{
  "$type": "site.standard.document",
  "description": "A thrust reverser system for a jet engine has a thrust reverser sleeve lock, preferably for each thrust reverser sleeve, that provides at least one of the redundant anti-deployment mechanisms of the thrust reverser. The thrust reverser sleeve lock has a lock pin that engages a lock pin hole in a…",
  "path": "/patents/1097873",
  "publishedAt": "2003-03-05T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02K1/72",
    "BOEING CO [US]"
  ],
  "textContent": "A thrust reverser system for a jet engine has a thrust reverser sleeve lock, preferably for each thrust reverser sleeve, that provides at least one of the redundant anti-deployment mechanisms of the thrust reverser. The thrust reverser sleeve lock has a lock pin that engages a lock pin hole in a slider of the thrust reverser when the thrust reverser sleeve is in a stowed position and the thrust reverser sleeve lock is in a lock position to prevent the thrust reverser sleeve from deploying. The thrust reverser sleeve lock is located out of a plane in which other anti-deployment mechanisms of the thrust reverser are located.",
  "title": "Thrust reverser sleeve lock"
}