{
  "$type": "site.standard.document",
  "description": "An engine system includes a gas turbine engine and an actuation system (26). The gas turbine engine includes a compressor section, a combustor section, a turbine section (39) and a flowpath (34) extending through the compressor section, the combustor section and the turbine section (39). The…",
  "path": "/patents/1393619",
  "publishedAt": "2025-12-03T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C7/264",
    "RTX CORP [US]"
  ],
  "textContent": "An engine system includes a gas turbine engine and an actuation system (26). The gas turbine engine includes a compressor section, a combustor section, a turbine section (39) and a flowpath (34) extending through the compressor section, the combustor section and the turbine section (39). The actuation system (26) includes a fluid reservoir (108), a flow regulator (112) and a flow circuit (110). The flow regulator (112) is configured as or otherwise includes a barrier between the fluid reservoir (108) and the flow circuit (110). The flow regulator (112) is configured to fluidly decouple the fluid reservoir (108) from the flow circuit (110) when the barrier is intact. The flow regulator (112) is configured to fluidly couple the fluid reservoir (108) with the flow circuit (110) when the barrier breaks. The flow circuit (110) is configured to direct gas from the fluid reservoir (108) into the flowpath (34) when the barrier breaks.",
  "title": "GAS TURBINE ENGINE WITH INTEGRAL ACTUATION SYSTEM"
}