A cart bay for an aircraft galley structure includes a housing defined by interior surfaces and capable of housing one or more removable galley carts in a secured position. Chilled air is introduced into the cart bay through a plenum of inlet to maintain perishable contents of the galley cart at a safe temperature. The side walls of the cart bay include rubstrip assemblies for guiding the galley carts in and out of the bay, absorbing impact and noise. The rubstrip assemblies may include a corrugated carrier layer behind a solid rubstrip; the corrugated carrier layer includes apertures for controlling and directing the flow of chilled air along the side walls to maximize the exterior surfaces of the galley carts reachable by the chilled air, separating the galley carts from the side walls and allowing chilled air to reach the side exterior surfaces of the galley carts via the apertures.

A galley for an aircraft includes a frame having metal structural members having interior surfaces and panels coupled to and supported by the frame. Each panel has a core and a facesheet having an inner surface. The frame and the panels define a cart compartment configured to receive a galley cart. The interior surfaces of the metal structural members are interior of the inner surface of the corresponding facesheet. The galley includes a cooling system having a supply duct and a return duct along one or more of the panels in flow communication with the cart compartment configured to supply cooled airflow from a heat exchanger. The galley includes insulating panels located in the cart compartment covering the interior surfaces of the corresponding metal structural members.

An aircraft monument for use in a cabin of an aircraft includes a monument assembly and a seat assembly. The monument assembly includes a frame having a plurality of walls defining a compartment. The plurality of walls include a first end wall having a forward section at a forward plane of the frame. The compartment is defined rearward of the forward section. The seat assembly is forward of the frame. The seat assembly has a shell configured to at least partially surround a passenger seat. The shell has a rear rearward of the forward plane of the frame.

A galley refrigeration system is provided in which a galley cart is positioned in the cavity of a galley compartment comprising at least a cart-facing opening positioned in a vertically intermediate region of the back wall, the galley cart or the galley compartment having a duct-facing opening positioned adjacent to the cart-facing opening. A heat exchanger configured to generate cooling air is provided within the galley compartment, adjacent the vertically intermediate region of the back wall of the galley compartment defining the cavity. An air supply duct, provided at the cart-facing opening, is configured to guide the cooling air from the heat exchanger into the galley cart, and configured to be detachably coupled to the duct-facing opening of the cart or the galley compartment. An electronically actuated valve controls a variable flow rate of the cooling air from the air supply duct into the galley cart.

A system may include an aircraft galley, which may include a standard unit meal box compartment configured to hold a standard unit meal box. The standard unit meal box compartment may include a door at a front of the standard unit meal box compartment and an air chiller near a rear of the standard unit meal box compartment. The air chiller may be configured to provide chilled air within the standard unit meal box compartment.

A galley refrigeration system is provided in which a galley cart is positioned in the cavity of a galley compartment comprising at least a cart-facing opening positioned in a vertically intermediate region of the back wall, the galley cart or the galley compartment having a duct-facing opening positioned adjacent to the cart-facing opening. A heat exchanger configured to generate cooling air is provided within the galley compartment, adjacent the vertically intermediate region of the back wall of the galley compartment defining the cavity. An air supply duct, provided at the cart-facing opening, is configured to guide the cooling air from the heat exchanger into the galley cart, and configured to be detachably coupled to the duct-facing opening of the cart or the galley compartment. An electronically actuated valve controls a variable flow rate of the cooling air from the air supply duct into the galley cart.

A system may include a heating element configured to heat a fluid, the fluid configured to heat a food or drink product. The system may include one or more fluid temperature monitoring components configured to monitor a temperature of the fluid while the fluid is heated by the heating element and configured to control the fluid temperature by controlling the heating element. The system may include one or more control units configured to control operation of an aircraft galley insert via one or more control signals. The system may include one or more heating element temperature limiters configured to maintain a temperature of the heating element below a select heating temperature limit. The system may include one or more heating element temperature monitoring components configured to provide information of a heating element temperature to the one or more heating element temperature limiters.

An air return duct and air return duct grille for a chiller in an aircraft galley has articulated slats that are biased to open during chilling cycles and close during defrost cycles. In the closed orientation, the articulated slats divert any condensate from the chiller to a collection hose; in the open orientation, the articulated slates allow unrestricted airflow. The articulated slats may include a passive biasing element to bias the articulated slats into an open or closed orientation as necessary. The air return duct may also include air return duct grills without articulated slates to allow unobstructed air flow when the articulated slats are in a closed orientation.

A method and apparatus for drying objects in low-volume enclosed spaces is disclosed. In one embodiment, the apparatus is a hand dryer that comprises a dryer cavity including an input port, an exhaust port, and an opening for insertion of a hand having moisture thereon, an air channel, pneumatically coupling the exhaust port of the dryer cavity to the input port of the dryer cavity, the air channel substantially isolated from an interior volume of the lavatory, and a blower, communicatively coupled to the air channel, for moving air through the air channel and the dryer cavity.