| 摘要 |
The invention provides a mixing faucet system for an aircraft capable of minimizing as much as possible the size of the portion visible to the user, to thereby enhance the design flexibility of the wash basin and the lavatory including the wash basin. A mixing faucet system 1 for an aircraft comprises a discharge unit 2 of hot and cold water disposed on the wash basin in a lavatory of an aircraft, and a supply unit 3 separated from the discharge unit 2 and provided at a remote location from the wash basin for supplying to the discharge unit 2 through a hose 4 cold water and hot water either independently or in a mixed state. The discharge unit 2 is not equipped with a mixing function, and the supply unit 3 provided with the mixing function can be placed at a position remote from the discharge unit 2. Therefore, the discharge unit 2 is the only portion of the mixing faucet system visible to the user in the lavatory unit, and therefore, the flexibility and freedom of design of the discharge unit 2 itself, the wash basin and the lavatory unit including the same can be improved.
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