehmer (18) berührungslos arbeitet.
The invention relates to a wind vane element (10) having a wind vane (12), which is oriented according to the wind direction, and having a rotation angle sensor (18) which provides an angular position of the wind vane (12) as a measurement signal, wherein the rotation angle sensor (18) operates in a contactless manner.
La présente invention concerne un élément à girouette (10) qui comprend une girouette (12) et est orienté selon la direction du vent, l'élément comprenant un capteur d'angle de rotation (18) qui indique une position angulaire de la girouette (12) sous la forme d'un signal de mesure, le capteur d'angle de rotation (18) fonctionnant sans contact. |
| format | Patent |
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The invention relates to a wind vane element (10) having a wind vane (12), which is oriented according to the wind direction, and having a rotation angle sensor (18) which provides an angular position of the wind vane (12) as a measurement signal, wherein the rotation angle sensor (18) operates in a contactless manner.
La présente invention concerne un élément à girouette (10) qui comprend une girouette (12) et est orienté selon la direction du vent, l'élément comprenant un capteur d'angle de rotation (18) qui indique une position angulaire de la girouette (12) sous la forme d'un signal de mesure, le capteur d'angle de rotation (18) fonctionnant sans contact.</description><language>eng ; fre ; ger</language><subject>AEROPLANES ; AIRCRAFT ; ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVEREDIN A SINGLE OTHER SUBCLASS ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; COSMONAUTICS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; HELICOPTERS ; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT ; MEASURING ; MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION,OR SHOCK ; MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE ; MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR ; PARACHUTES ; PERFORMING OPERATIONS ; PHYSICS ; TARIFF METERING APPARATUS ; TESTING ; TRANSPORTING</subject><creationdate>2009</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=20090129&DB=EPODOC&CC=WO&NR=2009013326A2$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20090129&DB=EPODOC&CC=WO&NR=2009013326A2$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>STEIGENBERGER, JOSEF</creatorcontrib><creatorcontrib>WILDSCHEK, ANDREAS</creatorcontrib><title>INDUCTIVE GUST SENSOR</title><description>Die Erfindung betrifft ein Windfahnenelement (10) mit einer Windfahne (12), das sich nach der Windrichtung ausrichtet, mit einem Drehwinkelaufnehmer (18), der eine Winkelstellung der Windfahne (12) als Messsignal bereitstellt, wobei der Drehwinkelaufnehmer (18) berührungslos arbeitet.
The invention relates to a wind vane element (10) having a wind vane (12), which is oriented according to the wind direction, and having a rotation angle sensor (18) which provides an angular position of the wind vane (12) as a measurement signal, wherein the rotation angle sensor (18) operates in a contactless manner.
La présente invention concerne un élément à girouette (10) qui comprend une girouette (12) et est orienté selon la direction du vent, l'élément comprenant un capteur d'angle de rotation (18) qui indique une position angulaire de la girouette (12) sous la forme d'un signal de mesure, le capteur d'angle de rotation (18) fonctionnant sans contact.</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVEREDIN A SINGLE OTHER SUBCLASS</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>HELICOPTERS</subject><subject>INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT</subject><subject>MEASURING</subject><subject>MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION,OR SHOCK</subject><subject>MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE</subject><subject>MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>PHYSICS</subject><subject>TARIFF METERING APPARATUS</subject><subject>TESTING</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2009</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZBD19HMJdQ7xDHNVcA8NDlEIdvUL9g_iYWBNS8wpTuWF0twMym6uIc4euqkF-fGpxQWJyal5qSXx4f5GBgaWBobGxkZmjkbGxKkCACFLH-o</recordid><startdate>20090129</startdate><enddate>20090129</enddate><creator>STEIGENBERGER, JOSEF</creator><creator>WILDSCHEK, ANDREAS</creator><scope>EVB</scope></search><sort><creationdate>20090129</creationdate><title>INDUCTIVE GUST SENSOR</title><author>STEIGENBERGER, JOSEF ; WILDSCHEK, ANDREAS</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_WO2009013326A23</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2009</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVEREDIN A SINGLE OTHER SUBCLASS</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>HELICOPTERS</topic><topic>INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT</topic><topic>MEASURING</topic><topic>MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION,OR SHOCK</topic><topic>MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE</topic><topic>MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>PHYSICS</topic><topic>TARIFF METERING APPARATUS</topic><topic>TESTING</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>STEIGENBERGER, JOSEF</creatorcontrib><creatorcontrib>WILDSCHEK, ANDREAS</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>STEIGENBERGER, JOSEF</au><au>WILDSCHEK, ANDREAS</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>INDUCTIVE GUST SENSOR</title><date>2009-01-29</date><risdate>2009</risdate><abstract>Die Erfindung betrifft ein Windfahnenelement (10) mit einer Windfahne (12), das sich nach der Windrichtung ausrichtet, mit einem Drehwinkelaufnehmer (18), der eine Winkelstellung der Windfahne (12) als Messsignal bereitstellt, wobei der Drehwinkelaufnehmer (18) berührungslos arbeitet.
The invention relates to a wind vane element (10) having a wind vane (12), which is oriented according to the wind direction, and having a rotation angle sensor (18) which provides an angular position of the wind vane (12) as a measurement signal, wherein the rotation angle sensor (18) operates in a contactless manner.
La présente invention concerne un élément à girouette (10) qui comprend une girouette (12) et est orienté selon la direction du vent, l'élément comprenant un capteur d'angle de rotation (18) qui indique une position angulaire de la girouette (12) sous la forme d'un signal de mesure, le capteur d'angle de rotation (18) fonctionnant sans contact.</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | AEROPLANES AIRCRAFT ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVEREDIN A SINGLE OTHER SUBCLASS ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HELICOPTERS INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT MEASURING MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION,OR SHOCK MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR PARACHUTES PERFORMING OPERATIONS PHYSICS TARIFF METERING APPARATUS TESTING TRANSPORTING |
| title | INDUCTIVE GUST SENSOR |
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