几乎更换了左侧主起落架内侧轮胎。
轮挡已安放在前起落架和主起落架处。
我们失去了前起落架和右侧主起落架的应答信号。
We've also lost the nose-gear down talkback, and right-main-gear down talkback.
右侧主起落架有漏油迹象。
检查发现左主起落架一液压管漏油超标。
向后滑门对主起落架左舷船尾，操作步骤如下。
Rearward-sliding door aft of main landing gear on port side, with steps below.
扼要地介绍了对某型主起落架结构的损伤容限特性研究。
A brief introduction to the study of damage tolerance behaviour of one type of main landing gear structure is given in this paper.
刹车系统由四个刹车组件组成，一个安装在每个主起落架舱。
Braking is provided by four brake assemblies, one mounted on each main gear wheel.
本文对主起落架轴裂纹产生的原因进行了分析，裂纹为磨削裂纹。
This paper deals with the cause of crack appearing on main landing gear axis. It shows that the cracks belong to the grinding ones.
每个主起落架支柱具有一部双机轮组件，主起落架支柱安装在机翼结构中。
The MLG legs, each with a twin-wheel assembly, are installed in the wings.
本文分析了B757飞机右主起落架后轮轴断裂原因、腐蚀状态及防腐措施。
This paper analyses the cracking cause, corrosion condition and anticorrosion measurements of the backaxle of aircraftB757 main landing gear.
当主起落架伸出时，一部侧向保持组件防止起落架侧向移动，并帮助保持在伸出位置。
When an MLG is extended, a side-stay assembly prevents sideways movement of the MLG and helps keep it extended.
主起落架机轮使用多盘碳刹车，正常情况使用绿色液压系统，备用刹车使用黄色液压系统。
The Main Landing Gear wheels have multi-disc carbon brakes using Green hydraulic pressure for normal operation and Yellow hydraulic pressure through an alternate braking system.
主起落架收入机身一侧的起落架舱，这意味着很可能其前面有类似F-22 的机侧武器舱。
The main landing gears retract into body-side bays, indicating the likely presence of F-22-style side weapon bays ahead of them.
使用上述模型，分别进行了主起落架落震仿真试验和全机着陆仿真试验，用以模拟真实的起落架落震和全机着陆情况，并将二者得到的主起落架仿真结果进行了对比。
The above models are used to simulate the dropping test of the main landing gear and landing test of the aircraft. The two results have a good correspondence.
它们可以给电力驱动的起落架轮子动力，让飞机不用主引擎就能在地面滑行。
They could power electrically driven wheels, letting an aircraft taxi without using its main engines.
它们可以给电力驱动的起落架轮子动力，让飞机不用主引擎就能在地面滑行。
They could power electrically driven wheels, letting an aircraft taxi without using its main engines.
应用推荐