{
  "$type": "site.standard.document",
  "description": "An aircraft flight attitude display device includes a central processing unit (CPU), a display unit electrically connected to the CPU for showing an aircraft image therein, a flight data receiver unit electrically connected to the CPU, a sky obstacle data receiver unit electrically to the CPU, a…",
  "path": "/patents/1330316",
  "publishedAt": "2022-10-27T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "G01C23/005",
    "HUNG-HSIN LIN"
  ],
  "textContent": "An aircraft flight attitude display device includes a central processing unit (CPU), a display unit electrically connected to the CPU for showing an aircraft image therein, a flight data receiver unit electrically connected to the CPU, a sky obstacle data receiver unit electrically to the CPU, a ground obstacle data receiver unit electrically connected to the CPU, and a power supply unit electrically connected to the CPU. With these arrangements, the aircraft flight attitude display device aids a pilot in making quick and correct judgment about the aircraft flight attitude relative to the sky and the ground, so as to upgrade the aviation safety.",
  "title": "AIRCRAFT FLIGHT ATTITUDE DISPLAY DEVICE"
}