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Propeller research advance paves way for quiet electric aviation

Elec­tri­fi­ca­tion plays an impor­tant role in fos­sil-free avi­a­tion but the more ener­gy-effi­cient an elec­tric air­craft is, the nois­i­er it gets, so researchers at Chalmers Uni­ver­si­ty of Tech­nol­o­gy in Swe­den claim to have now opti­mised pro­peller design to pave the way for qui­et elec­tric avi­a­tion.

In recent years, elec­tri­fi­ca­tion has had an impor­tant role in reduc­ing emis­sions but inter­est has been most­ly focussed on elec­tric pro­peller planes cov­er­ing short­er dis­tances, con­sid­ered to be the most effi­cient propul­sion sys­tem for region­al and domes­tic flights.

While the noise from the pro­peller blades may dis­turb air pas­sen­gers, future elec­tric air­craft will need to fly at rel­a­tive­ly low alti­tudes, with noise dis­tur­bance reach­ing res­i­den­tial areas and ani­mal life.

“We can see that the more blades a pro­peller has, the low­er the noise emis­sions, but with few­er blades, propul­sion becomes more effi­cient and an elec­tric air­craft can fly for longer,” explained Hua-Dong Yao (pic­tured), asso­ciate pro­fes­sor and researcher in flu­id dynam­ics and marine tech­nol­o­gy at Chalmers Uni­ver­si­ty of Tech­nol­o­gy.

“In that sense, there is a trade-off between ener­gy effi­cien­cy and noise, and this is some­thing of an obsta­cle for elec­tric air­crafts that are both qui­et and effi­cient.”

Now, Hua-Dong Yao and his research col­leagues have suc­ceed­ed in iso­lat­ing and explor­ing the noise that occurs at the tip of the pro­peller blades, or ‘tip vor­tices’, a known but less well-explored source of noise. In iso­lat­ing this noise, the researchers were able to ful­ly under­stand its role in rela­tion to oth­er noise sources gen­er­at­ed by pro­peller blades.

By adjust­ing a range of pro­peller para­me­ters, such as pitch angle, chord length and num­ber of blades, the team found a way to opti­mise the pro­peller design and even out the trade-off effect between effi­cien­cy and noise. The method, described in a study pub­lished in the jour­nal Aero­space, can now be used in the design process of qui­eter pro­pellers for future elec­tric air­craft.

Hua-Dong Yao con­tin­ued: “Mod­ern air­craft pro­pellers usu­al­ly have two to four blades, but we have found that by using six blades designed using our opti­mi­sa­tion frame­work, we can devel­op a pro­peller that is both rel­a­tive­ly effi­cient and qui­et.

“The pro­peller achieves a noise reduc­tion of up to 5–8 dBA with only a 3.5 per cent thrust penal­ty, com­pared to a pro­peller with three blades. That is com­pa­ra­ble to the noise reduc­tion of some­one going from speak­ing in a nor­mal con­ver­sa­tion voice to the sound you would per­ceive in a qui­et room.”

A‑weighted deci­bel (dBA) is an expres­sion of the rel­a­tive loud­ness of sounds as per­ceived by the human ear. A‑weighting gives more val­ue to fre­quen­cies in the mid-range of human hear­ing and less val­ue to fre­quen­cies at the edges as com­pared to a flat audio deci­bel mea­sure­ment. A‑weighting is the stan­dard for deter­min­ing hear­ing dam­age and noise pol­lu­tion.

The study, ‘Blade-Tip Vor­tex Noise Mit­i­ga­tion Trad­ed-Off against Aero­dy­nam­ic Design for Pro­pellers of Future Elec­tric Air­craft’, was pub­lished in the jour­nal Aero­space. The authors are Hua-Dong Yao, Zhongjie Huang, Lars David­son, Jiqiang Niu and Zheng-Wei Chen.

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Jason Pritchard

Jason Pritchard is the Editor of eVTOL Insights. He holds a BA from Leicester's De Montfort University and has worked in Journalism and Public Relations for more than a decade. Outside of work, Jason enjoys playing and watching football and golf. He also has a keen interest in Ancient Egypt.

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