公开(公告)号：US20140125121A1

公开(公告)日：2014-05-08

申请号：US14036721

申请日：2013-09-25

Applicant: ROLLS-ROYCE PLC

Inventor： Huw Llewelyn EDWARDS ,  Parag VYAS ,  Malcolm Laurence HILLEL ,  Alasdair GARDNER ,  Sean Patrick ELLIS ,  Nicholas HOWARTH

IPC: B60R16/03

CPC classification number: B60R16/03 ,  B64D2221/00 ,  H02J4/00 ,  H02J7/1446 ,  Y02T50/54

Abstract: A method of operating an electrical power generation system on an aircraft. The method includes assessing a required electrical power of the aircraft, assessing whether a first and a second electrical power source are able to provide the required electrical power in combination, assessing a predetermined condition, determining an operating mode of the first and second electrical power sources to match the predetermined condition, and operating the first and second electrical power sources according to the determined operating mode.

Abstract translation: 一种在飞机上操作发电系统的方法。 该方法包括评估飞行器的所需电力，评估第一和第二电源是否能够组合提供所需的电力，评估预定条件，确定第一和第二电源的操作模式 以匹配预定条件，并且根据所确定的操作模式操作第一和第二电源。

公开(公告)号：US20150308353A1

公开(公告)日：2015-10-29

申请号：US14688423

申请日：2015-04-16

Applicant: ROLLS-ROYCE PLC

Inventor： Alasdair GARDNER ,  Arthur Laurence ROWE ,  Mark David TAYLOR ,  Nicholas HOWARTH

IPC: F02C9/22 ,  F02C7/36 ,  F02C6/00

CPC classification number: F02C9/22 ,  F01D17/162 ,  F02C6/00 ,  F02C7/36 ,  F02C9/20 ,  F02C9/54 ,  F05D2220/32 ,  F05D2220/76 ,  F05D2270/05 ,  F05D2270/06 ,  F05D2270/303 ,  F05D2270/304 ,  Y02T50/671

Abstract: An engine that has, in axial flow series, booster compressor, core compressor, combustion equipment, core turbine, and low-pressure turbine. Core turbine drives core compressor via an interconnecting high-pressure shaft. Low-pressure turbine drives booster compressor via an interconnecting low-pressure shaft. Low-pressure turbine also drives external load having a defined speed characteristic that dictates speed of the low-pressure turbine and booster compressor. Booster compressor has one or more rows of variable stator vanes. The method includes: scheduling variation in the angle of variable stator vanes as a function of speed of the booster compressor wherein the vanes open as booster compressor speed increases; measuring or setting one or more operational parameters which are determinative of temperature at entry to core turbine; and biasing scheduling of angle variation of variable stator vanes as a function of operational parameter(s) to reduce variation in temperature at entry to core turbine.

Abstract translation: 具有轴流式系列的增压压缩机，核心压缩机，燃烧设备，核心涡轮机和低压涡轮机的发动机。 核心涡轮机通过互连的高压轴驱动核心压缩机。 低压涡轮机通过互连低压轴驱动增压压缩机。 低压涡轮机还驱动具有限定低速涡轮机和增压压缩机的速度的限定速度特性的外部负载。 增压压缩机具有一排或多排可变定子叶片。 该方法包括：根据增压压缩机的速度调整可变定子叶片的角度变化，其中当增压压缩机转速增加时叶片打开; 测量或设定一个或多个确定进入核心涡轮机时的温度的操作参数; 并且可变定子叶片的角度变化的偏置调度作为操作参数的函数，以减少进入核心涡轮机时的温度变化。