{
  "$type": "site.standard.document",
  "description": "A method for operating a thrust reverser (202) of an aircraft engine (100), the thrust reverser (202) having a deployed state and a stowed state comprises placing the thrust reverser (202) in the stowed state when the thrust reverser (202) is in the deployed state, a thrust lever (302) associated…",
  "path": "/patents/1410889",
  "publishedAt": "2023-12-06T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02K1/72",
    "PRATT & WHITNEY CANADA [CA]"
  ],
  "textContent": "A method for operating a thrust reverser (202) of an aircraft engine (100), the thrust reverser (202) having a deployed state and a stowed state comprises placing the thrust reverser (202) in the stowed state when the thrust reverser (202) is in the deployed state, a thrust lever (302) associated with the engine (100) is in a forward position (F), and the engine (100) is rotating at a speed below an idle speed, wherein hydraulic pressure for stowing the thrust reverser (202) is provided by a pump (304) driven by the engine (100) rotating at the speed below the idle speed.",
  "title": "METHOD AND SYSTEM FOR THRUST REVERSER OPERATION"
}