发明名称 ICE TOLERANT GAS TURBINE FUEL SYSTEMS
摘要 A fuel system for a gas turbine engine includes a fuel conditioner. The fuel conditioner has an ice debris separator, a fuel pump, a heat exchanger, and an air oil cooler. The ice debris separator has a fuel inlet and a fuel outlet. The fuel pump connects to the fuel outlet of the ice and debris separator for receiving a fuel flow, pressurizing the fuel flow, and providing the pressurized fuel flow to an outlet of the fuel pump. The heat exchanger is connected to receive pressurized fuel from the fuel pump outlet and has an oil inlet for receiving heated oil, an oil outlet for discharging cooled oil, and a fuel outlet for discharging heated fuel. The air oil cooler is connected to the heat exchanger oil outlet and has an air cooled body configured for further cooling oil from the heat exchanger using an air flow.
申请公布号 US2016298547(A1) 申请公布日期 2016.10.13
申请号 US201415104738 申请日期 2014.11.19
申请人 United Technologies Corporation 发明人 Ripley David Lloyd;Fausett Taylor
分类号 F02C7/224;F01D15/08;F02C7/141 主分类号 F02C7/224
代理机构 代理人
主权项 1. A fuel conditioning system, comprising: an ice debris separator; a fuel pump in fluid communication with the ice debris separator, wherein the fuel pump is downstream of the ice debris separator and configured to receive filtered fuel and output pressurized fuel; and a heat exchanger in fluid communication with the fuel pump, wherein the heat exchanger is downstream from the fuel pump and configured to receive pressurized fuel from the fuel pump.
地址 Farmington CT US