{
  "$type": "site.standard.document",
  "coverImage": {
    "$type": "blob",
    "ref": {
      "$link": "bafkreiap4c3ha5qjinbrzeqol73vyib2fyl4gsskyqduxvla2zy4lexp5y"
    },
    "mimeType": "image/png",
    "size": 102174
  },
  "description": "Combustor mounting structures (400; 500; 600; 700; 800; 900; 1000; 1100; 1200) for gas turbine engines (300) are described. The combustor mounting structures (400; 500; 600; 700; 800; 900; 1000; 1100; 1200) include a shell portion (326; 402; 502; 602; 702; 802; 902; 1002; 1102; 1202) defining an…",
  "path": "/patents/1433201",
  "publishedAt": "2023-05-31T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D11/001",
    "RAYTHEON TECH CORP [US]"
  ],
  "textContent": "Combustor mounting structures (400; 500; 600; 700; 800; 900; 1000; 1100; 1200) for gas turbine engines (300) are described. The combustor mounting structures (400; 500; 600; 700; 800; 900; 1000; 1100; 1200) include a shell portion (326; 402; 502; 602; 702; 802; 902; 1002; 1102; 1202) defining an outer ring arranged at an outer radius relative to a central axis, a combustor connection element (320; 404; 508; 608; 708; 808; 908; 1008; 1108; 1208) defining an inner ring arranged at an inner radius that is less than the outer radius relative to the central axis, and a plurality of struts (328; 406; 506; 606; 706; 806; 906; 1006; 1106; 1206) extending radially between and connecting the shell portion (326; 402; 502; 602; 702; 802; 902; 1002; 1102; 1202) to the combustor connection element (320; 404; 508; 608; 708; 808; 908; 1008; 1108; 1208), wherein one or more flow apertures (410) are defined between the shell portion (326; 402; 502; 602; 702; 802; 902; 1002; 1102; 1202) and the combustor connection element (320; 404; 508; 608; 708; 808; 908; 1008; 1108; 1208) in a radial direction and between adjacent struts of the plurality of struts (328; 406; 506; 606; 706; 806; 906; 1006; 1106; 1206) in a circumferential direction.",
  "title": "COMBUSTOR MOUNTING STRUCTURES FOR GAS TURBINE ENGINES"
}