Abstract: Provided is an aircraft seat that enhances passenger comfort and reduces the burden on cabin attendants. The aircraft seat includes a base with a relatively movable seat portion and a backrest portion; an actuator for relatively moving the seat portion and the backrest portion; a biometric sensor installed on the base and configured to obtain biometric information of a passenger; a plurality of elastic members installed on the base; a modification device configured to change an elastic force of at least one elastic member, and a control device, wherein the control device operates the actuator or the modification device in response to a signal from the biometric sensor.

Abstract: Provided is an aircraft seat that enhances passenger comfort and reduces the burden on cabin attendants. The aircraft seat includes a base with a relatively movable seat portion and a backrest portion; an actuator for relatively moving the seat portion and the backrest portion; a biometric sensor installed on the base and configured to obtain biometric information of a passenger; a plurality of elastic members installed on the base; a modification device configured to change an elastic force of at least one elastic member, and a control device, wherein the control device operates the actuator or the modification device in response to a signal from the biometric sensor.

Abstract: Provided is a system in which a camera monitors safety of a galley arranged in a cabin of an aircraft. A galley 100 includes a storage space 130 of carts divided by structural members 110, and carts 150 are stored. Turn retainers 200 in closed positions prevent the carts 150 from flying out. Hinged doors 310 are attached to front sides of compartments 300, and latches 320 lock the hinged doors 310. A monitoring camera 500 determines safety or unsafety of the turn retainers 200 and the latches 320 by an image and displays the safety or unsafety on a display device 600 or on a PDA terminal device 800 carried by a cabin attendant CA.

Abstract: Provided is a system in which a camera monitors safety of a galley arranged in a cabin of an aircraft. A galley 100 includes a storage space 130 of carts divided by structural members 110, and carts 150 are stored. Turn retainers 200 in closed positions prevent the carts 150 from flying out. Hinged doors 310 are attached to front sides of compartments 300, and latches 320 lock the hinged doors 310. A monitoring camera 500 determines safety or unsafety of the turn retainers 200 and the latches 320 by an image and displays the safety or unsafety on a display device 600 or on a PDA terminal device 800 carried by a cabin attendant CA.

Abstract: Water leakage of a steam oven provided on an aircraft for heating ingredients is to be prevented. Two solenoid valves 6 and 7 are inserted in series in a water supply circuit of a steam oven. A power switch 12 supplies a 15 V direct current to the solenoid valves 6 and 7. A controller 1 transmits a command to driving circuits 4 and 5 of the solenoid valves according to a signal of a temperature sensor 10 in the oven. An output of a clock generator 14 is counted by a frequency counter and a time in which the valves are opened is counted. When count of a valve opening time becomes longer than a predetermined value, the power switch 12 of the solenoid valves is disconnected to prevent water leakage.

Abstract: A control system is provided that adopts a communication network using wireless visible light and IR light communications in a galley of an aircraft which is subjected to limitations of aviation regulations regarding wired communications. Insert equipments each having a visible light receiving element and an IR emitting element are disposed in a galley of an aircraft, and a galley controller is disposed within the galley or a circumference area thereof having a visible light emitting panel, an IR receiving element and a display/control panel for controlling the insert equipments. A mutual communication function between the galley controller and the insert equipments and a remote control function for controlling the insert equipments from the galley controller are realized via transmission and reception of visible light communication data and IR communication data.

Abstract: A current control circuit (active element) is provided that is connected between a rectifier of a DC power source and a smoothing capacitor in a power frequency converter and that controls a variation in the rectified current caused by a variation in the instantaneous power consumption of the load device. When the rectified current increases, the current control circuit limits the current to have a reference current value or lower and, when the rectified current decreases, the current control circuit increases the current to have a value close to the reference current to thereby suppress the rectified current from the rectifier to a substantially-constant value. This consequently mitigates the influence on the primary power source by the variation in the instantaneous power consumption of the load device, thus clearing the Load Demand Variation specification required for the power source to be used in an aircraft.

Abstract: Water leakage of a steam oven provided on an aircraft for heating ingredients is to be prevented. Two solenoid valves 6 and 7 are inserted in series in a water supply circuit of a steam oven. A power switch 12 supplies a 15 V direct current to the solenoid valves 6 and 7. A controller 1 transmits a command to driving circuits 4 and 5 of the solenoid valves according to a signal of a temperature sensor 10 in the oven. An output of a clock generator 14 is counted by a frequency counter and a time in which the valves are opened is counted. When count of a valve opening time becomes longer than a predetermined value, the power switch 12 of the solenoid valves is disconnected to prevent water leakage.

