{
  "$type": "site.standard.document",
  "description": "A gas turbomachine inlet system (20) includes a duct member (24) having an inlet portion fluidically coupled to an outlet portion (32) through an intermediate portion (34). The inlet portion, outlet portion, and intermediate portion define a fluid flow zone (37). A throttling system (40) is…",
  "path": "/patents/982494",
  "publishedAt": "2013-10-30T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D17/146",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "A gas turbomachine inlet system (20) includes a duct member (24) having an inlet portion fluidically coupled to an outlet portion (32) through an intermediate portion (34). The inlet portion, outlet portion, and intermediate portion define a fluid flow zone (37). A throttling system (40) is arranged in the duct member at one of the inlet portion, outlet portion and intermediate portion. The throttling system is configured and disposed to selectively establish a pressure drop through the fluid flow zone. A method of controlling inlet pressure drop through an inlet system for a gas turbomachine is also described herein.",
  "title": "Gas turbine inlet system and method"
}