Abstract: Disclosed is a chiller including a pull-down procedure or pull-down mode, a sustain procedure or sustain mode and, additionally, a heat-up procedure or heat-up mode or temper mode. This allows the chiller to deliberately and determined heat up content if the starting temperature of the content is below the target temperature for serving the content.

Abstract: The invention relates to An aircraft on-board kitchen module (1) comprising at least one heater and/or cooler with at least one first compartment (2) for drinks and/or food and whose temperature can be conditioned by at least one thermoelectric element (5) having a first and a second heat exchanger (8, 9), one of the heat exchangers (8, 9) forming a cold side and the other heat exchanger (8, 9) forming a hot side of the thermoelectric element (5) such that heat generated by the thermoelectric element (5) is dissipated by a primary coolant from a central cooling system (11) of the aircraft, the primary coolant being supplied via a coolant duct (10) that is selectively supplied with ambient air from the cabin and/or conditioned cold air from the central cooling system (11) of the aircraft.

Abstract: An on-board device for a vehicle, preferably a galley or a bar for an airplane, has at least one visible side wall and at least one paneling for partially or completely concealing a work area of the on-board device. The paneling is adjustable between at least two configurations. The paneling forms or covers at least part of the side wall in a first configuration and conceals the work area partially or completely in a second configuration.

Abstract: The invention relates to An aircraft on-board kitchen module (1) comprising at least one heater and/or cooler with at least one first compartment (2) for drinks and/or food and whose temperature can be conditioned by at least one thermoelectric element (5) having a first and a second heat exchanger (8, 9), one of the heat exchangers (8, 9) forming a cold side and the other heat exchanger (8, 9) forming a hot side of the thermoelectric element (5) such that heat generated by the thermoelectric element (5) is dissipated by a primary coolant from a central cooling system (11) of the aircraft, the primary coolant being supplied via a coolant duct (10) that is selectively supplied with ambient air from the cabin and/or conditioned cold air from the central cooling system (11) of the aircraft.

Abstract: The invention relates to a monitoring system (1) for an aircraft for monitoring mobile accessory devices (2) in the aircraft, in particular rolling containers for an on-board kitchen of the aircraft, comprising at least one stationary sensor device (3) for detecting one of the mobile accessory devices (2) and comprising a central unit (10) for evaluating a current security state of the mobile accessory devices (2) based on detection results (DS) of the at least one stationary sensor device (3) reported to the central unit (10). The monitoring system (1) also comprises at least one mobile sensor device (4) for detecting any accessory device (2) of the mobile accessory devices moving relative to the mobile sensor device (4) within a predetermined distance (E), and for reporting a respective detection result (DM) to the central unit (10).

Abstract: The invention relates to a monitoring system (1) for an aircraft for monitoring mobile accessory devices (2) in the aircraft, in particular rolling containers for an on-board kitchen of the aircraft, comprising at least one stationary sensor device (3) for detecting one of the mobile accessory devices (2) and comprising a central unit (10) for evaluating a current security state of the mobile accessory devices (2) based on detection results (DS) of the at least one stationary sensor device (3) reported to the central unit (10). The monitoring system (1) also comprises at least one mobile sensor device (4) for detecting any accessory device (2) of the mobile accessory devices moving relative to the mobile sensor device (4) within a predetermined distance (E), and for reporting a respective detection result (DM) to the central unit (10).

Abstract: Embodiments of the present disclosure relate generally to the use of the fuel cell systems on board aircraft and other passenger transportation vehicles and to methods of using heat, air, and water generated by such fuel cell systems. The heat may be used to address condensation within the aircraft. The heat may be used to help evaporate excess water that would otherwise condense in the aircraft skin. The excess water collected may be used to create humidification for cabin air. In other examples, the heat, warmed air, or warmed water may be delivered to other locations or heating systems for beneficial use.

Abstract: An on-board device for a vehicle, preferably a galley or a bar for an airplane, has at least one visible side wall and at least one paneling for partially or completely concealing a work area of the on-board device. The paneling is adjustable between at least two configurations. The paneling forms or covers at least part of the side wall in a first configuration and conceals the work area partially or completely in a second configuration.

Abstract: Described are inerting systems that may be used on board an aircraft or other passenger transportation vehicle to reduce a risk of fire due to electronic components or to other elements in a compartment and to assist in preventing or extinguishing any fire or hazardous condition that may occur. The systems include a source of inert gas such as oxygen depleted air generated from a fuel cell on board the aircraft. The oxygen depleted air or other inert gas is conveyed through ducts to compartments that house the electronics, thus changing the conditions in the compartment to be less conducive to fire.

Abstract: Described are inerting systems that may be used on board an aircraft or other passenger transportation vehicle to reduce a risk of fire due to electronic components or to other elements in a compartment and to assist in preventing or extinguishing any fire or hazardous condition that may occur. The systems include a source of inert gas such as oxygen depleted air generated from a fuel cell on board the aircraft. The oxygen depleted air or other inert gas is conveyed through ducts to compartments that house the electronics, thus changing the conditions in the compartment to be less conducive to fire.

Abstract: Embodiments of the present disclosure relate generally to the use of the fuel cell systems on board aircraft and other passenger transportation vehicles and to methods of using heat, air, and water generated by such fuel cell systems. The heat may be used to address condensation within the aircraft. The heat may be used to help evaporate excess water that would otherwise condense in the aircraft skin. The excess water collected may be used to create humidification for cabin air. In other examples, the heat, warmed air, or warmed water may be delivered to other locations or heating systems for beneficial use.

