To enable higher gross weights, the later –30 and –40 series have an additional two-wheel main landing gear, which retracts into the center of the fuselage.[47]【参考译文】DC-10的主要飞行控制包括内外副翼、两节升降舵和两节方向舵;次要飞行控制包括前缘缝翼、扰流板和双速移动水平安定面。垂直安定...
Report Zhiren Chen6 年以前 DC-10 has larger tail wings and its CF6-50s have big tailpipes. Also, DC-10-10s do not have the middle landing gear. Report Donald G. Elliott6 年以前 Robert, it is a MD10, no center gear and no winglets. Report动态...
Stress Analysis of the McDonnell Douglas DC-10 Nose Landing Gear Unit: An account of the use of the photoelastic coating technique to determine the stress distribution and maximum stress areas over the external surface of the nose undercarriage assembly...
驾驶舱应急出口escape hatch, overhead hatch辅助动力装置舱门APU(Auxiliary Power Unit) access door电子/电气舱门E&E compartment door冲压空气涡轮舱门RAT compartment door前起落架舱门nose landing gear door主起落架舱门main landing gear door·门结构DOOR STRUCTURE门框door frame, door-case门梁door beam门加强肋...
图片题注:The heavier DC-10-30 has an additional center landing gear.参考译文:更重的DC-10-30型飞机增加了一套中央起落架。图片作者:Pedro Aragão 3.2.2 DC-10-30CF The convertible cargo/passenger transport version of the DC-10-30. The first deliveries were to Overseas National Airways (ONA...
IN 1968, Dowry Rotol Ltd., Staverton, Gloucester, were awarded a contract by McDonnell Douglas Corporation to implement a surface stress survey on the DC-10 Nose Undercarriage Assembly.doi:10.1108/eb034698Gullick, D.S.Birch, B.D.Aircraft Engineering & Aerospace Technology...