SwePub
Tyck till om SwePub Sök här!
Sök i LIBRIS databas

  Utökad sökning

id:"swepub:oai:DiVA.org:mdh-60961"
 

Sökning: id:"swepub:oai:DiVA.org:mdh-60961" > Impact of boundary ...

Impact of boundary layer ingestion on the performance of propeller systems for hybrid electric aircraft

Vouros, Stavros (författare)
Mälardalens universitet,Framtidens energi
Hiebl, David (författare)
Mälardalens universitet
Kyprianidis, Konstantinos (författare)
Mälardalens universitet,Framtidens energi
 (creator_code:org_t)
American Society of Mechanical Engineers (ASME), 2022
2022
Engelska.
Ingår i: Proceedings of the ASME Turbo Expo. - : American Society of Mechanical Engineers (ASME). - 9780791885970
  • Konferensbidrag (refereegranskat)
Abstract Ämnesord
Stäng  
  • Boundary layer ingestion (BLI) has demonstrated potential for reduced thrust requirements, fuel consumption and environmental impact. An integrated approach is developed for evaluating the performance of propeller systems including BLI propulsors. A rotor model based on lifting-line theory is coupled with a high-order panel method and an integral boundary layer formulation. The impact of BLI on single propeller performance maps is quantified, with efficiencies up to 15% higher compared to uniform freestream conditions. A design space exploration framework is developed for the analysis of BLI effects at propeller system level, including the impact of weight differentiation, installation technology factors, thrust split between rotors and electrical transmission losses. A reference 19-passenger aircraft featuring two wing-mounter propellers is compared with a series of conceptual designs featuring an aftfuselage BLI propeller and two wing-mounted propellers. A system-wide power saving coefficient is derived for the quantification of performance deltas between the conceptual and the reference system, including all propulsors. For systems with BLI aerodynamic benefits entirely negated by weight penalties, and electrical transmission losses of 10%, power savings of 1.5% are accrued. In a technologically advanced system with 2% reduced thrust requirements due to BLI and 3% transmission losses, power savings rise to 6.5%. This work reveals the anticipated performance potential and limitations of BLI propeller systems for the electrified future fleet.

Ämnesord

TEKNIK OCH TEKNOLOGIER  -- Maskinteknik -- Rymd- och flygteknik (hsv//swe)
ENGINEERING AND TECHNOLOGY  -- Mechanical Engineering -- Aerospace Engineering (hsv//eng)

Nyckelord

Boundary layer ingestion (BLI)
hybrid electric propulsion
installation aerodynamics
propeller performance
Boundary layers
Environmental impact
Propellers
Vehicle performance
Vehicle transmissions
Wave transmission
Wings
Boundary layer ingestion
Electrical transmission
Installation aerodynamic
Performance
Power-saving
Propulsors
Transmission-loss
Aerodynamics

Publikations- och innehållstyp

ref (ämneskategori)
kon (ämneskategori)

Hitta via bibliotek

Till lärosätets databas

Hitta mer i SwePub

Av författaren/redakt...
Vouros, Stavros
Hiebl, David
Kyprianidis, Kon ...
Om ämnet
TEKNIK OCH TEKNOLOGIER
TEKNIK OCH TEKNO ...
och Maskinteknik
och Rymd och flygtek ...
Artiklar i publikationen
Proceedings of t ...
Av lärosätet
Mälardalens universitet

Sök utanför SwePub

Kungliga biblioteket hanterar dina personuppgifter i enlighet med EU:s dataskyddsförordning (2018), GDPR. Läs mer om hur det funkar här.
Så här hanterar KB dina uppgifter vid användning av denna tjänst.

 
pil uppåt Stäng

Kopiera och spara länken för att återkomma till aktuell vy