Electrical Tail Drive Modelling Simulation and Rig Prototype Development
The research programme will capitalise on the most recent advances in electrical machine technologies, thermal modelling, design optimisation and manufacturing processes to realise and evaluate a full-scale helicopter electric tai...
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Información proyecto ELETAD
Líder del proyecto
UNIVERSITY OF BRISTOL
No se ha especificado una descripción o un objeto social para esta compañía.
TRL
4-5
Presupuesto del proyecto
2M€
Fecha límite de participación
Sin fecha límite de participación.
Descripción del proyecto
The research programme will capitalise on the most recent advances in electrical machine technologies, thermal modelling, design optimisation and manufacturing processes to realise and evaluate a full-scale helicopter electric tail rotor (ETR) motor that is engineered for flight-critical operation and is representative of an aircraft installation. A direct drive ETR solution will be optimised against the objectives of a peak output power of 3kW per kg of installed active mass making it weight-competitive with current mechanical technology, and will be a fault-tolerant design specified to an integrity target of 10 to the -9 failures per flight hour, whilst offering demonstrable performance and whole-life cost benefits.