{
  "$type": "site.standard.document",
  "coverImage": {
    "$type": "blob",
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  "description": "A propulsion system for an aircraft (1000) includes a battery (64), a battery management system (68), and an engine controller (28). The battery management system (68) includes a plurality of first battery temperature sensors (110), at least one second battery temperature sensor (110), and a…",
  "path": "/patents/1385960",
  "publishedAt": "2026-06-03T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B60L3/0046",
    "PRATT & WHITNEY CANADA [CA]"
  ],
  "textContent": "A propulsion system for an aircraft (1000) includes a battery (64), a battery management system (68), and an engine controller (28). The battery management system (68) includes a plurality of first battery temperature sensors (110), at least one second battery temperature sensor (110), and a single-channel battery management system (BMS) controller (92). The single-channel BMS controller (92) includes a BMS control channel connected in signal communication with the plurality of first temperature sensors (110). The engine controller (28) includes a first engine control channel (98) and a second engine control channel (100). The first engine control channel (98) is connected in signal communication with the BMS control channel to form a first control lane (142A). The second engine control channel (100) is connected in signal communication with the at least one second battery temperature sensor (110) to form a second control lane (142B).",
  "title": "BATTERY MANAGEMENT SYSTEM, TEMPERATURE SENSING SYSTEMS AND METHODS"
}