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Anatomy of the Hudson

机译:哈德逊的解剖

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摘要

The Hudson's airframe was essentially the same as the Model 14 Super Electra, but with additional military equipment. While the wings and empennage were unchanged, the fuselage was heavily modified internally, initially to meet British requirements, and later, with further minor changes, for Australian, New Zealand and Canadian service variations. American equipment was fitted for use by the US services, though this involved more in the way of emergency adaptations than full re-designs. Both the Model 14 and the Hudson derived benefit from the use of Fowler flaps, which, by moving aft as they were lowered, both increased the camber and the area of the wing. This was otherwise of conventional all-metal form and construction, though the Hudson eventually gained self-sealing fuel tanks. Additional tanks could be positioned in the bomb bay and fuselage depending on range and operational requirements. The Hudson and Super Electra were laterfitted with built-in outer wing slots as a fix to a stall and roll problem.
机译:哈德逊的机体与Model 14 Super Electra基本相同,但增加了军事装备。尽管机翼和尾翼没有变化,但机身内部进行了重大改动,最初是为了满足英国的要求,后来又进行了较小的改动,以适应澳大利亚,新西兰和加拿大的服务需求。美国的设备适合美国的服务使用,尽管这涉及的是紧急应变方式,而不是完全重新设计。 Fowler襟翼的使用使Model 14和Hudson都受益匪浅,Fowler襟翼随着放低而向后移动,都增加了弧度和机翼面积。尽管Hudson最终获得了自动密封的燃油箱,但它还是采用了传统的全金属形式和结构。根据射程和操作要求,可以在炸弹舱和机身中放置其他坦克。哈德逊和超级伊莱克特拉后来装配了内置的外机翼插槽,以解决失速和侧倾问题。

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    《Aeroplane》 |2015年第10期|77-78|共2页
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