publication . Doctoral thesis . 2013

Turboelectric Distributed Propulsion System Modelling

Liu, Chengyuan;
Open Access English
  • Published: 01 Dec 2013
  • Publisher: Cranfield University
  • Country: United Kingdom
Abstract
The Blended-Wing-Body is a conceptual aircraft design with rear-mounted, over wing engines. Turboelectric distributed propulsion system with boundary layer ingestion has been considered for this aircraft. It uses electricity to transmit power from the core turbine to the fans, therefore dramatically increases bypass ratio to reduce fuel consumption and noise. This dissertation presents methods on designing the TeDP system, evaluating effects of boundary layer ingestion, modelling engine performances, and estimating weights of the electric components. The method is first applied to model a turboshaft-driven TeDP system, which produces thrust only by the propulsor...
Subjects
free text keywords: BLI, TeDP, Distortion, NASA N3-X Aircraft, Turbogenerator, Propulsor, thrust split ratio
Related Organizations
Download from
Cranfield CERES
Doctoral thesis . 2013
Powered by OpenAIRE Research Graph
Any information missing or wrong?Report an Issue