公开(公告)号：US20140037448A1

公开(公告)日：2014-02-06

申请号：US13932692

申请日：2013-07-01

Applicant: General Electric Company

Inventor： Xu FU ,  NA NI ,  Qiang LI ,  Zhilin WU ,  Lihan HE ,  Hai QIU ,  Yong YANG ,  Gerald Addison CURTIN, JR. ,  Myungkeun YOON

IPC: F03D7/02

CPC classification number: F03D7/0224 ,  F03D17/00 ,  F03D80/00 ,  F05B2260/84 ,  F05B2260/96 ,  F05B2270/1095 ,  F05B2270/328 ,  F05B2270/331 ,  F05B2270/332 ,  F05B2270/807 ,  Y02E10/722 ,  Y02E10/723

Abstract: A wind turbine includes multiple blades, multiple Micro Inertial Measurement Units (MIMUs) for sensing parameter signals of the blades, and a control system. The control system includes a blade bending moment calculation unit, a blade bending moment error signal calculation unit, and a pitch angle compensation command calculation unit. The blade bending moment calculation unit is used for calculating blade bending moment values of the blades based at least on the sensed parameters. The blade bending moment error signal calculation unit is used for calculating blade bending moment error signals of the blades based on the calculated blade bending moment values of the blades and multiple blade bending moment commands. The pitch angle compensation command calculation unit is used for calculating pitch angle compensation commands of the blades based on the calculated blade bending moment error signals to adjust pitch angles of the blades respectively.

Abstract translation: 风力涡轮机包括多个叶片，用于感测叶片的参数信号的多个微惯性测量单元（MIMU）和控制系统。 控制系统包括叶片弯矩计算单元，叶片弯矩误差信号计算单元和俯仰角补偿指令计算单元。 叶片弯矩计算单元用于至少基于所感测的参数来计算叶片的叶片弯矩值。 刀片弯矩误差信号计算单元用于根据叶片的计算叶片弯矩值和多叶片弯矩命令来计算叶片的叶片弯矩误差信号。 桨距角补偿指令计算单元用于基于所计算的叶片弯矩误差信号来计算叶片的俯仰角补偿命令，以分别调节叶片的桨距角。

公开(公告)号：US20170044681A1

公开(公告)日：2017-02-16

申请号：US15304682

申请日：2015-04-02

Applicant: GENERAL ELECTRIC COMPANY

Inventor： Qiang LI ,  Nicholas Joseph KRAY ,  Michael W. PERETTI ,  Tod Winton DAVIS

IPC: C25D1/02 ,  F04D29/38 ,  F04D29/32

CPC classification number: C25D1/02 ,  C25D1/00 ,  F04D29/325 ,  F04D29/388

Abstract: A method for making a metallic leading edge guard of the type haying a nose with first and second wings extending therefrom is disclosed. The method includes machining from a metallic blank a first half comprising a first portion of the nose and one of the wings, wherein the first portion of the nose includes an interface surface; and electroforming a second half comprising a second portion of the nose and the second wing, wherein the second half is joined to the first half at the interface surface.

Abstract translation: 公开了一种用于制造具有从其延伸的第一和第二翼的鼻子类型的金属前缘防护件的方法。 该方法包括从金属坯料加工包括鼻部的第一部分和翼中的一个的第一半部，其中鼻部的第一部分包括界面; 以及电铸第二半部分，其包括所述鼻部和所述第二机翼的第二部分，其中所述第二半部在所述界面处接合到所述第一半部。

公开(公告)号：US20160010468A1

公开(公告)日：2016-01-14

申请号：US14771970

申请日：2013-03-01

Applicant: GENERAL ELECTRIC COMPANY

Inventor： Nicholas Joseph KRAY ,  Qiang LI ,  Richard W. ALBRECHT, JR.

IPC: F01D5/28 ,  F01D5/14 ,  F01D9/04

CPC classification number: F01D5/28 ,  B23P15/04 ,  F01D5/147 ,  F01D5/282 ,  F01D5/288 ,  F01D9/041 ,  F04D29/324 ,  F05D2220/32 ,  F05D2230/23 ,  F05D2230/60 ,  F05D2240/303 ,  F05D2300/133 ,  F05D2300/171 ,  F05D2300/174 ,  Y02T50/672

Abstract: An airfoil assembly (30) comprises a composite airfoil (40) having a leading edge (32) and a trailing edge (34), a pressure side (36) extending between the leading edge and the trailing edge, a suction side (38) extending between the leading edge and the trailing edge, opposite the leading edge, a metallic leading edge assembly (130) disposed over the composite air-foil, the metallic leading edge assembly including a high density base (50), the metallic leading edge assembly also including a nose (60) disposed over the base, an adhesive bond layer disposed between the composite airfoil and the metallic leading edge assembly.

