Equations for a preliminary actuator design

Please use this identifier to cite or link to this item: https://doi.org/10.48441/4427.3818

Publisher URL:	https://www.fzt.haw-hamburg.de/pers/Scholz/paper/TN-EV52-360_91.pdf
Title:	Equations for a preliminary actuator design
Language:	English
Authors:	Scholz, Dieter
metadata.local.contributorCorporate.other:	Airbus Operations GmbH
Keywords:	aviation; airplane; aircraft; aeronautical engineering; system; flight control; actuator; system design; installation; hinge moment; valve; servo valve
Issue Date:	7-Oct-2026
Publisher:	Deutsche Airbus
Abstract:	This Technical Note summarizes equations used for a preliminary actuator design. The equations can be applied for the preliminary design of elevator, aileron, rudder, THS, and spoiler actuators.
URI:	http://hdl.handle.net/20.500.12738/12675
DOI:	10.48441/4427.3818
Review status:	Currently there is no review planned for this version
Institute:	Forschungsgruppe Flugzeugentwurf und -systeme (AERO) Fakultät Luftfahrt- und Fahrzeugsysteme
Type:	Report
Additional note:	SCHOLZ, Dieter, 2026. Equations for a Preliminary Actuator Design. Technical Note. Originally written at Deutsche Airbus in 1991; updated at Hamburg University of Applied Sciences (HAW Hamburg) in 2026. Hamburg: HAW Hamburg. Available from: http://hdl.handle.net/20.500.12738/12675
Appears in Collections:	Publications with full text