Abstract: Disclosed is a cooling device (1), in particular for a galley of an aeroplane, comprising a cooling compartment (2) formed by inner walls (12, 13, 14, 15) of the cooling device, holding at least one refrigerated goods container (20), in particular a trolley, and further comprising a cooling air feed device (3) for introducing cooled air into the cooling compartment and a hot air discharge device (4) for discharging heated air (98) from the cooling compartment, wherein a primary flow channel is configured in use with the at least one refrigerated goods container (20) in the cooling compartment (2) between the inner walls (12, 13, 14, 15) of the cooling device and outer walls (22, 23, 24, 25) of the at least one refrigerated goods container (20), to guide a cooling air flow along a primary flow direction, deflected a plurality of limes through the arrangement of inner walls, from the cooling air feed device (3) around the at least one refrigerated goods container (20) to the hot air discharge device (4).

Abstract: A trolley arrangement for a galley of an aircraft has a trolley container in which at least two trolleys can be arranged in a longitudinal direction and a trolley-handling device for pulling and pushing a trolley longitudinally into the trolley container. This device has a linear guide with a stationary guiding bar and a slide movable along the guiding bar longitudinally, a pulling and pushing bar extending along a longitudinal axis, axially fixed on the slide, but rotatable about the longitudinal axis, a hook at a distal end of the pulling and pushing bar remote from the slide, a handling bar axially fixed on the slide or on the pulling and pushing bar, and a joint between the handling bar and the slide or the pulling and pushing bar, so that the handling bar and the pulling and pushing bar are axially connected and are rotationally coupled.

Abstract: The invention relates to a trolley arrangement (1) of a galley of a vehicle, especially of an aircraft, wherein the trolley arrangement (1) comprises a trolley container (2) in which at least two trolleys (3, 4) can be arranged along a longitudinal direction (L), wherein the trolley arrangement (1) furthermore comprises a trolley handling device (5) for pulling and pushing a trolley (3, 4) into the trolley container (2) in the longitudinal direction (L).

Abstract: A hinge arrangement of a door for closing off an opening, such as a housing opening, a partition opening, a wall opening, or the like, having at least one pivot pin connected to the door and oriented vertically in the direction of the housing, wherein the pin can be engaged in a pivot pin receptacle on the housing. The pivot pin can be moved from a retracted position, in which the pivot pin is not engaged in the pivot pin receptacle, by vertical displacement into an extended position in which the pivot pin is engaged in the pivot pin receptacle and is rotatably supported therein. A releasable, spring-loaded locking device acts on the pivot pin and holds the pivot pin in the retracted position.

Abstract: A cabinet provided with a cabinet body having at least one vertical row of superimposed compartments which are separated by shelves and which can be opened and closed with compartment doors articulated on the cabinet. This invention simplifies and substantially reduces the cost of parts and of mounting the cabinet. Thus, a joint rod extending over a height of the cabinet body is assigned to each vertical row of compartments. The shelves are guided by a shoulder in the hinge zone having the joint rod and are fixed vertically on the joint rod by flange sleeves overlooking the upper and/or lower side of the shelves and their shoulder. The compartment doors which are adjusted to the heights of the compartments bear, on their rear surface, in the hinge zone, housings for the flange sleeves and can be covered with a shroud.

Abstract: The invention relates to a hinge arrangement of a door (14) for closing off an opening, such as a housing opening, partition opening, wall opening, or the like, having at least one pivot pin (18a) that is connected to the door (14) and oriented vertically in the direction of the housing (22), wherein the pin can be engaged in a pivot pin receptacle (20a) on the housing (22). The pivot pin (18a) can be moved from a retracted position, in which the pivot pin (18a) is not engaged in the pivot pin receptacle (20a), by vertical displacement into an extended position in which the pivot pin (18a) is engaged in the pivot pin receptacle (20a) and is rotatably supported therein. A releasable, spring-loaded locking device (41) acts on the pivot pin (18a) and holds the pivot pin (18a) in the retracted position.

Abstract: A switching cabinet with a switching cabinet housing delimited at a top by an upper cover plate and having at least one switching cabinet door on a front surface. A plurality of transport eyes are attached to the top of the switching cabinet housing that can be covered by a detachably fastenable roof. The transport eyes include angle elements that each have one leg which protrudes from the upper cover plate and that has a through bore, and one fastening leg oriented at an angle. The fastening legs of at least a portion of the angle elements each have a fastening region with which they are attached to the top of the switching cabinet housing and a holding region with which they engage behind an edge profile formed onto the roof.

Abstract: A closure for multi-point locking of doors or wall parts in housings or cabinets by a—preferably securable—actuating element such as a handle lever comprises a coupling element which is connected with the actuating element mounted in the door or wall so as to be rigid against rotation relative to it and which transforms a rotational movement into a substantially translational movement and which is coupled with a rod that is mounted near the edge of the door or wall so as to be displaceable, one or more locking elements being coupled with the rod by a coupling element, respectively, in such a way that they move from a locked position into an unlocked position (or vice versa) by the displacement of the rod from a first position into a second position, wherein the locking elements and the coupling elements are formed in each instance by a two-armed, one-piece lever, one of whose lever arms is a locking tongue and whose other lever arm is articulated by its end at the rod.

Abstract: A cabinet provided with a cabinet body having at least one vertical row of superimposed compartments which are separated by shelves and which can be opened and closed with compartment doors articulated on the cabinet. This invention simplifies and substantially reduces the cost of parts and of mounting the cabinet. Thus, a joint rod extending over a height of the cabinet body is assigned to each vertical row of compartments. The shelves are guided by a shoulder in the hinge zone having the joint rod and are fixed vertically on the joint rod by flange sleeves overlooking the upper and/or lower side of the shelves and their shoulder. The compartment doors which are adjusted to the heights of the compartments bear, on their rear surface, in the hinge zone, housings for the flange sleeves and can be covered with a shroud.