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B-50C是为了发挥出B-50最大的潜能而设计的,装4台新型的R-4360-43涡轮增压发动机.重新设计了机身结构,机翼面积增加并且机身加长,起飞重量也增加至97吨,比其他型号的B-50增加了22吨。 早期生产的一架B-50A被改装成B-50C的原型机YB-50C,生产型的B-50C于1948年定型。美军共订购了14架B-50C和29架RB-50C。美军认为该机的性能比A型和B型有了很大的提高,完全是为此决定赋予该机一个新的编号-B-54。不过,正当美军雄心勃勃开始发展该机时,美国国防经费陷入了困境,1949年是美国国防经费最为困难的一年,大批的项目被迫取消.B-54受原型性能的限制,性能上不可能有质的飞跃,而且更为严重的是,该机由于机翼加长,需要在机翼外端加装支撑轮,为此原
The B-50C is designed to maximize the potential of the B-50, with four new R-4360-43 turbocharged engines, a redesigned fuselage structure, increased wing area and longer fuselage, take-off weight Also increased to 97 tons, 22 tons more than other models of the B-50. Early production of a B-50A was converted into the prototype of the B-50C YB-50C, production B-50C stereotypes in 1948. The United States ordered a total of 14 B-50C and 29 RB-50C. The U.S. military believes that the performance of this aircraft has been greatly improved over that of Type A and Type B. It is entirely up to this decision to give the aircraft a new code, B-54. However, just as the U.S. military ambitiously started to develop the aircraft, the U.S. defense spending was in a dilemma. 1949 was the most difficult year for U.S. defense funds and a large number of projects were canceled. B-54 is not subject to performance limitations There may be a qualitative leap, but more serious is that the aircraft due to longer wings, the need to install a support wheel on the outer wing, for the original