InGe Integrated electric Generator and motor
Reference number | |
Coordinator | GKN Aerospace Sweden AB - Avd 9005 |
Funding from Vinnova | SEK 4 500 000 |
Project duration | October 2019 - December 2022 |
Status | Completed |
Venture | National Aeronautical Research Program 7 |
Call | Research project in aviation technology - spring 2019 |
Important results from the project
** Denna text är maskinöversatt ** A future aircraft engine concept with integrated electric generator is described in: T. Grönstedt et al, "Multidisciplinary Assessment of a Year 2035 Turbofan Propulsion System", 33rd Congress of The International Council of The Aeronautical Sciences (ICAS), 49 Sept 2022, Stockholm An integrated electric generator concept for future aircraft engines: A. Reinap et al," Analysis and development of integrated lowpressure shaft generator", 33rd Congress of The International Council of The Aeronautical Sciences (ICAS), 49 Sept 2022, Stockholm
Expected long term effects
** Denna text är maskinöversatt ** Project results have been published at conferences, e.g. ICAS 2022 in Stockholm. Input to the numerical and experimental studies within the framework of this project has been based on aircraft engine concepts for civil future aircraft engines developed by GKN. An important outcome of the project is an increased understanding of the potential of integrating electric machines in future aircraft engines and what gains this can bring in the form of reduced fuel consumption but also challenges and limitations related to the aircraft engine environment.
Approach and implementation
** Denna text är maskinöversatt ** The work has progressed according to the project plan. Both digital and physical meetings between the project´s participants have been applied. During the pandemic and the restrictions that followed, digital meetings were an appropriate way to meet. GKN has during the project delivered data for studies of the integration of electric machines into future aircraft engines. Detailed results from studies and experiments regarding electric machines and their limitations have been fed back into motor system models for evaluation.