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Bringing Sustainable Air Transport Closer - Clean Sky

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7<br />

NO X Reduction Potential (2020 Technologies, %)<br />

Baseline: 2000 Emissions<br />

-20<br />

-40<br />

-60<br />

-70<br />

<strong>Bringing</strong> <strong>Sustainable</strong> <strong>Air</strong> <strong>Transport</strong> <strong>Closer</strong><br />

Fixed Wing<br />

<strong>Air</strong>craft (2)<br />

(1) Rotorcraft: Turbofan based. Diesel NO X reduction more limited<br />

(2) Additional gains being investigated (new <strong>Clean</strong> <strong>Sky</strong> project areas)<br />

EPNdB<br />

-5<br />

-10<br />

-15<br />

(2)<br />

Rotorcraft (1)<br />

Noise Reduction Potential (2020 Technologies, EPNdB)<br />

Baseline: 2000 Emissions<br />

-50% Perceived Noise<br />

e Fixed Wing<br />

<strong>Air</strong>craft<br />

Rotorcraft<br />

Significant increase in benefits through<br />

flightpath optimisation<br />

In large commercial and regional jet<br />

aircraft, a key design option concerns<br />

the incorporation of the Counter<br />

Rotating Open Rotor (CROR) engine<br />

architecture and technology. This<br />

design option involves an important<br />

trade-off: signifi cantly more fuel burn<br />

and CO 2 reductions are expected,<br />

coupled with less progress on noise,<br />

when compared to future turbofan<br />

architectures. The fi gures in these<br />

graphs assume the use of CROR on<br />

short/medium haul aircraft. Fixed wing<br />

aircraft fi gures represent the median<br />

performance improvement across the<br />

spectrum of business jets, regional<br />

aircraft and short/medium range<br />

commercial aircraft. Long-range<br />

commercial aircraft are, as yet, not<br />

included as no (integrated) concept<br />

aircraft predictions are available.<br />

In rotorcraft, an innovation being<br />

investigated concerns the adoption<br />

of Diesel engine propulsion (on<br />

so-called light single-engine helicopters).<br />

The Diesel engine could<br />

deliver impressive fuel burn and CO 2<br />

benefi ts, albeit with a penalty in NO X<br />

performance when compared to a<br />

future turboshaft engine. The graphs<br />

depict the range of variance this<br />

would imply for both CO 2 and NO X .<br />

Note: noise reduction is measured in Effective Perceived Noise (EPNdB), and fi gures represent the average reduction per operation (take-off,<br />

approach or fl y-past). A reduction of 10 EPNdB is widely accepted as corresponding to a halving of perceived noise in terms of the human<br />

auditive capacity and perception. The ACARE target of ‘halving perceived noise’ thus corresponds with a fi gure in the graph of -10 EPNdB.

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