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NOISE IMPACT OF ELECTRIC AND HYBRID PROPULSION IN AVIATION Opportunities and Threats Rod Self ISVR, University of Southampton 20 th November 2018 Greener By Design Conference -- London

NOISE IMPACT OF ELECTRIC AND HYBRID PROPULSION IN … · NOISE IMPACT OF ELECTRIC AND HYBRID PROPULSION IN AVIATION Opportunities and Threats Rod Self ISVR, University of Southampton

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Page 1: NOISE IMPACT OF ELECTRIC AND HYBRID PROPULSION IN … · NOISE IMPACT OF ELECTRIC AND HYBRID PROPULSION IN AVIATION Opportunities and Threats Rod Self ISVR, University of Southampton

NOISE IMPACT OF ELECTRIC AND HYBRID PROPULSION IN AVIATION

Opportunities and Threats

Rod SelfISVR, University of Southampton

20th November 2018Greener By Design Conference -- London

Page 2: NOISE IMPACT OF ELECTRIC AND HYBRID PROPULSION IN … · NOISE IMPACT OF ELECTRIC AND HYBRID PROPULSION IN AVIATION Opportunities and Threats Rod Self ISVR, University of Southampton

What electric aircraft are:

Page 3: NOISE IMPACT OF ELECTRIC AND HYBRID PROPULSION IN … · NOISE IMPACT OF ELECTRIC AND HYBRID PROPULSION IN AVIATION Opportunities and Threats Rod Self ISVR, University of Southampton

Types of electric aircraft:

Drones

Small UAVs for package delivery and other roles

Page 4: NOISE IMPACT OF ELECTRIC AND HYBRID PROPULSION IN … · NOISE IMPACT OF ELECTRIC AND HYBRID PROPULSION IN AVIATION Opportunities and Threats Rod Self ISVR, University of Southampton

Types of electric aircraft:

Air Taxis

Images Curtesy NASA

Larger UAVs for urban and sub-regional passenger transport

Page 5: NOISE IMPACT OF ELECTRIC AND HYBRID PROPULSION IN … · NOISE IMPACT OF ELECTRIC AND HYBRID PROPULSION IN AVIATION Opportunities and Threats Rod Self ISVR, University of Southampton

Types of electric aircraft:

Hybrid Electric

Images Curtesy Zunum Aero

Replacement for short and medium haul passenger transport

Page 6: NOISE IMPACT OF ELECTRIC AND HYBRID PROPULSION IN … · NOISE IMPACT OF ELECTRIC AND HYBRID PROPULSION IN AVIATION Opportunities and Threats Rod Self ISVR, University of Southampton

What electric aircraft are not:

• Electric aircraft are not necessarily quieter than equivalent conventional aircraft

• Main noise sources: jet, fan, and airframe still present

• Combustor and turbine noise may be absent

• Electric motor noise is present

Page 7: NOISE IMPACT OF ELECTRIC AND HYBRID PROPULSION IN … · NOISE IMPACT OF ELECTRIC AND HYBRID PROPULSION IN AVIATION Opportunities and Threats Rod Self ISVR, University of Southampton

SAECA Project Results

• e-A320 v. A320neo – 900nm mission -- TO

Page 8: NOISE IMPACT OF ELECTRIC AND HYBRID PROPULSION IN … · NOISE IMPACT OF ELECTRIC AND HYBRID PROPULSION IN AVIATION Opportunities and Threats Rod Self ISVR, University of Southampton

SAECA Project Results

• e-A320 v. A320neo – noise v. mission length -- TO

Page 9: NOISE IMPACT OF ELECTRIC AND HYBRID PROPULSION IN … · NOISE IMPACT OF ELECTRIC AND HYBRID PROPULSION IN AVIATION Opportunities and Threats Rod Self ISVR, University of Southampton

SAECA Project Results

• e-A320 v. A320neo – Approach

Page 10: NOISE IMPACT OF ELECTRIC AND HYBRID PROPULSION IN … · NOISE IMPACT OF ELECTRIC AND HYBRID PROPULSION IN AVIATION Opportunities and Threats Rod Self ISVR, University of Southampton

More realistic concept aircraft do show noise gains

• E.g. Boing Sugar-Volt concept estimate is 22 EPNdB below Chapter 4

• However, more conventional concept aircraft have comparable gains

• Main noise gains of e-aircraft from increased propulsive efficiency

• More radical designs such as DEP may give greater gains

• But we are less sure how to estimate the impact

Page 11: NOISE IMPACT OF ELECTRIC AND HYBRID PROPULSION IN … · NOISE IMPACT OF ELECTRIC AND HYBRID PROPULSION IN AVIATION Opportunities and Threats Rod Self ISVR, University of Southampton

Estimating noise from novel aircraft – physical noise

• Because conventional aircraft have the same type of noise emission we know how to estimate changes

• More novel designs require understanding:

• In principle this is not a problem

New noise sources such as motor noise and BLI noise

New installation effects

New operational profiles

Page 12: NOISE IMPACT OF ELECTRIC AND HYBRID PROPULSION IN … · NOISE IMPACT OF ELECTRIC AND HYBRID PROPULSION IN AVIATION Opportunities and Threats Rod Self ISVR, University of Southampton

Estimating noise from novel aircraft – perception

• How people respond to noise depends on a number of factors – not just loudness

• Do current metrics, EPNL and Leq apply to novel aircraft?

