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From Popular Science; By Clay Dillow 05.17.2010 Original Article | ||
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Competing with designs from GE Aviation, Boeing and Northrop Grumman, the object was to create a passenger jet that burns 70 percent less fuel, cuts emissions of nitrogen oxides by 75 percent, takes off from shorter runways, and reduces sound pollution. MIT's solution: A "double bubble" architecture that relies on a dual fuselage design -- that is, two cylindrical structures placed side by side to make up the fuselage rather than a single tube-and-wing structure (such that a cross section would resemble two soap bubbles fused together). The design allows for a wider, shorter fuselage that should help passenger loading and unloading as well as increase seating capacity. But the real innovation is in the engine placement. Rather than wing-mounted turbines that scoop up the untouched fast-moving air away from the fuselage, the tail-mounted D series engines suck up the slower-moving air coming off the wake of the fuselage. This Boundary Layer Ingestion (BLI) technique allows less fuel to be burned while generating the same amount of thrust, allowing the D series design to hit the 70 percent fuel reduction goals outlined by NASA. NASA envisions aggressive designs like the D series taking flight by 2035, when air traffic is expected to double from current levels. To bridge the gap, MIT also mocked up an H series plane based on the same design principles but using current jet technology and conventional aluminums that achieves a 50 percent fuel burn and could serve as an alternative until something like the D series becomes standard. There are drawbacks to both designs of course. The rear engine layout would increase engine stress, and both planes would travel about 10 percent slower than a 737. But given the fuel savings and reduced runway real estate needed to launch and land the D series, a small concession in flight time sounds pretty reasonable. |