Once integrated with the electrical part, the TMS must allow a weight/power ratio of 14 kW/kg (or 20 kW/kg at peak power) while maintaining the temperature below the limit temperature with reasonable safety margins. Submerged jet oil is the cooling technique here applied with a focus on ...
Design of the assembly tooling including the safety measures (fence, a technical floor, etc.). 3.3. Description of the Assembly Sequence This chapter describes the main steps of the ARE fuselage assembly process. The presented sequence is a basic simplification of the real process, which is mu...
European Union Aviation Safety Agency EIS: Entry into service ELCD: European reference life cycle database EM: Electric motor ERLIG: Emissions Related Landing Charges Investigation Group ETS: Emissions trading system GDP: Gross domestic product HEA: Hybrid-electric aircraft IATA: Internatio...
Riveting involves five stages, detailed in Figure 1d, that directly influence the squeezing force, and are essential for aircrafts’ structural strength and safety [2,6]. Initially, the rivet is placed centrally in the hole between the bucking bar and punch. In stage 2, under the squeezing fo...