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A method to determine the torque-speed-characteristic of a motor for an electric aircraft from real mission profiles

Knapp, Tobias and Centner, Matthias and Sturm, Gino and Lang, Matthias and Hepperle, Martin (2025) A method to determine the torque-speed-characteristic of a motor for an electric aircraft from real mission profiles. VDE - Antriebssysteme, 2025-10-08 - 2025-10-09, München.

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Abstract

[‎03.‎12.‎2025 15:58] Lang, Matthias ( EL-KPT ): This paper proposes a method to derive the torque and speed of an airplane propeller out of a given altitude and velocity profile. The method includes an efficiency optimization for the variable pitch propeller at every single timestep and therefore, utilizes the advantage that an electric drive system can dynamically follow the resulting variablespeed reference. The determined torque-speed-characteristic forms the basis for designing a suitable electrical motor. Additionally, the influence of the blade angle to the required power of the drive is discussed. Finally, the derived method is applied in order to compare the proposed variable speed strategy to a conventional strategy with constant rotational speed, which reveals only small improvements.

Item URL in elib:https://elib.dlr.de/220328/
Document Type:Conference or Workshop Item (Speech)
Title:A method to determine the torque-speed-characteristic of a motor for an electric aircraft from real mission profiles
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Knapp, TobiasTU DresdenUNSPECIFIEDUNSPECIFIED
Centner, MatthiasTU DresdenUNSPECIFIEDUNSPECIFIED
Sturm, GinoTU DredenUNSPECIFIEDUNSPECIFIED
Lang, Matthiasmatthias1.lang (at) dlr.deUNSPECIFIEDUNSPECIFIED
Hepperle, MartinMartin.Hepperle (at) dlr.deUNSPECIFIEDUNSPECIFIED
Date:8 October 2025
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:electric aircraft, variable pitch propeller, blade angle, torque-speed characteristic, variable speed operation, constant rotational speed operation, mission profile
Event Title:VDE - Antriebssysteme
Event Location:München
Event Type:international Conference
Event Start Date:8 October 2025
Event End Date:9 October 2025
Organizer:VDE
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Clean Propulsion
DLR - Research area:Aeronautics
DLR - Program:L CP - Clean Propulsion
DLR - Research theme (Project):L - Components and Emissions
Location: Cottbus
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > Transport Aircraft
Institute of Electrified Aero Engines > Component Technologies
Deposited By: Ragotzky, Sabine
Deposited On:08 Dec 2025 15:17
Last Modified:08 Dec 2025 15:17

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