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主单元是单轮并收起到机身下轮槽中。
The main units are single-wheeled and retract into wheel troughs in the fuselage.
步骤简要说明包含在主单元。
来自恒温维持装置的主单元(1)的冷却侧水箱(43)的被调整到预定的温度的低温循环液通过供给配管(14)被供给给辅助单元(2)的三通阀(20)。
A cool fluid of a predetermined temperature is supplied to a three-way valve (20) of a sub unit (2) from a cooling side tank (43) of a main unit (1) of a controller, through a supply pipe (14).
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