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HYDROGEN POWERED FREIGHTER AIRCRAFT-THE FINAL RESULTS OF THE GREEN FREIGHTER PROJECT

机译:氢动力货运飞机-绿色货运项目的最终结果

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This paper presents the results of the jointaircraft design project 'The Green Freighter'that dealt with the investigation of hydrogenfueledfreighter aircraft. This includedconventional as well as blended-wing-body(BWB) aircraft designs. Within the scope of theproject the Preliminary Aircraft Design andOptimization program PrADO was extendedand applied to analyses of conventional andunconventional freighter aircraft designs. Theinvestigations show that hydrogen as aviationfuel is feasible. Rising energy prices will makeair transport more expensive than today, buthydrogen is a potential alternative fuel thatkeeps air traffic possible even if low-pricedkerosene is no longer available. In addition, airtraffic could become more environmentallyfriendly. Hydrogen-fueled regional freighteraircraft have up to 5 % smaller maximum takeoffmasses and consume about 10 % less energythan the kerosene reference version despitetheir up to 7 % higher operating empty masses.The installation of large hydrogen tanks usingthe full fuselage cross section is significantlysuperior to an installation of removable tankswith smaller diameter. An unmanned freightercan use the cockpit volume for hydrogen storageand further helps to optimize the design. Theinvestigations of the hydrogen-fueled BWBdesigns show possible savings of about 6.5 % intake-off mass, which is predominantly due to a66.5 % lower fuel mass. The combination ofnecessary minimum aircraft size and low fuelmass causes a low wing loading. In effect, theBWB designs cannot make use of theirtheoretically very high aerodynamicperformance during cruise flight.
机译:本文介绍了联合飞机设计项目“绿色货轮”的结果,该项目涉及氢燃料货运飞机的研究。这包括常规以及混合机翼(BWB)飞机的设计。在项目范围内,初步飞机设计和优化程序PrADO已扩展并应用于常规和非常规货机的设计分析。研究表明,氢气作为航空燃料是可行的。不断上涨的能源价格将使航空运输比今天更加昂贵,但是氢是一种潜在的替代燃料,即使不再提供低价的煤油,也可以使空中交通保持畅通。另外,空中交通可能变得更加环保。氢燃料支线货机的最大起飞质量比煤油参考型号小多达5%,而能耗却比煤油参考型号低约10%,而使用全机身横截面的大型氢罐的安装明显优于安装直径较小的可移动水箱。无人驾驶货轮可以将驾驶舱的容积用于氢气存储,并进一步帮助优化设计。氢燃料电池BWB设计的研究表明,可节省约6.5%的进气质量,这主要是由于燃料质量降低了66.5%。必要的最小飞机尺寸和低燃油质量相结合,导致机翼负载较低。实际上,BWB设计在巡航飞行期间无法利用其理论上非常高的空气动力学性能。

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