{
  "$type": "site.standard.document",
  "description": "The present invention pertains to a power management system (100), comprising an electrical power supply input (SV) configured to be coupled to an electrical power supply, a first power supply bus bar (B2) coupled to the power supply input, a power management device (1) coupled to the first power…",
  "path": "/patents/960278",
  "publishedAt": "2015-06-03T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B60R16/03",
    "AIRBUS OPERATIONS GMBH [DE]"
  ],
  "textContent": "The present invention pertains to a power management system (100), comprising an electrical power supply input (SV) configured to be coupled to an electrical power supply, a first power supply bus bar (B2) coupled to the power supply input, a power management device (1) coupled to the first power supply bus bar, at least one primary electrical equipment (4a to 4k) including a primary load being coupled in parallel to the power management device, and at least one secondary electrical equipment (3a to 3m) including a secondary load being coupled in parallel to the power management device, wherein the power manager device is configured to supply electrical power to the at least one secondary electrical equipment, to supply electrical power to the at least one primary electrical equipment, and to deactivate the power supply to the at least one secondary electrical equipment, as long as the at least one primary electrical equipment is supplied with electrical power.",
  "title": "Aircraft power management system and method for managing power supply in an aircraft"
}