{
  "$type": "site.standard.document",
  "coverImage": {
    "$type": "blob",
    "ref": {
      "$link": "bafkreifw7qgx3v7lj3pnubfgmmwyq2qlkcvzghikfqc77dkud4ybantezm"
    },
    "mimeType": "image/png",
    "size": 111956
  },
  "description": "An aircraft power distribution system according to an exemplary aspect of the present disclosure includes, among other things, a power source 14, a load 20, 22, and a power distribution panel 12 receiving power from the power source 14 and selectively providing power to the load 20, 22. The power…",
  "path": "/patents/932862",
  "publishedAt": "2016-12-28T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B60R16/005",
    "HAMILTON SUNDSTRAND CORP [US]"
  ],
  "textContent": "An aircraft power distribution system according to an exemplary aspect of the present disclosure includes, among other things, a power source 14, a load 20, 22, and a power distribution panel 12 receiving power from the power source 14 and selectively providing power to the load 20, 22. The power distribution panel 12 includes a contactor 18 having a housing. A heat sink 58 provides a portion of the housing.",
  "title": "POWER DISTRIBUTION PANEL HAVING CONTACTOR WITH THERMAL MANAGEMENT FEATURE"
}