Weight Estimation of the Wiring in a Distributed Propulsion System for Aircraft

2019 ◽  
Author(s):  
Adolfo Dannier ◽  
Andrea Del Pizzo ◽  
Luigi Pio Di Noia ◽  
Santolo Meo
Keyword(s):  
Propulsion System ◽  
Weight Estimation ◽  
Distributed Propulsion

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

scholarly journals Modelling of aerodynamical interaction of the wing and propellers of a distributed propulsion system

2021 ◽  
Vol 1891 (1) ◽  
pp. 012012
Author(s):  
A V Vlasov ◽  
A N Varyukhin ◽  
I A Brailko ◽  
A O Lebedev ◽  
V S Zakharchenko ◽  
...  
Keyword(s):  
Propulsion System ◽  
Distributed Propulsion

Aerodynamic benefits of boundary layer ingestion for distributed propulsion configuration

2019 ◽  
Vol 91 (10) ◽  
pp. 1285-1294 ◽  
Author(s):  
Jing Zhang ◽  
Wenwen Kang ◽  
Lingyu Yang
Keyword(s):  
Boundary Layer ◽  
Reference Value ◽  
Aerodynamic Characteristics ◽  
Comprehensive Analysis ◽  
Propulsion System ◽  
Analysis Method ◽  
Content Type ◽  
Model Based ◽  
Distributed Propulsion ◽  
Lift And Drag

Purpose Boundary layer ingestion (BLI) is one of the probable noteworthy features of distributed propulsion configuration (DPC). Because of BLI, strong coupling effects are generated between the aerodynamics and propulsion system of aircraft, leading to the specific lift and drag aerodynamic characteristics. This paper aims to propose a model-based comprehensive analysis method to investigate this unique aerodynamic. Design/methodology/approach To investigate this unique aerodynamics, a model-based comprehensive analysis method is proposed. This method uses a detailed mathematical model of the distributed propulsion system to provide the essential boundary conditions and guarantee the accuracy of calculation results. Then a synthetic three-dimensional computational model is developed to analyze the effects of BLI on the lift and drag aerodynamic characteristics. Findings Subsequently, detailed computational analyses are conducted at different flight states, and the regularities under various flight altitudes and velocities are revealed. Computational results demonstrate that BLI can improve the lift to drag ratio evidently and enable a great performance potentiality. Practical implications The general analysis method and useful regularities have reference value to DPC aircraft and other similar aircrafts. Originality/value This paper proposed a DPS model-based comprehensive analysis method of BLI benefit on aerodynamics for DPC aircraft, and the unique aerodynamics of this new configuration under various flight altitudes and velocities was revealed.

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