Invention Application
US20170003029A1 FUEL NOZZLE WITH FLEXIBLE SUPPORT STRUCTURES 审中-公开
燃油喷嘴与柔性支撑结构

FUEL NOZZLE WITH FLEXIBLE SUPPORT STRUCTURES
Abstract:
A fuel nozzle apparatus for a gas turbine engine includes: a fuel discharge element having a discharge orifice communicating with a fuel supply connection; a static supporting structure; and a cantilevered flexible support structure interconnecting the supporting structure and the fuel discharge element, the flexible support structure having a first end connected to the static supporting structure, and a second end connected to the fuel discharge element.
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