Page 13: NOISE IMPACT OF ELECTRIC AND HYBRID PROPULSION IN … · NOISE IMPACT OF ELECTRIC AND HYBRID PROPULSION IN AVIATION Opportunities and Threats Rod Self ISVR, University of Southampton

Effective Perceived Noise Level

• Effective Perceived Noise Level (EPNL) is the current metric used to assess noise emissions for certification.

Frequency

Sou

nd

Pre

ssu

re L

evel

(d

B)

Noise SPECTRUM

• EPNL:

o Perceived Noise Level (PNL),

o duration effects, and

o tonal penalty based on the level of the strongest protruding tone.

Page 14: NOISE IMPACT OF ELECTRIC AND HYBRID PROPULSION IN … · NOISE IMPACT OF ELECTRIC AND HYBRID PROPULSION IN AVIATION Opportunities and Threats Rod Self ISVR, University of Southampton

• EPNL is not able to account for the perceptual effect of complex tones.o 1/3-octave banding for tone detection.

o Solely focused on strongest protruding tone.

14

0

10

20

30

40

50

60

70

80

100 1000 10000

Sou

nd

Lev

el (

dB

)

Frequency (Hz)

Frequency (Hz)

1/3-octave bands (Hz)

0

10

20

30

40

50

60

70

80

100 1000 10000

Sou

nd

Lev

el (

dB

)

Frequency (Hz)

Frequency (Hz)

1/3-octave bands (Hz)

• Work at the ISVR shows Aures Tonality based metric better at predicting perception than EPNL when multiple tones are present

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15

Courtesy of Rolls-Royce plc - Advanced open rotor concept

Courtesy of NASA - Sceptor project

Annoyance model for DEP using Loudness, Roughness and AuresTonality as predictors (Rizzi et al., 2017)

Source: Kingan (2014)

Page 16: NOISE IMPACT OF ELECTRIC AND HYBRID PROPULSION IN … · NOISE IMPACT OF ELECTRIC AND HYBRID PROPULSION IN AVIATION Opportunities and Threats Rod Self ISVR, University of Southampton

• Small-size quadcopters (DJI Phantom and HS-200): Multiple complex tones distributed across the whole spectrum (significant content in high frequency).

• Drone noise certification: More sophisticated tonality methods needed.

16

Tones -- A major potential problem for drones and air taxis

Page 17: NOISE IMPACT OF ELECTRIC AND HYBRID PROPULSION IN … · NOISE IMPACT OF ELECTRIC AND HYBRID PROPULSION IN AVIATION Opportunities and Threats Rod Self ISVR, University of Southampton

• Currently Leq used to measure community annoyance around airports

• Not always reliable

• Will need to be amended to reflect novel aircraft noise signatures

17

Community Noise Considerations -- I

Page 18: NOISE IMPACT OF ELECTRIC AND HYBRID PROPULSION IN … · NOISE IMPACT OF ELECTRIC AND HYBRID PROPULSION IN AVIATION Opportunities and Threats Rod Self ISVR, University of Southampton

• The most annoying noise is a new noise

• Drones and other urban aircraft will increasingly affect people away from airports

• Visual intrusion from low altitude flights increases perceived noise substantially

• Public understanding and trust are major issues

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Community Noise Considerations -- II

Page 19: NOISE IMPACT OF ELECTRIC AND HYBRID PROPULSION IN … · NOISE IMPACT OF ELECTRIC AND HYBRID PROPULSION IN AVIATION Opportunities and Threats Rod Self ISVR, University of Southampton

• E-aircraft replacing current fleet:

– are likely to show substantial noise benefits but variation in noise signature will require novel metrics to reflect noise impact

– Will require additional source modelling and knowledge of operation to establish confident prediction of noise impact

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Conclusions and Requirements -- I

Page 20: NOISE IMPACT OF ELECTRIC AND HYBRID PROPULSION IN … · NOISE IMPACT OF ELECTRIC AND HYBRID PROPULSION IN AVIATION Opportunities and Threats Rod Self ISVR, University of Southampton

• Urban E-aircraft – Drones and Air Taxis:

– New noise source whose impact cannot be predicted with confidence

– Will require source modelling and knowledge of operation to establish confident prediction of noise levels

– Will require significant research on multi-model attitudinal response to establish appropriate metrics

– Will require establishment of low noise operational rules

– Will require public participation to maintain trust

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Conclusions and Requirements -- II

Page 21: NOISE IMPACT OF ELECTRIC AND HYBRID PROPULSION IN … · NOISE IMPACT OF ELECTRIC AND HYBRID PROPULSION IN AVIATION Opportunities and Threats Rod Self ISVR, University of Southampton

Thank you!