An assessment of distributed propulsion: Advanced propulsion system architectures for conventional aircraft configurations

2015 ◽  
Vol 46 ◽  
pp. 42-50 ◽  
Author(s):  
Rudi Kirner ◽  
Lorenzo Raffaelli ◽  
Andrew Rolt ◽  
Panagiotis Laskaridis ◽  
Georgios Doulgeris ◽  
...  
Keyword(s):  
Propulsion System ◽  
System Architectures ◽  
Distributed Propulsion ◽  
Aircraft Configurations

An assessment of distributed propulsion: Part B – Advanced propulsion system architectures for blended wing body aircraft configurations

2016 ◽  
Vol 50 ◽  
pp. 212-219 ◽  
Author(s):  
Rudi Kirner ◽  
Lorenzo Raffaelli ◽  
Andrew Rolt ◽  
Panagiotis Laskaridis ◽  
Georgios Doulgeris ◽  
...  
Keyword(s):  
Propulsion System ◽  
System Architectures ◽  
Distributed Propulsion ◽  
Blended Wing Body ◽  
Aircraft Configurations

A novel hybrid aircraft propulsion based on the DEA compressor—Part A: Design

2021 ◽  
pp. 095441002110253
Author(s):  
Babak Aryana
Keyword(s):  
High Performance ◽  
Static Condition ◽  
Propulsion System ◽  
Hybrid Propulsion ◽  
Pulse Detonation ◽  
Low Emission ◽  
Wide Range ◽  
Exit Nozzle ◽  
Distributed Propulsion ◽  
Detonation Process

This two-part article introduces a novel hybrid propulsion system based on the DEA compressor. The system encompasses a Pulse Detonation TurboDEA as the master engine that supplies several full-electric ancillary thrusters called DEAThruster. The system, called the propulsion set, can be categorized as a distributed propulsion system based on the design mission and number of ancillary thrusters. Part A of this article explains the design process comprising intake, compressor, detonation process, diffuser, axial turbine, and the exit nozzle. The main target is to design a high-performance low emission propulsion system capable of serving in a wide range of altitudes and flight Mach numbers that covers altitudes up to 20,000 m and flight Mach number up to the hypersonic edge. Designing the propulsion set, the design point is considered at the static condition in the sea level. Design results show the propulsion set can satisfy all requirements necessary for its mission.

scholarly journals Aerodynamic interaction between propellers of a distributed-propulsion system in forward flight

2021 ◽  
pp. 107009
Author(s):  
Reynard de Vries ◽  
Nando van Arnhem ◽  
Tomas Sinnige ◽  
Roelof Vos ◽  
Leo L.M. Veldhuis
Keyword(s):  
Propulsion System ◽  
Forward Flight ◽  
Aerodynamic Interaction ◽  
Distributed Propulsion

Aero-Propulsive and Propulsor Cross-Coupling Effects on a Distributed Propulsion System

2018 ◽  
Vol 55 (6) ◽  
pp. 2414-2426 ◽  
Author(s):  
Aaron T. Perry ◽  
Phillip J. Ansell ◽  
Michael F. Kerho
Keyword(s):  
Cross Coupling ◽  
Propulsion System ◽  
Coupling Effects ◽  
Distributed Propulsion

Methodology to qualify marine electrical propulsion system architectures for platform supply vessels

2018 ◽  
Vol 8 (2) ◽  
pp. 152-165 ◽  
Author(s):  
Srinivasarao Kamala ◽  
Priyesh J. Chauhan ◽  
Sanjib K. Panda ◽  
Gary Wilson ◽  
Xiong Liu ◽  
...  
Keyword(s):  
Propulsion System ◽  
System Architectures ◽  
Electrical Propulsion
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