Sustainable Networking Plane De-Energization
US-2024414102-A1 · Dec 12, 2024 · US
US2016342188A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2016342188-A1 |
| Application number | US-201615146969-A |
| Country | US |
| Kind code | A1 |
| Filing date | May 5, 2016 |
| Priority date | May 19, 2015 |
| Publication date | Nov 24, 2016 |
| Grant date | — |
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A portable power device including an enclosure, a plurality of power elements housed within the enclosure, and a controller housed within the enclosure and configured to control the power output of the plurality of power elements. The controller is configured to determine if the portable power device is located on an aircraft that is operating in a stationary, taxiing, or flight mode, and if the aircraft is in the stationary, taxiing, or flight mode, to prevent power to be supplied from the plurality of power elements.
Opening claim text (preview).
What is claimed is: 1 . A portable power device comprising: an enclosure; a plurality of power elements housed within the enclosure; and a controller housed within the enclosure and configured to control the power output of the plurality of power elements, wherein the controller is configured to determine if the portable power device is located on an aircraft that is operating in a stationary, taxiing, or flight mode, and if the aircraft is in the stationary, taxiing, or flight mode, to prevent power to be supplied from the plurality of power elements. 2 . The portable power device of claim 1 , further comprising a switch located within the enclosure and electrically configured between the plurality of power elements and an output of the portable power device. 3 . The portable power device of claim 2 , wherein the controller is configured to control the switch, and if the aircraft is in the stationary, taxiing, or flight mode, the controller controls the switch to disengage and prevent power output from the plurality of power elements. 4 . The portable power device of claim 1 , wherein the determination made by the controller is based on at least one of GPS location, RFID tagging or other RF proximity scheme, manual input, Wi-Fi location determination, and Bluetooth. 5 . The portable power device of claim 1 , further comprising a first output power line from the plurality of power elements and a second output power line from the plurality of power elements. 6 . The portable power device of claim 5 , further comprising a switch electrically configured on the first output power line, the controller configured to control the power output along the first output power line by controlling the switch, and the second output power line configured to continuously supply power even if the controller stops power along the first output power line. 7 . The portable power device of claim 1 , wherein the plurality of power elements comprise a plurality of at least one of (i) batteries, (ii) power cells, and (iii) piezoelectric generators. 8 . A method of controlling power to one or more devices, the method comprising: monitoring the location of a portable power device having a plurality of power elements; determining that the portable power device is located on an aircraft that is stationary, taxiing, or in-flight; and disabling a power output of the plurality of power elements of the portable power device. 9 . The method of claim 8 , wherein the disabling comprising switching a switch located between the plurality of power elements and an output of the portable power device. 10 . The method of claim 8 , wherein the determining comprises one of at least one of GPS locating, RFID or other RF proximity scheme detection, manual input, Wi-Fi location determination, and Bluetooth detection. 11 . The method of claim 8 , wherein the plurality of power elements comprise a plurality of at least one of (i) batteries, (ii) power cells, and (iii) piezoelectric generators.
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