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- W2333972764 abstract "The gas turbine engines on commercial aircraft produce both propulsive power and non-propulsive or secondary power for aircraft subsystems, which can be in the form of either pneumatic or mechanical power off-take. While there is a degradation in performance and an increase in the thrust-specific fuel consumption in both cases, the extent is not necessarily identical. In addition, subsystem architecture choices also have an effect on aircraft empty weight and possibly on drag. Therefore, the current industry trend towards More Electric subsystem architectures has potentially far-reaching impacts on aircraft performance. To ascertain the effect of subsystem architecture choices on aircraft-level and mission-level metrics of interest, the subsystems as well as their impacts on the aircraft and propulsion system must be modeled in suitable detail. Such an approach is demonstrated in this paper for the case of a representative single-aisle aircraft with a focus on two subsystems which collectively consume a large fraction of the aircraft’s total secondary power requirements the Environmental Control System and the Ice Protection Systems." @default.
- W2333972764 created "2016-06-24" @default.
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- W2333972764 date "2015-06-18" @default.
- W2333972764 modified "2023-09-27" @default.
- W2333972764 title "Effect of Major Subsystem Power Off-takes on Aircraft Performance in More Electric Aircraft Architectures" @default.
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- W2333972764 doi "https://doi.org/10.2514/6.2015-3287" @default.
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