发明名称 IMAGE CONDUIT FOR FUEL NOZZLE ASSEMBLIES
摘要 A fuel nozzle for a gas turbine engine includes a feed arm including a fuel passage for issuing a spray of fuel. A nozzle assembly is fixed at an upstream end of the feed arm having a fuel inlet in fluid communication with the fuel passage. A fiber optic cable is configured to collect burner radiation for a pyrometer input and has a first end centered within an optical connector of the nozzle assembly and a second end exposed from the spray outlet. The fiber optic cable fitted within the feed arm and nozzle assembly has a permanent bend radius preformed in the fiber optic cable. The bend radius can be equal to or greater than the minimum bend radii for the fiber optic cable to serve as a wave guide in wavelengths for monitoring combustion.
申请公布号 US2017038073(A1) 申请公布日期 2017.02.09
申请号 US201514821284 申请日期 2015.08.07
申请人 Delavan Inc 发明人 Paradise Bruce D.
分类号 F23R3/28;G01J5/00;G01J5/08;G02B6/44 主分类号 F23R3/28
代理机构 代理人
主权项 1. A fuel nozzle for a gas turbine engine, comprising: a feed arm including a fuel passage for issuing a spray of fuel; a nozzle assembly fixed at an upstream end of the feed arm having a fuel inlet in fluid communication with the fuel passage; and a fiber optic cable configured to collect burner radiation for a pyrometer input having a first end centered within an optical connector of the nozzle assembly and a second end exposed from the spray outlet, wherein the fiber optic cable fitted within the feed arm and nozzle assembly has a permanent bend radius preformed in the fiber optic cable.
地址 West Des Moines IA US