Results 91 to 100 of about 10,974 (193)
Protection system considerations for DC distributed electrical propulsion systems
Distributed electrical propulsion for aircraft, also known as turbo-electric distributed propulsion (TeDP), will require a complex electrical power system which can deliver power to multiple propulsor motors from gas turbine driven generators.
Catherine E. Jones +13 more
core +1 more source
The Multidisciplinary Design Optimization of a Distributed Propulsion Blended-Wing-Body Aircraft
The purpose of this study is to examine the multidisciplinary design optimization (MDO) of a distributed propulsion blended-wing-body (BWB) aircraft. The BWB is a hybrid shape resembling a flying wing, placing the payload in the inboard sections of the ...
Ko, Yan-Yee Andy
core
Protection Coordination Strategy for the Distributed Electric Aircraft Propulsion Systems
The current trend in distributed electric aircraft propulsion systems is to utilize the DC bus system at higher voltage levels than conventional aircraft systems.
Wang, Fred +7 more
core +1 more source
Electric aircraft face a steep tradeoff between the demand for runway performance and range. While fuel based propulsion technologies typically increase in specific power with increasing size, electric propulsion is typically much more scalable.
Moore, Kevin, Ning, Andrew
core
This study presents an aeroelastic wing shaping control concept for distributed propulsion aircraft. By leveraging wing flexibility, wing-mounted distributed propulsion can be used to re-twist wing shapes in-flight to improve aerodynamic efficiency.
Nguyen, Nhan T. +3 more
core
The present paper details the design of the counter rotating fans for a Turboelectric Distributed Propulsion (TeDP) system. Sixteen propulsors installed in mail-slot-shape nacelles are embedded on an aerodynamically optimized hybrid wing-body ...
Lee, Byung Joon +2 more
core
Sustainable Autonomous Solar UAV with Distributed Propulsion System
Solar-powered Unmanned Aerial Vehicles (UAVs) solve the problem of loiter time as aircrafts can fly as long as sufficient illumination and reserve battery power is available.
Liu, Shupeng
core
Safety boundary protection control for distributed propulsion vehicle operating in plateau environment. [PDF]
Dong Z, Da X, Zhang B, Guo L.
europepmc +1 more source
Joint Optimization of Trajectory-Resource Allocation and Deep Task Partial Offloading for MEC-Enabled Multi-UAV. [PDF]
Liu C, Wang Y, Mei H, Du S, Guo B.
europepmc +1 more source
Numerical Simulation of Distributed Propulsion Systems Using Cfd
Geng Qiao, Tao Zhang, George N. Barakos
openaire +1 more source

