33th Congress of the International Council of the Aeronautical Sciences

07 - Systems, Subsystems and Equipment

ANALYSIS AND DEVELOPMENT OF INTEGRATED LOW-PRESSURE SHAFT GENERATOR

A. Reinap¹, M. Genrup¹, R. Avellán², H. Mårtensson²; ¹Lund University, Sweden ;²GKN Aerospace, Sweden

The work focuses on analysis and development of integrated low-pressure shaft generator in a geared twin-spool turbofan engine. It starts with manufacturing and evaluation of direct cooled hollow conductor coils, and has focus manufacturing, assembling and integration issues essential to machine design. The design is used to assess the features of power transfer between the turbo engine spools.


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