An aircraft galley system is configured with a GAIN to GAIN network that allows for data exchange and communication between each GAIN on the system. By omitting reliance on a galley network controller for acquisition of GAIN data, the present system is simpler, lighter, and more cost-effective. Each
An aircraft galley system is configured with a GAIN to GAIN network that allows for data exchange and communication between each GAIN on the system. By omitting reliance on a galley network controller for acquisition of GAIN data, the present system is simpler, lighter, and more cost-effective. Each GAIN may be polled for data by any other GAIN, such as via a data port, dedicated bus, or wireless connection. The data acquisition between the GAIN and a data collection and display device may be wired in network, wired out of network, or through a wireless link such as a Wi-Fi network.
대표청구항▼
1. An adaptive aircraft galley network, comprising: a plurality of galley powered inserts (hereafter “powered GAINS”) comprising a network interface, a controller in communication with the network interface, a sensor monitoring a status of the powered GAIN, an actuator controlled by the controller,
1. An adaptive aircraft galley network, comprising: a plurality of galley powered inserts (hereafter “powered GAINS”) comprising a network interface, a controller in communication with the network interface, a sensor monitoring a status of the powered GAIN, an actuator controlled by the controller, a user interface including a display, and a power interface with power conversion circuitry;a digital data bus connecting each powered GAIN in the network to each other powered GAIN in the network; andwherein the powered GAINs in the network read and display data of any powered GAIN in the network, and where the display of the other powered GAINS in the network does not rely on a galley network controller. 2. The adaptive aircraft galley network of claim 1, wherein the sensor is selected from a group comprising current, voltage, and temperature. 3. The adaptive aircraft galley network of claim 1, wherein the actuator is an electro-mechanical actuator. 4. The adaptive aircraft galley network of claim 1, wherein the display is operatively connected to a powered GAIN by connecting to a data port in the network via a cable. 5. The adaptive aircraft galley network of claim 1, wherein the display is operatively connected to a powered GAIN through a wireless data connection. 6. The adaptive aircraft galley network of claim 5, wherein the wireless connection between the display and a powered GAIN is a bluetooth connection. 7. The adaptive aircraft galley network of claim 5, wherein the wireless connection between the display and a powered GAIN is across a local WiFi network. 8. The adaptive aircraft galley network of claim 5, wherein the wireless connection between the display and a powered GAIN uses passive infrared signals. 9. The adaptive aircraft galley network of claim 1, wherein the display is a hand-held unit. 10. The adaptive aircraft galley network of claim 1, wherein data specific to a powered GAIN's operation pertains to a group comprising maintenance and fault data. 11. The adaptive aircraft galley network of claim 1, wherein each powered GAIN recognizes all other powered GAINs connected in the network.
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이 특허에 인용된 특허 (5)
Aronson, William D.; Dettmer, Joseph C.; Ramus, Sebastien A., Adaptive power management system for aircraft galleys.
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