发明名称 EMERGENCY POWER GENERATION VIA LIMITED VARIABLE PITCH FAN BLADE
摘要 A method of generating emergency power includes identifying a power-loss condition. In the power-loss condition, a desired quantity of power is determined Emergency power is generated from a turbofan section of the aircraft's engine. The turbofan has a plurality of blades, which have a variable pitch that can be adjusted as a function of the desired quantity of power and actual generated emergency power.
申请公布号 US2015158597(A1) 申请公布日期 2015.06.11
申请号 US201414553793 申请日期 2014.11.25
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 Suciu Gabriel L.;Lord Wesley K.
分类号 B64D41/00;F02C3/107;B64C11/30;F02K3/075;F01D21/14 主分类号 B64D41/00
代理机构 代理人
主权项 1. A gas turbine engine comprising: a low pressure spool including: a low spool shaft; anda fan section, the fan section comprising a plurality of adjustable fan blades and configured to co-rotate with the low pressure shaft; a high pressure spool including a high spool shaft, wherein the high pressure spool is configured to co-rotate with the low pressure spool during a power-loss condition; a generator coupled to the high pressure spool and configured to generate power; and a controller configured to adjust a pitch of the plurality of adjustable fan blades during the power-loss condition.
地址 Hartford CT US