Conceptual Design Study on Electrical Vertical Take Off and Landing Aircraft for Urban Air Mobility Applications

Author(s):  
Matthias Kraenzler ◽  
Manfred Schmitt ◽  
Eike Stumpf
Aerospace ◽  
2021 ◽  
Vol 8 (2) ◽  
pp. 54
Author(s):  
Julia A. Cole ◽  
Lauren Rajauski ◽  
Andrew Loughran ◽  
Alexander Karpowicz ◽  
Stefanie Salinger

There is currently interest in the design of small electric vertical take-off and landing aircraft to alleviate ground traffic and congestion in major urban areas. To support progress in this area, a conceptual design method for single-main-rotor and lift-augmented compound electric helicopters has been developed. The design method was used to investigate the feasible design space for electric helicopters based on varying mission profiles and technology assumptions. Within the feasible design space, it was found that a crossover boundary exists as a function of cruise distance and hover time where the most efficient configuration changes from a single-main-rotor helicopter to a lift-augmented compound helicopter. In general, for longer cruise distances and shorter hover times, the lift-augmented compound helicopter is the more efficient configuration. An additional study was conducted to investigate the potential benefits of decoupling the main rotor from the tail rotor. This study showed that decoupling the main rotor and tail rotor has the potential to reduce the total mission energy required in all cases, allowing for increases in mission distances and hover times on the order of 5% for a given battery size.


2013 ◽  
Vol 25 (8) ◽  
pp. 989-1008 ◽  
Author(s):  
Rafic M Ajaj ◽  
Michael I Friswell ◽  
Erick I Saavedra Flores ◽  
Andy Keane ◽  
Askin T Isikveren ◽  
...  

1983 ◽  
Vol 4 (2P3) ◽  
pp. 854-859 ◽  
Author(s):  
N. Nakamura ◽  
H. Omura ◽  
S. Ido ◽  
S. Nakai ◽  
C. Yamanaka

1994 ◽  
Vol 10 (04) ◽  
pp. 258-273
Author(s):  
A. D. Karstensen ◽  
A. C. Fairlie-Clarke ◽  
I. E. Winkle

Hydrodynamic control surfaces are traditionally built as steel fabrications. While this gives a very strong structure, it is rather heavy and costly, it is difficult to achieve smooth surfaces, and the steel is susceptible to erosion, corrosion and marine fouling. This paper describes a conceptual design study aimed at creating a competitive advantage for the manufacturers of control surfaces by using modern materials in a composite structure. The conceptual design process, as applied here, starts by specifying the design requirements for the construction of control surfaces and listing a set of criteria against which the concept designs can be evaluated. A total of six concept designs are described and evaluated in comparison with a traditional steel fabrication, and one concept is selected for further development. This comprises a light steel frame structure with thin steel inner face plates enclosing an inner core that is filled with polyurethane foam. The surface shape is also formed with polyurethane foam poured between the face plates and a surface mold plate. Finally, the surface is sprayed with a polyurethane elastomer coating.


1995 ◽  
Author(s):  
Blair P. Bromley ◽  
John DeMora ◽  
Brett Casey ◽  
Paul Humm ◽  
Erik Kirstein ◽  
...  

1999 ◽  
Author(s):  
Hitoshi Yokobori ◽  
Makoto Sasaki ◽  
Toshiyuki Yamanaka

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