Composition and Parametrization of a Digital Twin of a Propeller Control System using Physical Modelling | Research Square window.SnipcartSettings = { analytics: { enabled: false } }; (function() { var accessVector = localStorage.getItem('access_vector') || ''; window.dataLayer = window.dataLayer || []; if (accessVector) { window.dataLayer.push({ user: { profile: { profileInfo: { snid: accessVector } } } }); } })(); (function(w,d,s,l,i){w[l]=w[l]||[];w[l].push({'gtm.start':new Date().getTime(),event:'gtm.js'});var f=d.getElementsByTagName(s)[0],j=d.createElement(s),dl=l!='dataLayer'?'&l='+l:'';j.async=true;j.src='https://www.googletagmanager.com/gtm.js?id='+i+dl;f.parentNode.insertBefore(j,f);})(window,document,'script','dataLayer','GTM-K279D39R'); Browse Preprints In Review Journals COVID-19 Preprints AJE Video Bytes Research Tools Research Promotion AJE Professional Editing AJE Rubriq About Preprint Platform In Review Editorial Policies Our Team Advisory Board Help Center Sign In Submit a Preprint Cite Share Download PDF Research Article Composition and Parametrization of a Digital Twin of a Propeller Control System using Physical Modelling Andres Lopez Pulzovan, Rudy Cepeda-Gomez This is a preprint; it has not been peer reviewed by a journal. https://doi.org/ 10.21203/rs.3.rs-6202921/v1 This work is licensed under a CC BY 4.0 License Status: Posted Version 1 posted You are reading this latest preprint version Abstract Constant-speed, variable pitch propellers are widely used in medium to large aircraft, where the shaft power typically exceeds 100 kW. These propellers are usually hydraulically actuated, and their speed kept constant by means of a valve controlled by a centrifugal governor. In this paper, a digital twin of the pitch control system of a TPE331 turboprop engine is developed through physical modelling with the purpose of identifying its dynamic behavior. The operation of the system in both beta mode and flight operating mode is shown, and a comparison with experimental data is presented. digital twin turboprop electric propulsion propeller control Full Text Additional Declarations No competing interests reported. Cite Share Download PDF Status: Posted Version 1 posted You are reading this latest preprint version Research Square lets you share your work early, gain feedback from the community, and start making changes to your manuscript prior to peer review in a journal. As a division of Research Square Company, we’re committed to making research communication faster, fairer, and more useful. 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