{
  "$type": "site.standard.document",
  "description": "A gas turbine engine recuperator (30) including a plurality of independent arcuate segments (32), each segment having an inlet connection member (58) designed to sealingly engage a plenum (28) in fluid flow communication with the compressor discharge, and an outlet connection member (74) designed…",
  "path": "/patents/998877",
  "publishedAt": "2012-08-29T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C7/08",
    "PRATT & WHITNEY CANADA [CA]"
  ],
  "textContent": "A gas turbine engine recuperator (30) including a plurality of independent arcuate segments (32), each segment having an inlet connection member (58) designed to sealingly engage a plenum (28) in fluid flow communication with the compressor discharge, and an outlet connection member (74) designed to sealingly engage a plenum (26) containing the combustor (16). One of the inlet and outlet connection members (74) is a rigid member forming a rigid connection to the respective plenum (26), and the other (56) of the inlet and outlet connection members includes a flexible member (56) and forms a floating connection to the respective plenum (28), the floating connection allowing relative movement between the segment (32) and a remainder of the gas turbine engine.",
  "title": "Gas Turbine Engine Recuperator with Floating Connection"
}