公开(公告)号：US20210264072A1

公开(公告)日：2021-08-26

申请号：US16797323

申请日：2020-02-21

Applicant: United Technologies Corporation

Inventor： Peter Cocks ,  Wookyung Kim

IPC: G06F30/17 ,  G06N3/08

Abstract: A process for designing an internal turbine engine component including operating a test rig incorporating a physical morphing component having a first geometry and generating a data set of empirically determined component performance parameters corresponding to the first geometry. Providing the data set of empirically determined component performance parameters to a computational optimization system and automatically. Determining a geometry optimization of the morphing component. Altering the geometry of the morphing component to match the geometry optimization. Reiterating operating the test rig and providing the data set of empirically determined component performance parameters.

公开(公告)号：US10060629B2

公开(公告)日：2018-08-28

申请号：US14627709

申请日：2015-02-20

Applicant: United Technologies Corporation

Inventor： Wookyung Kim ,  Zhongtao Dai ,  Kristin Kopp-Vaughan

IPC: F23R3/34 ,  F23R3/28 ,  F23R3/50

CPC classification number: F23R3/286 ,  F23R3/28 ,  F23R3/283 ,  F23R3/34 ,  F23R3/346 ,  F23R3/50

Abstract: A combustor is provided. The combustor may comprise an axial fuel delivery system, and a radial fuel delivery system aft of the axial fuel delivery system. The radial fuel delivery system may be configured to direct fuel at least partially towards the axial fuel delivery system. A radial fuel delivery system is also provided. The system may comprise a combustor including a combustor liner, a mixer coupled to the combustor liner, and a nozzle disposed within the mixer, wherein the mixer and the nozzle are configured to direct fuel in a direction at least partially forward.

公开(公告)号：US11379629B2

公开(公告)日：2022-07-05

申请号：US16797323

申请日：2020-02-21

Applicant: United Technologies Corporation

Inventor： Peter Cocks ,  Wookyung Kim

IPC: G06F30/00 ,  G06F30/17 ,  G06N3/08 ,  G06F30/20 ,  G06F111/20

Abstract: A process for designing an internal turbine engine component including operating a test rig incorporating a physical morphing component having a first geometry and generating a data set of empirically determined component performance parameters corresponding to the first geometry. Providing the data set of empirically determined component performance parameters to a computational optimization system and automatically. Determining a geometry optimization of the morphing component. Altering the geometry of the morphing component to match the geometry optimization. Reiterating operating the test rig and providing the data set of empirically determined component performance parameters.

公开(公告)号：US20160245523A1

公开(公告)日：2016-08-25

申请号：US14627709

申请日：2015-02-20

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Wookyung Kim ,  Zhongtao Dai ,  Kristin Kopp-Vaughan

IPC: F23R3/28

CPC classification number: F23R3/286 ,  F23R3/28 ,  F23R3/283 ,  F23R3/34 ,  F23R3/346 ,  F23R3/50

Abstract: A combustor is provided. The combustor may comprise an axial fuel delivery system, and a radial fuel delivery system aft of the axial fuel delivery system. The radial fuel delivery system may be configured to direct fuel at least partially towards the axial fuel delivery system. A radial fuel delivery system is also provided. The system may comprise a combustor including a combustor liner, a mixer coupled to the combustor liner, and a nozzle disposed within the mixer, wherein the mixer and the nozzle are configured to direct fuel in a direction at least partially forward.

Abstract translation: 提供燃烧器。 燃烧器可以包括轴向燃料输送系统和轴向燃料输送系统后部的径向燃料输送系统。 径向燃料输送系统可以构造成将燃料至少部分地引向轴向燃料输送系统。 还提供径向燃料输送系统。 该系统可以包括燃烧器，该燃烧器包括燃烧器衬套，联接到燃烧器衬套的混合器和设置在混合器内的喷嘴，其中混合器和喷嘴构造成沿至少部分向前的方向引导燃料。