Galley control system of aircraft
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.
1. A galley control system of an aircraft comprising:
an insert equipment having a visible light receiving element and an IR emitting element and disposed in the galley of an aircraft; and
a galley controller for controlling the insert equipment disposed in the galley or in a circumference thereof and having a visible light emitting panel, an IR receiving element and a display/control panel,
wherein the galley control system is equipped with a mutual communication function between the galley controller and the insert equipment and a remote control function for controlling the insert equipment from the galley controller via transmission of visible light communication data from the visible light emitting panel of the galley controller to the visible light receiving element of the insert equipment and via transmission of IR communication data from the IR emitting element of the insert equipment to the IR receiving element of the galley controller,
the visible light emitting panel of the galley controller has both the function to emit light for transmitting visible light communication data to the insert equipment and a function to emit light for illuminating the interior of the galley,
the visible light receiving sensor and the IR emitting element of the insert equipment are disposed on a front panel thereof, and the visible light emitting panel and the IR receiving element of the galley controller is either disposed to face the front panel of respective insert equipments or on a ceiling or at a high position close to the ceiling within the galley or in a circumference area thereof, and
the insert equipment is provided with an ID for correctly performing identification of various insert equipments, and the insert equipment corresponding to the ID is associated when performing communication.
2. The galley control system of an aircraft according to claim 1 , wherein
a deflection angle conversion element for changing a deflection angle of visible light and IR light entering or exiting the insert equipment is disposed on an upper side of the visible light receiving sensor and the IR emitting element of the insert equipment, and the deflection angle conversion element is provided with a mechanism for varying a mounting angle of the deflection angle conversion element, in order for the insert equipment to perform visible light and IR light communication at a precise position.
3. The galley control system of an aircraft according to claim 1 , wherein
a back light emission of the display/control panel is used instead of the visible light emitting panel of the galley controller for illuminating the interior of the galley and for transmitting the visible light communication data.
4. The galley control system of an aircraft according to claim 2 , wherein
a back light emission of the display/control panel is used instead of the visible light emitting panel of the galley controller for illuminating the interior of the galley and for transmitting the visible light communication data.