초록 ▼

A galley chiller system for an aircraft includes at least one condenser having a refrigerant fluid. The fluid within the condenser rejects heat to a first surrounding environment. To more efficiently use the condenser of the galley chiller system and reduce the requirement on other cooling systems w

A galley chiller system for an aircraft includes at least one condenser having a refrigerant fluid. The fluid within the condenser rejects heat to a first surrounding environment. To more efficiently use the condenser of the galley chiller system and reduce the requirement on other cooling systems within an aircraft, the condenser may reject its heat to a desired location using a heat exchanger. The galley chiller system includes at least one evaporator that receives fluid from the condenser. A first evaporator absorbs heat from a galley, which may include a bank of carts. The first evaporator is arranged in ducting that carries cooled air to the carts. A second evaporator may absorb heat from a cabin recirculation air duct of the aircraft cooling system. In this manner, the evaporators of the inventive galley chilling system cools not only the galley carts but also provides supplemental cooling to the aircraft cooling system thereby reducing its cooling requirements.

대표청구항 ▼

What is claimed is: 1. A galley chiller system for an aircraft comprising: at least one condenser having a fluid, said fluid in said at least one condenser rejecting heat to a first surrounding environment; at least one evaporator receiving said fluid from at least one condenser, said fluid in sai

What is claimed is: 1. A galley chiller system for an aircraft comprising: at least one condenser having a fluid, said fluid in said at least one condenser rejecting heat to a first surrounding environment; at least one evaporator receiving said fluid from at least one condenser, said fluid in said evaporator absorbing heat from a second surrounding environment including a galley cart and a third surrounding environment including an air duct of an aircraft cooling system, said at least one evaporator including a first evaporator absorbing heat from said second surrounding environment, and a second evaporator absorbing heat from said third surrounding environment; a recirculation evaporator control valve; a controller connected to said control valve controlling a flow of fluid through said control valve into said evaporators to obtain a desired proportion of fluid flow between said evaporators; and a temperature sensor in said third surrounding environment detecting a temperature with said temperature sensor connected to said controller, said controller commanding said control valve in response to said temperature. 2. A galley chiller system for an aircraft comprising: at least one condenser having a fluid, said fluid in said at least one condenser rejecting heat to a first surrounding environment; at least one evaporator receiving said fluid from at least one condenser, said fluid in said evaporator absorbing heat from a second surrounding environment including a galley cart and a third surrounding environment including an air duct of an aircraft cooling system, said at least one evaporator including a first evaporator absorbing heat from said second surrounding environment, and a second evaporator absorbing heat from said third surrounding environment; a recirculation evaporator control valve; and a controller connected to said control valve controlling a flow of fluid through said control valve into said evaporators to obtain a desired proportion of fluid flow between said evaporators, wherein opening said control valve increases the absorption of heat from the air duct, and closing said control valve increases the absorption of heat from the galley cart. 3. The galley chiller system according to claim 2, wherein opening said control valve decreases the flow of fluid to said first evaporator and increases the flow of fluid to said second evaporator, and closing said control valve increases the flow of fluid to said first evaporator and decreases the flow of fluid to said second evaporator. 4. The galley chiller system according to claim 2, wherein opening said control valve decreases a load on said aircraft cooling system. 5. A galley chiller system for an aircraft comprising: at least one condenser having a fluid, said fluid in said at least one condenser rejecting heat to a first surrounding environment; at least one evaporator receiving said fluid from at least one condenser, said fluid in said evaporator absorbing heat from a second surrounding environment including a galley cart and a third surrounding environment including an air duct of an aircraft cooling system; and an air conditioning pack having a ram air duct with a liquid heat exchanger arranged in said ram air duct, said heat exchanger including a liquid cooling passage extending in a loop between said heat exchanger and said condenser, said fluid cooling passage at least partially defining said first surrounding environment.