Eva Y Wong, 496556 Dibble Ave NW, Seattle, WA 98117

2020034, Nov 5, 2020

May 3, 2019

16/402707

- Farmington CT, US
Eva Wong - Glastonbury CT, US
San Quach - Southington CT, US
Jeremy Styborski - East Hartford CT, US
Caroline Karanian - West Hartford CT, US
Lauryn M. Curtis - Manchester CT, US
Steven D. Porter - Wethersfield CT, US
Zhongtao Dai - West Hartford CT, US

F23R 3/00
F23R 3/04
F02C 7/18

A gas turbine engine component assembly including: a first component having a first surface and a second surface opposite the first surface; a second component having a first surface and a second surface opposite the first surface of the second component; and a cooling circuit formed in the second component, the cooling circuit including an inlet at the second surface of the second component, an outlet at the first surface of the second component, an inward surface, and an outward surface, the inward surface and the outward surface being in a facing spaced relationship extending from the inlet to the outlet defining an airflow passageway therebetween, wherein the airflow passageway includes a parallel portion that is oriented about parallel to at least one of the first surface of the second component and the second surface of the second component.

2018007, Mar 15, 2018

Sep 12, 2016

15/262888

- Windsor Locks CT, US
Eva Wong - Glastonbury CT, US

F28D 9/00
B23P 15/26
F28F 3/08
F28F 21/04

A heat exchanger assembly embodiment includes a plurality of laminated ceramic tape layers having at least one hole surrounded by at least one tape remainder portion. The plurality of layers is arranged in a build direction defined parallel to a counter-flow plane. Each laminated ceramic tape layer is stacked and sintered to define a ceramic core section integrally formed with a first ceramic manifold and a second ceramic manifold. The ceramic core section of the assembly includes a plurality of spaced apart counter-flow plates stacked along a stacking direction normal to the counter-flow plane and the build direction, defining a plurality of flow passages parallel to the counter-flow plane. Each flow passage is in communication with the first manifold and the second manifold. A plurality of counter-flow fins is disposed in at least one of the plurality of flow passages, between adjacent ones of the plurality of counter-flow plates.

2017019, Jul 13, 2017

Jan 13, 2016

14/994775

- Charlotte NC, US
Eva Wong - Glastonbury CT, US
Brian St. Rock - Andover CT, US
Joseph Turney - Amston CT, US

F28D 7/00
B23P 15/26

A heat exchanger includes a body, a plurality of first flow channels defined in the body, and a plurality of second flow channels defined in the body, the second flow channels fluidly isolated from the first flow channels, wherein at least one of the first flow channels or the second flow channels have a changing characteristic along a direction of flow within the first flow channels or the second flow channels.

2017014, May 25, 2017

Nov 24, 2015

14/950143

- Windsor Locks CT, US
Eva Wong - Glastonbury CT, US
Brian St. Rock - Andover CT, US

F28F 9/02
B23P 15/26

A header for a heat exchanger having a first phase with a first pipe connector defining a first flow path and a second pipe connector defining a second flow path fluidly isolated from the first flow path. A second phase in which the first and second flow paths are merged while maintaining fluid isolation of the two flow paths wherein in the second phase the first flow path comprises at least one first layer and the second flow path comprises at least one second layer. A third phase in which the at least one first layer and the at least one second layer are substantially overlapping and wherein the third phase is configured to fluidly connect the first flow path to a first section of a core of a heat exchanger and the second flow path to a second section of the core different from the first section.