飞行器专业术语Aircraft professional term contrast in both Chinese and English 飞行器专业术语的中英文对照 1、the airframe 机身,结构 2、The front (fore) part 前部 3、The rear (aft) part 后部 4、port 左旋(舵)5、starboard 右旋(舵)6、the inboard engine or inboards 内侧发动机 7、the outboard ...
aircraft basic operating weight aircraft block speed aircraft bolts aircraft bonding aircraft call sign aircraft cannon aircraft capacity aircraft captain, aircraft commander aircraft carrier aircraft ceiling aircraft classification aircraft classification number ...
maximum ramp weight 最 大滑行重量 215、nose taxi lamp 前滑行灯 232、basic operating weight 基本重量 216、right navigation lamp 右航行灯 233、maximum take-off weight 最大起飞 217、Anti-collision lights (flashing 重量 beacon) 防撞灯(闪光灯) 234、maximum landing weight 最大着陆 218、weather rad ...
Due to new regulations, you’ll also need to provide maximum takeoff weight, basic operating weight, takeoff fuel, fuel consumption en route, and payload details to your ground handler in advance. The flight plan needs to be given to your ground handler so he or she can ...
These methods will only give a rudimentary idea as to how heavy the airplane may become and are intended to allow basic sizing to take place. The second set of methods are more detailed estimations that usually include a mixture of known weights (such as for engines, landing gear components,...
RegisterLog in Sign up with one click: Facebook Twitter Google Share on Facebook AFM (redirected fromAircraft Flight Manual) Category filter: AcronymDefinition AFMAirplane Flight Manual AFMAtomic Force Microscope AFMAtomic Force Microscopy AFMAmerican Federation of Musicians ...
, and more particularly to such an aircraft of selected design and configuration so as to permit the adjustment of its load carrying capability with respect to its basic weight as well as its lift to drag to the end that maximum payload capacity can be realized for a given airframe weight....
The materials fitted in aircraft to increase safety and comfort levels are referred to as aerospace insulation. In severe weather conditions, the aircraft's functions shall be guided by some basic operations and safety measures in the field of weight and temperature terms and overall performance. A...
The gasoline engine was chosen as the basic aircraft engine because it weighed the least. Improvements in gasoline engines included making all engine parts lighter through the use of high-strength materials, boosting engine performance (a supercharger to boost the engine has been designed for that ...
By integrating so-called RSS into the basic aircraft design, equilibrium of pitching increments was achieved with the horizontal tail generating lift rather than download, so that the lift that the wing must produce to carry the weight of the aircraft is reduced. This means a smaller wing with...