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The water extractor is made from light alloy or fiberglass, and contains static swirl vanes and a water drain inside a body. Swirl vanes centrifuge the water droplets in the air to the inner surface of the water extractor body. The water collects at the lowest point of the body. It is then drained to ducts which leads to the water injectors which spray the water into the ram airflow. This helps the cooling capacity through the process of evaporation.
The water extractor is made from light alloy or fiberglass, and contains static swirl vanes and a water drain inside a body. Swirl vanes centrifuge the water droplets in the air to the inner surface of the water extractor body. The water collects at the lowest point of the body. It is then drained to ducts which leads to the water injectors which spray the water into the ram airflow. This helps the cooling capacity through the process of evaporation.
The configuration of the inserts is related to the dimensions of the connector shell.
The wheel to rudder interconnect system (WTRIS) assists turns during flight control manual reversion operations when both flight control A and B hydraulics are OFF, and the standby system is ON.
The accessory compartments are located on the inner or on the outer areas of the pressurized fuselage.
These windshields are formed to the exact shape required, but are slightly larger than necessary so they may be trimmed to the exact size.
Each approved word in the dictionary has a specified approved meaning which can be more restricted than its meaning in standard English.
Sometimes a work step is only applied to some special conditions.
偏航阻尼器是一个重要的装置， 它帮助改进飞机的整体稳定性和操纵性， 尤其是在起降等关键阶段。
The yaw damper works by sensing any yaw motion and then applying corrective inputs to the aircraft＇s rudder to reduce or eliminate any unwanted yawing. It is particularly useful in minimizing the effects of turbulence or other external disturbances that can cause yawing and make the aircraft harder to control. The yaw damper is an important safety feature that helps to improve the overall stability and control of the aircraft, especially during critical phases of flight such as takeoff and landing.
