Trailing edge actuator system and associated method

A trailing edge system for an aircraft may include a trailing edge 202 element mounted to a trailing edge. An electric motor actuator 300 having an electric motor may be configured to actuate the trailing edge element. A linkage system 360 may couple the electric motor actuator to the trailing edge...

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Bibliographic Details
Main Authors FINN, MICHAEL R, MOSER, MATTHEW A
Format Patent
LanguageEnglish
French
German
Published 25.03.2015
Subjects
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Abstract A trailing edge system for an aircraft may include a trailing edge 202 element mounted to a trailing edge. An electric motor actuator 300 having an electric motor may be configured to actuate the trailing edge element. A linkage system 360 may couple the electric motor actuator to the trailing edge element for actuation thereof.
AbstractList A trailing edge system for an aircraft may include a trailing edge 202 element mounted to a trailing edge. An electric motor actuator 300 having an electric motor may be configured to actuate the trailing edge element. A linkage system 360 may couple the electric motor actuator to the trailing edge element for actuation thereof.
Author FINN, MICHAEL R
MOSER, MATTHEW A
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DocumentTitleAlternate Système d'actionneur de bord de fuite et procédé associé
Hinterkantenaktuatorsystem und -verfahren
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Snippet A trailing edge system for an aircraft may include a trailing edge 202 element mounted to a trailing edge. An electric motor actuator 300 having an electric...
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SourceType Open Access Repository
SubjectTerms AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
Title Trailing edge actuator system and associated method
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