公开(公告)号：US09667112B2

公开(公告)日：2017-05-30

申请号：US14471306

申请日：2014-08-28

Applicant: General Electric Company

Inventor： Wei Zhang ,  Xiaochuan Jia ,  Charles T. Sigler ,  Xiaomei Fang ,  Hao Huang ,  David Dimitri Karipides

IPC: H02K3/34 ,  H02K15/10 ,  H02K3/30

CPC classification number: H02K3/345 ,  H02K3/30 ,  H02K15/10

Abstract: A slot liner for a rotor assembly in one embodiment includes a metallic support member and a coating. The coating is disposed on at least one side of the metallic support member, and includes a mixture of a filler and a polyimide resin. The filler is a high thermal conductivity electrical insulating (HTCEI) filler, and includes particles of at least one of boron nitride, aluminum nitride, or a diamond material.

公开(公告)号：US20160065024A1

公开(公告)日：2016-03-03

申请号：US14471306

申请日：2014-08-28

Applicant: General Electric Company

Inventor： Wei Zhang ,  Xiaochuan Jia ,  Charles T. Sigler ,  Xiaomei Fang ,  Hao Huang ,  David Dimitri Karipides

IPC: H02K3/34 ,  H02K15/10

CPC classification number: H02K3/345 ,  H02K3/30 ,  H02K15/10

Abstract: A slot liner for a rotor assembly in one embodiment includes a metallic support member and a coating. The coating is disposed on at least one side of the metallic support member, and includes a mixture of a filler and a polyimide resin. The filler is a high thermal conductivity electrical insulating (HTCEI) filler, and includes particles of at least one of boron nitride, aluminum nitride, or a diamond material.

Abstract translation: 在一个实施例中，用于转子组件的槽衬套包括金属支撑构件和涂层。 涂层设置在金属支撑构件的至少一侧，并且包括填料和聚酰亚胺树脂的混合物。 填料是高导热电绝缘（HTCEI）填料，并且包括氮化硼，氮化铝或金刚石材料中的至少一种的颗粒。

公开(公告)号：US20210316878A1

公开(公告)日：2021-10-14

申请号：US16843243

申请日：2020-04-08

Applicant: General Electric Company

Inventor： Hao Huang ,  David Dimitri Karipides ,  Jia Xiaochuan

IPC: B64D41/00 ,  H02K7/18 ,  H02K7/20 ,  H02K11/04 ,  H02K11/27 ,  B64D27/10 ,  F02C7/32

Abstract: An electric generator assembly for an aircraft is provided. The electric generator assembly includes: a main generator having a main rotor and a main stator, the main stator comprising a first three-phase winding and a second three-phase winding, the first and second three-phase windings each configured to have a voltage induced therein by the main rotor, the first three-phase winding defining a phase shift from the second three-phase winding greater than zero degrees

公开(公告)号：US11884416B2

公开(公告)日：2024-01-30

申请号：US18161335

申请日：2023-01-30

Applicant: General Electric Company

Inventor： Hao Huang ,  David Dimitri Karipides ,  Jia Xiaochuan

IPC: H02K3/00 ,  B64D41/00 ,  H02K11/27 ,  F02C7/32 ,  H02K7/18 ,  H02K7/20 ,  H02K11/049

CPC classification number: B64D41/00 ,  F02C7/32 ,  H02K3/00 ,  H02K7/1823 ,  H02K7/20 ,  H02K11/049 ,  H02K11/27 ,  B64D2221/00 ,  F05D2220/762

Abstract: An electric generator assembly for an aircraft is provided. The electric generator assembly includes: a main generator having a main rotor and a main stator, the main stator includes a first three-phase winding and a second three-phase winding, the first and second three-phase windings each configured to have a voltage induced therein by the main rotor, the first three-phase winding defining a phase shift from the second three-phase winding greater than zero degrees.

公开(公告)号：US20230166859A1

公开(公告)日：2023-06-01

申请号：US18161335

申请日：2023-01-30

Applicant: General Electric Company

Inventor： Hao Huang ,  David Dimitri Karipides ,  Jia Xiaochuan

IPC: B64D41/00 ,  H02K11/27 ,  F02C7/32 ,  H02K3/00 ,  H02K7/18 ,  H02K7/20 ,  H02K11/049

CPC classification number: B64D41/00 ,  H02K11/27 ,  F02C7/32 ,  H02K3/00 ,  H02K7/1823 ,  H02K7/20 ,  H02K11/049 ,  B64D2221/00 ,  F05D2220/762

Abstract: An electric generator assembly for an aircraft is provided. The electric generator assembly includes: a main generator having a main rotor and a main stator, the main stator includes a first three-phase winding and a second three-phase winding, the first and second three-phase windings each configured to have a voltage induced therein by the main rotor, the first three-phase winding defining a phase shift from the second three-phase winding greater than zero degrees.

公开(公告)号：US11565824B2

公开(公告)日：2023-01-31

申请号：US16843243

申请日：2020-04-08

Applicant: General Electric Company

Inventor： Hao Huang ,  David Dimitri Karipides ,  Jia Xiaochuan

IPC: H02K3/00 ,  B64D41/00 ,  H02K11/27 ,  F02C7/32 ,  H02K7/18 ,  H02K7/20 ,  H02K11/04

Abstract: An electric generator assembly for an aircraft is provided. The electric generator assembly includes: a main generator having a main rotor and a main stator, the main stator includes a first three-phase winding and a second three-phase winding, the first and second three-phase windings each configured to have a voltage induced therein by the main rotor, the first three-phase winding defining a phase shift from the second three-phase winding greater than zero degrees.