公开(公告)号：US20150033746A1

公开(公告)日：2015-02-05

申请号：US13957735

申请日：2013-08-02

Applicant: SOLAR TURBINES INCORPORATED

Inventor： Daniel William Carey ,  Robert Anthony Corr, II ,  Crosby Hayhurst Johnson ,  Yong Weon Kim

IPC: F02C7/24

CPC classification number: F02C7/24 ,  F23R3/002 ,  F23R3/10 ,  F23R2900/03044

Abstract: A heat shield for a combustion chamber of a gas turbine engine is disclosed. The heat shield includes a plate portion, an inner ring, and a plurality of standoffs. The plate portion includes an annular sector shape. The inner ring extends from an inner part of the plate portion. The inner ring includes a hollow cylinder shape. The plurality of standoffs extends from the plate portion, proximate outer edges of the plate portion and in the same direction as the inner ring. The plurality of standoffs forms a plurality of scallops. Each scallop is located between adjacent standoffs.

Abstract translation: 公开了一种用于燃气涡轮发动机的燃烧室的隔热罩。 隔热罩包括板部，内圈和多个支座。 板部分包括环形扇形。 内环从板部的内部延伸。 内圈包括中空圆筒形状。 多个支座从板部分延伸，邻近板部分的外边缘并且沿与内圈相同的方向延伸。 多个间隔形成多个扇贝。 每个扇贝位于相邻的支架之间。

公开(公告)号：US20160334102A1

公开(公告)日：2016-11-17

申请号：US14711628

申请日：2015-05-13

Applicant: Solar Turbines Incorporated

Inventor： Crosby Hayhurst Johnson ,  Yong Weon Kim ,  Ted Edwin Groocock

IPC: F23R3/00 ,  F23R3/50 ,  F23R3/06

CPC classification number: F23R3/002 ,  F23R3/045 ,  F23R3/06 ,  F23R3/50 ,  F23R2900/00012 ,  F23R2900/00014

Abstract: A grommet for a combustor of a gas turbine engine is disclosed. The grommet includes a lower platform and a raised platform. The lower platform includes a plurality of top slots located in the top surface and a plurality of bottom slots located in the bottom surface. Each top slot and bottom slot may extend radially along the lower platform. The plurality of top slots may be spaced equidistantly from one another along the circumference of the lower platform. The plurality of bottom slots may be spaced equidistantly from one another along the circumference of the lower platform.

Abstract translation: 公开了一种用于燃气涡轮发动机的燃烧器的垫圈。 索环包括一个较低的平台和一个凸起的平台。 下平台包括位于顶表面中的多个顶槽和位于底表面中的多个底槽。 每个顶槽和底槽可以沿下平台径向延伸。 多个顶部槽可以沿着下部平台的圆周彼此间隔开等距离地间隔开。 多个底槽可以沿着下平台的圆周彼此间隔开等间距。

公开(公告)号：US09803863B2

公开(公告)日：2017-10-31

申请号：US14711628

申请日：2015-05-13

Applicant: Solar Turbines Incorporated

Inventor： Crosby Hayhurst Johnson ,  Yong Weon Kim ,  Ted Edwin Groocock

IPC: F02C7/20 ,  F23R3/00 ,  F23R3/06 ,  F23R3/50 ,  F23R3/04

CPC classification number: F23R3/002 ,  F23R3/045 ,  F23R3/06 ,  F23R3/50 ,  F23R2900/00012 ,  F23R2900/00014

Abstract: A grommet for a combustor of a gas turbine engine is disclosed. The grommet includes a lower platform and a raised platform. The lower platform includes a plurality of top slots located in the top surface and a plurality of bottom slots located in the bottom surface. Each top slot and bottom slot may extend radially along the lower platform. The plurality of top slots may be spaced equidistantly from one another along the circumference of the lower platform. The plurality of bottom slots may be spaced equidistantly from one another along the circumference of the lower platform.