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Robustness of the Liebherr-Aerospace EHA Technology for future flight control application

Future more electric aircraft (MEA) architectures require a new generation of power-by-wire actuators, e.g. Electro Hydrostatic Actuators (EHA). These units have to be capable of frontline operation of safety critical flight control surfaces over the entire aircraft life. Prove of robustness becomes a challenging objective. This paper illustrates the Liebherr-Aerospace EHA technology as well as methods for validation of robustness. It gives an insight regarding the design of a robust piston pump.

Identiferoai:union.ndltd.org:DRESDEN/oai:qucosa:de:qucosa:71210
Date25 June 2020
CreatorsRöben, Tobias, Viennet, Emmanuel, Wider, Henry
ContributorsDresdner Verein zur Förderung der Fluidtechnik e. V. Dresden
PublisherTechnische Universität Dresden
Source SetsHochschulschriftenserver (HSSS) der SLUB Dresden
LanguageEnglish
Detected LanguageEnglish
Typeinfo:eu-repo/semantics/publishedVersion, doc-type:conferenceObject, info:eu-repo/semantics/conferenceObject, doc-type:Text
Rightsinfo:eu-repo/semantics/openAccess
Relation10.25368/2020.7, urn:nbn:de:bsz:14-qucosa2-709173, qucosa:70917

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