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 |