{
  "$type": "site.standard.document",
  "description": "A power system for an aircraft having a plurality of power-consuming components, some of which have transient power requirements, which is greater than the average power requirement, the power system includes at least one generator, a power distribution buss, a non-battery power source, a battery…",
  "path": "/patents/1164233",
  "publishedAt": "2016-07-14T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "H02J5/00",
    "GE AVIATION SYSTEMS LLC"
  ],
  "textContent": "A power system for an aircraft having a plurality of power-consuming components, some of which have transient power requirements, which is greater than the average power requirement, the power system includes at least one generator, a power distribution buss, a non-battery power source, a battery power source, and a power controller selectively coupling the non-battery power source and the battery power source to the power distribution buss to satisfy the transient power requirements.",
  "title": "POWER SYSTEM FOR AN AIRCRAFT WITH DUAL HYBRID ENERGY SOURCES"
}