Abstract: The invention provides a visible light communication apparatus for in-flight entertainment system in an aircraft cabin in which a visible light communication (VLC) system is used for wireless communication of various contents data for in-flight entertainment. The invention provides a visible light communication apparatus for in-flight entertainment system in an aircraft cabin comprising an illuminating apparatus for illuminating the aircraft cabin via light emitted from an OLED element 20, and a visible light communication apparatus 19 for modulating a light quantity of light emitted from the OLED element 20 via electric signals to perform optical communication from an area distribution box 17 to a seat electronics box 18 by modulating the emission of the OLED element 20 so as to construct an in-flight entertainment system for offering information for service to passengers within the aircraft cabin.

Abstract: The invention provides an illuminating device suitable for illuminating a cabin of an aircraft. An OLED illuminating panel 100 is arranged on a ceiling of the cabin of an aircraft in a direction parallel to an axis line of the fuselage to illuminate the interior of the cabin. Further, the OLED illuminating panel is arranged on an upper portion of the window panels in a direction parallel to the axis line of the fuselage to illuminate the interior of the cabin. A control system for controlling the illumination within the cabin includes a central control unit and OLED illuminating panels 100 disposed above window panels and divided into multiple zones within the cabin, which is connected to the central control unit via power/signal lines, wherein the central control unit has a function to change and control the color of the OLED illuminating panels 100 of the respective zones.

Abstract: The invention provides a control system adopting a communication network using wireless visible light and IR light communications in a galley of an aircraft which is subjected to limitations of aviation regulations regarding wired communications. Insert equipments 6a through 6c each having a visible light receiving element and an IR emitting element are disposed in a galley 1 of an aircraft, and a galley controller 2 is disposed within the galley 1 or a circumference area thereof having a visible light emitting panel 4, an IR receiving element 5 and a display/control panel 3 for controlling the insert equipments 6a through 6c. A mutual communication function between the galley controller 2 and the insert equipments 6 and a remote control function for controlling the insert equipments 6a through 6c from the galley controller 2 are realized via transmission and reception of visible light communication data and IR communication data.

Abstract: A current control circuit (active element) is provided that is connected between a rectifier of a DC power source and a smoothing capacitor in a power frequency converter and that controls a variation in the rectified current caused by a variation in the instantaneous power consumption of the load device. When the rectified current increases, the current control circuit limits the current to have a reference current value or lower and, when the rectified current decreases, the current control circuit increases the current to have a value close to the reference current to thereby suppress the rectified current from the rectifier to a substantially-constant value. This consequently mitigates the influence on the primary power source by the variation in the instantaneous power consumption of the load device, thus clearing the Load Demand Variation specification required for the power source to be used in an aircraft.

Abstract: There is provided a highly safe steam oven capable of controlling the amount of steam generated appropriately. Water dripped from a water feeder to the inside of a cooking chamber is converted into steam by a heater in the cooking chamber. The thus generated steam in the cooking chamber is discharged through a steam channel which keeps the inside of the cooking chamber connected to the outside of the steam oven. The temperature of steam passing through the steam channel is measured by a steam temperature measuring device. The amount of water fed from the water feeder is controlled in response to the measured temperature.

Abstract: There is provided a highly safe steam oven capable of controlling the amount of steam generated appropriately. Water dripped from a water feeder to the inside of a cooking chamber is converted into steam by a heater in the cooking chamber. The thus generated steam in the cooking chamber is discharged through a steam channel which keeps the inside of the cooking chamber connected to the outside of the steam oven. The temperature of steam passing through the steam channel is measured by a steam temperature measuring device. The amount of water fed from the water feeder is controlled in response to the measured temperature.

Abstract: A galley 1 has a main body 10 constructed of a panel material, and the galley main body 10 has a table 20, a sink 30, a storage compartment 40 and a service cart housing compartment 60. A hot-water supply unit 100 has a hot-water tank 10 with an electric heater and an electric instantaneous water heater 120 and is supplied with electric power by a control unit 150. The hot-water tank 110 and a hot-water tap 180 are connected via a hot-water supply line 190. In response to a command from a device that manages the electric power in the aircraft, the control unit 150 provides hot water using the instantaneous water heater 120 when the electric power consumption in the aircraft is low.

Abstract: A galley 1 has a main body 10 constructed of a panel material, and the galley main body 10 has a table 20, a sink 30, a storage compartment 40 and a service cart housing compartment 60. A hot-water supply unit 100 has a hot-water tank 110 with an electric heater and an electric instantaneous water heater 120 and is supplied with electric power by a control unit 150. The hot-water tank 110 and a hot-water tap 180 are connected via a hot-water supply line 190. In response to a command from a device that manages the electric power in the aircraft, the control unit 150 provides hot water using the instantaneous water heater 120 when the electric power consumption in the aircraft is low.

Abstract: A door for an amenity receiving section of a lavatory unit for a passenger airplane formed from honey-comb panels the door having a narrow width length plate and a structure wherein one side edge lengthwise thereof is curved, and a straight rigid rod is secured adjacent to the curved side edge lengthwise of the door and having a spring action for pressing a curved convex portion of the door to exert a spring force on the inside of the receiving section.