{
  "$type": "site.standard.document",
  "description": "Landing gear strut (1) for an aircraft comprising a main part (1a) extending along a main axis (X-X) of the strut and comprising an axle axis (1b) extending in a plane (P) perpendicular to the main axis (1a) of the strut, this axle axis (1b) being arranged to support at least one landing wheel (2a…",
  "path": "/patents/932576",
  "publishedAt": "2017-01-04T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B60B35/02",
    "SAFRAN LANDING SYSTEMS [FR]"
  ],
  "textContent": "Landing gear strut (1) for an aircraft comprising a main part (1a) extending along a main axis (X-X) of the strut and comprising an axle axis (1b) extending in a plane (P) perpendicular to the main axis (1a) of the strut, this axle axis (1b) being arranged to support at least one landing wheel (2a, 2b) equipped with brakes (3a, 3b) to brake the wheel, said axle axis (1b) being made of steel. [0002] The axle axis (1b) carries at least one coating layer (C) made of an alloy of Zinc and Nickel, this Zinc and Nickel alloy comprising, as a percentage by mass of the alloy, between 12% and 18% nickel, at most 0.5% of elements other than Nickel and zinc, the remainder being zinc.",
  "title": "AIRCRAFT LANDING GEAR AXLES COATED IN ZINC-NICKEL ALLOY"
}