Thrust control lever
INVENTORS: BERND NEUD?RFFER, KLAUS ALEXANDER LANGNER, AND WOLFGANG KUMMLE INVENTION: CONTROL LEVER ASSEMBLY FOR SETTING ENGINE THRUST IN AN AIRCRAFT In a control lever assembly for setting the engine thrust in an aircraft with a control lever and a thrust control signal transmitter for generating di...
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creator | BERND NEUDOERFFER KLAUS ALEXANDER LANGNER WOLFGANG KUMMLE |
description | INVENTORS: BERND NEUD?RFFER, KLAUS ALEXANDER LANGNER, AND WOLFGANG KUMMLE INVENTION: CONTROL LEVER ASSEMBLY FOR SETTING ENGINE THRUST IN AN AIRCRAFT In a control lever assembly for setting the engine thrust in an aircraft with a control lever and a thrust control signal transmitter for generating discrete thrust settings, the thrust control signal transmitter is a high-resolution digital, optical absolute angle sensor, which is rigidly coupled with the control lever. The control lever assembly provides the various discrete thrust settings, when predetermined associated output data of the digital absolute angle sensor are reached. A particularly advantageous design of the optical absolute angle sensor is described. |
format | Patent |
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The control lever assembly provides the various discrete thrust settings, when predetermined associated output data of the digital absolute angle sensor are reached. A particularly advantageous design of the optical absolute angle sensor is described.</description><edition>6</edition><language>eng</language><subject>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 ; CONTROL DEVICES OR SYSTEMS INSOFAR AS CHARACTERISED BYMECHANICAL FEATURES ONLY ; CONTROLLING ; COSMONAUTICS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; MEASURING ; MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE ; MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR ; PARACHUTES ; PERFORMING OPERATIONS ; PHYSICS ; REGULATING ; TARIFF METERING APPARATUS ; TESTING ; TRANSPORTING</subject><creationdate>1995</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=19950322&DB=EPODOC&CC=GB&NR=2281882A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=19950322&DB=EPODOC&CC=GB&NR=2281882A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>BERND NEUDOERFFER</creatorcontrib><creatorcontrib>KLAUS ALEXANDER LANGNER</creatorcontrib><creatorcontrib>WOLFGANG KUMMLE</creatorcontrib><title>Thrust control lever</title><description>INVENTORS: BERND NEUD?RFFER, KLAUS ALEXANDER LANGNER, AND WOLFGANG KUMMLE INVENTION: CONTROL LEVER ASSEMBLY FOR SETTING ENGINE THRUST IN AN AIRCRAFT In a control lever assembly for setting the engine thrust in an aircraft with a control lever and a thrust control signal transmitter for generating discrete thrust settings, the thrust control signal transmitter is a high-resolution digital, optical absolute angle sensor, which is rigidly coupled with the control lever. The control lever assembly provides the various discrete thrust settings, when predetermined associated output data of the digital absolute angle sensor are reached. 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The control lever assembly provides the various discrete thrust settings, when predetermined associated output data of the digital absolute angle sensor are reached. A particularly advantageous design of the optical absolute angle sensor is described.</abstract><edition>6</edition><oa>free_for_read</oa></addata></record> |
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subjects | 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 CONTROL DEVICES OR SYSTEMS INSOFAR AS CHARACTERISED BYMECHANICAL FEATURES ONLY CONTROLLING COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS MEASURING MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR PARACHUTES PERFORMING OPERATIONS PHYSICS REGULATING TARIFF METERING APPARATUS TESTING TRANSPORTING |
title | Thrust control lever |
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