{
  "$type": "site.standard.document",
  "description": "The method involves applying and manufacturing an abradable coating (20) on a component of a turbomachine by a kinetic cold gas compacting process. The component is a static or rotating component (16) of the turbomachine. An adhesive layer or a thermal insulation- or titanium fire protective layer…",
  "path": "/patents/983518",
  "publishedAt": "2013-10-09T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D11/122",
    "MTU AERO ENGINES AG [DE]"
  ],
  "textContent": "The method involves applying and manufacturing an abradable coating (20) on a component of a turbomachine by a kinetic cold gas compacting process. The component is a static or rotating component (16) of the turbomachine. An adhesive layer or a thermal insulation- or titanium fire protective layer is applied on a to be coated surface of the static or rotating component with the abradable coating to form a composite abradable coating. The adhesive layer or the thermal insulation- or titanium fire protective layer is formed by a thermal spraying process. An independent claim is included for a static or rotating component for a turbomachine with a rotor blade tip.",
  "title": "Method for producing an abradable"
}