Abstract translation: 翼型组件（30）包括具有前缘（32）和后缘（34）的复合翼型件（40），在前缘和后缘之间延伸的压力侧（36），吸力侧（38） 在所述前缘和所述后缘之间延伸，与所述前缘相对，设置在所述复合空气箔上方的金属前缘组件，所述金属前缘组件包括高密度基座（50），所述金属前缘组件 还包括设置在所述基座上方的鼻部（60），设置在所述复合翼面和所述金属前缘组件之间的粘合剂粘结层。

公开(公告)号：US20160341052A1

公开(公告)日：2016-11-24

申请号：US14893639

申请日：2014-05-29

Applicant: GENERAL ELECTRIC COMPANY

Inventor： Qiang LI ,  Nicholas Joseph KRAY ,  Scott Roger FINN

IPC: F01D5/30 ,  F04D29/32 ,  F01D5/28

CPC classification number: F01D5/3092 ,  F01D5/282 ,  F01D5/284 ,  F01D5/3007 ,  F01D5/3084 ,  F04D29/324 ,  F05D2220/36 ,  F05D2240/30 ,  F05D2260/941 ,  F05D2300/174 ,  F05D2300/6033 ,  Y02T50/672

Abstract: A composite airfoil comprises a leading edge and a trailing edge, a pressure side and a suction side extending between the leading edge and the trailing edge, a tip at a radial outer end of the airfoil, a shank at a radial inner end of the airfoil, a dovetail connected to the shank, and a metal patch disposed between the dovetail and the shank.

Abstract translation: 复合翼型件包括前缘和后缘，压力侧和在前缘和后缘之间延伸的吸力侧，在翼型件的径向外端处的尖端，在翼型件的径向内端处的柄部 ，连接到柄的燕尾榫和设置在燕尾榫和柄之间的金属补片。

公开(公告)号：US20160333889A1

公开(公告)日：2016-11-17

申请号：US15111199

申请日：2014-11-17

Applicant: GENERAL ELECTRIC COMPANY

Inventor： Nicholas Joseph KRAY ,  Qiang LI

IPC: F04D29/34 ,  F04D29/32 ,  F04D29/02

CPC classification number: F04D29/34 ,  F01D5/282 ,  F01D5/288 ,  F01D5/3007 ,  F01D5/3092 ,  F04D29/023 ,  F04D29/325 ,  Y02T50/672

Abstract: A gas turbine engine blade root shim for use between a composite blade root and a wall of a slot in a rotor includes a longitudinally extending base having distal first and second transversely spaced apart ends, first and second longitudinally extending legs acutely angled inwardly towards the base from the first and second ends, and one or more apertures disposed through each of the longitudinally extending first and second legs. Apertures may include rectangular slots having rounded edges along the first and second outwardly facing surfaces of the first and second legs respectively and/or rounded corners between the first and second outwardly facing surfaces and the first and second inwardly facing surfaces of the first and second legs. Low coefficient of friction coatings may be disposed on outwardly facing surfaces, of the legs. Coatings may include polytetrafluoroethylene powder dispersed in a resin binder and other coatings having polytetrafluoroethylene.

Abstract translation: 用于在复合叶片根部和转子中的槽的壁之间使用的燃气涡轮发动机叶片根垫片包括纵向延伸的基部，其具有远端第一和第二横向间隔开的端部，第一和第二纵向延伸的腿向内朝向基部 从第一端和第二端以及穿过每个纵向延伸的第一和第二腿设置的一个或多个孔。 孔可以包括具有沿着第一和第二腿的第一和第二向外表面的圆形边缘的矩形槽和/或第一和第二向外表面之间的圆角以及第一和第二腿的第一和第二向内的表面 。 低摩擦系数涂层可以设置在腿的向外的表面上。 涂层可以包括分散在树脂粘合剂中的聚四氟乙烯粉末和具有聚四氟乙烯的其它涂层。