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Water supply system, method for preventing freezing or icing and aircraft
The invention relates to a water supply system, a method for preventing freezing or icing and an aircraft. A water supply system (12) for use in an aircraft (10) and a method for preventing obstruction in a water supply system (12) in an aircraft (10) are described. The system (12) comprises: a central tank (14) comprising a fluid inlet (16) and a fluid outlet (20); a supply duct (24) for allowing fluid to flow from the outlet (20) of the central tank (14) to the user equipment (26) wherein at least a section of the supply duct (24) is connected and thermally coupled to the aircraft air conduit (32) so as to enable heat energy to be transferred from the aircraft air conduit to the supply duct (24), the temperature of the water in the supply conduit (24) is kept above the freezing point temperature of the water.
本发明涉及水供应系统、用于防止发生冻结或结冰的方法及飞行器。本发明描述了用于在飞行器(10)中使用的水供应系统(12)以及用于防止飞行器(10)中的水供应系统(12)中发生阻塞的方法。该系统(12)包括：中央水箱(14)，该中央水箱包括流体入口(16)和流体出口(20)；供应导管(24)，该供应导管用于允许流体从中央水箱(14)的出口(20)流动至用户设备(26)，其中，供应导管(24)的至少一部段连接和热联接至飞行器空气管道(32)，以便使得能够从飞行器空气管道向供应导管(24)传递热能，以将供应导管(24)中的水的温度保持在水的冰点温度以上。
Water supply system, method for preventing freezing or icing and aircraft
The invention relates to a water supply system, a method for preventing freezing or icing and an aircraft. A water supply system (12) for use in an aircraft (10) and a method for preventing obstruction in a water supply system (12) in an aircraft (10) are described. The system (12) comprises: a central tank (14) comprising a fluid inlet (16) and a fluid outlet (20); a supply duct (24) for allowing fluid to flow from the outlet (20) of the central tank (14) to the user equipment (26) wherein at least a section of the supply duct (24) is connected and thermally coupled to the aircraft air conduit (32) so as to enable heat energy to be transferred from the aircraft air conduit to the supply duct (24), the temperature of the water in the supply conduit (24) is kept above the freezing point temperature of the water.
本发明涉及水供应系统、用于防止发生冻结或结冰的方法及飞行器。本发明描述了用于在飞行器(10)中使用的水供应系统(12)以及用于防止飞行器(10)中的水供应系统(12)中发生阻塞的方法。该系统(12)包括：中央水箱(14)，该中央水箱包括流体入口(16)和流体出口(20)；供应导管(24)，该供应导管用于允许流体从中央水箱(14)的出口(20)流动至用户设备(26)，其中，供应导管(24)的至少一部段连接和热联接至飞行器空气管道(32)，以便使得能够从飞行器空气管道向供应导管(24)传递热能，以将供应导管(24)中的水的温度保持在水的冰点温度以上。
Water supply system, method for preventing freezing or icing and aircraft
水供应系统、用于防止发生冻结或结冰的方法及飞行器
MATTHIAS HEGENBART (author) / ALBERS FR ¨ (author)
2024-11-05
Patent
Electronic Resource
Chinese
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