{
  "$type": "site.standard.document",
  "coverImage": {
    "$type": "blob",
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  "description": "A battery arrangement for integration in a vehicle, in particular an aircraft or spacecraft, comprises two cover plates having battery sockets; a plurality of batteries, which are held on both sides between the cover plates by the battery sockets, wherein the batteries are arranged in battery rows…",
  "path": "/patents/1424649",
  "publishedAt": "2024-01-10T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B60L50/66",
    "AIRBUS DEFENCE & SPACE GMBH [DE]"
  ],
  "textContent": "A battery arrangement for integration in a vehicle, in particular an aircraft or spacecraft, comprises two cover plates having battery sockets; a plurality of batteries, which are held on both sides between the cover plates by the battery sockets, wherein the batteries are arranged in battery rows along the cover plates; and a microchannel tube arrangement having a plurality of thermally conducting tubes configured to dissipate heat from the batteries, wherein a lateral surface of each battery is wrapped in a thermally conductive sheet, which is thermally connected to the microchannel tube arrangement. (Fig. 6)",
  "title": "BATTERY ARRANGEMENT FOR INTEGRATION IN A VEHICLE"
}