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Inventor profile of:

Matthew A. Devore

City:

Rocky Hill, Connecticut

Country:

United States

Published Applications:

44

Last publication date:

2026-05-21

Top Assignees for applications by Matthew A. Devore

The entities that hold a legal rights for patent applications filed by inventor Devore Matthew A.:

Recent patent applications by Devore Matthew A.

Matthew A. Devore from Rocky Hill, US has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2026-05-21
US20260139593A1
Mechanical engineering

BONDING METHOD FOR REPAIR OF SUPERALLOY ARTICLE

 #2 | 2026-05-07
US20260126249A1
Mechanical engineering

HEAT AUGMENTATION FEATURES IN A CAST HEAT EXCHANGER

 #3 | 2026-04-30
US20260117666A1
Mechanical engineering

HYBRID BONDED CONFIGURATION FOR BLADE OUTER AIR SEAL (BOAS)

 #4 | 2023-10-12
US20230323784A1
Mechanical engineering

Advanced passive clearance control (APCC) control ring produced by field assisted sintering technology (FAST)

 #5 | 2023-05-18
US20230151738A1
Mechanical engineering

HYBRID BONDED CONFIGURATION FOR BLADE OUTER AIR SEAL (BOAS)

 #6 | 2023-05-18
US20230151736A1
Mechanical engineering

BONDING METHOD FOR REPAIR OF SUPERALLOY ARTICLE

 #7 | 2022-12-22
US20220403755A1
Mechanical engineering

Hybrid superalloy article and method of manufacture thereof

 #8 | 2022-12-22
US20220403742A1
Mechanical engineering

HYBRID SUPERALLOY ARTICLE AND METHOD OF MANUFACTURE THEREOF

 #9 | 2020-09-03
US20200277861A1
Mechanical engineering

Trailing edge pressure and flow regulator

 #10 | 2020-06-11
US20200182070A1
Mechanical engineering

Internal cooling cavity with trip strips

 #11 | 2020-06-11
US20200182060A1
Mechanical engineering

Dual cooling airflow to blades

 #12 | 2020-05-07
US20200141271A1
Mechanical engineering

Impingement cooling for a gas turbine engine component

 #13 | 2020-03-12
US20200080424A1
Mechanical engineering

Gas turbine component with platform cooling

 #14 | 2020-01-23
US20200024970A1
Mechanical engineering

Airfoil cooling circuits

 #15 | 2019-10-10
US20190310030A1
Mechanical engineering

HEAT AUGMENTATION FEATURES IN A CAST HEAT EXCHANGER

 #16 | 2019-10-10
US20190309685A1
Mechanical engineering

FLUID INJECTION COOLING

 #17 | 2019-09-26
US20190293367A1
Mechanical engineering

Asymmetric application of cooling features for a cast plate heat exchanger

 #18 | 2018-12-27
US20180371941A1
Mechanical engineering

Gaspath component including minicore plenums

 #19 | 2018-10-18
US20180298774A1
Mechanical engineering

Forward facing tangential onboard injectors for gas turbine engines

 #20 | 2018-10-18
US20180298770A1
Mechanical engineering

FORWARD FACING TANGENTIAL ONBOARD INJECTORS FOR GAS TURBINE ENGINES

 #21 | 2018-10-11
US20180291762A1
Mechanical engineering

Cooled cooling air to blade outer air seal passing through a static vane

 #22 | 2018-10-11
US20180291760A1
Mechanical engineering

COOLING AIR CHAMBER FOR BLADE OUTER AIR SEAL

 #23 | 2018-10-11
US20180291744A1
Mechanical engineering

Dual cooling airflow to blades

 #24 | 2018-07-26
US20180209286A1
Mechanical engineering

Trailing edge pressure and flow regulator

 #25 | 2018-05-24
US20180142971A1
Mechanical engineering

Staged high temperature heat exchanger

 #26 | 2018-05-17
US20180135446A1
Mechanical engineering

Airfoil with ceramic airfoil piece having internal cooling circuit

 #27 | 2018-05-17
US20180135439A1
Mechanical engineering

Airfoil with geometrically segmented coating section

 #28 | 2018-05-17
US20180135437A1
Mechanical engineering

Method for making ceramic turbine engine article

 #29 | 2018-05-10
US20180128115A1
Mechanical engineering

Airfoil cooling circuits

 #30 | 2017-08-10
US20170226893A1
Mechanical engineering

Modulated turbine vane cooling

 #31 | 2017-07-20
US20170204742A1
Mechanical engineering

Axial flowing cooling passages for gas turbine engine components

 #32 | 2017-07-20
US20170204731A1
Mechanical engineering

Flow exchange baffle insert for a gas turbine engine component

 #33 | 2017-06-22
US20170175539A1
Mechanical engineering

Crossover hole configuration for a flowpath component in a gas turbine engine

 #34 | 2017-03-30
US20170089206A1
Mechanical engineering

Turbine airfoil and method of cooling

 #35 | 2017-02-23
US20170051623A1
Mechanical engineering

Cooling channels for gas turbine engine component

 #36 | 2017-01-05
US20170002662A1
Mechanical engineering

GAS TURBINE ENGINE AIRFOIL WITH BI-AXIAL SKIN CORE

 #37 | 2016-12-29
US20160376895A1
Mechanical engineering

Gas turbine engine component platform cooling

 #38 | 2016-07-21
US20160208619A1
Mechanical engineering

Internal cooling cavity with trip strips

 #39 | 2016-06-30
US20160186576A1
Mechanical engineering

Large-footprint turbine cooling hole

 #40 | 2016-04-21
US20160108738A1
Mechanical engineering

Gas turbine component with platform cooling

 #41 | 2016-02-04
US20160032732A1
Mechanical engineering

GAS TURBINE ENGINE AIRFOIL GEOMETRIES AND CORES FOR MANUFACTURING PROCESS

 #42 | 2016-02-04
US20160032416A1
Chemistry; metallurgy

Gas turbine engine airfoil impingement cooling

 #43 | 2016-01-14
US20160010465A1
Mechanical engineering

Gas turbine engine airfoil leading edge cooling

 #44 | 2015-04-09
US20150098835A1
Mechanical engineering

Castings, casting cores, and methods
InventorID:

1123578 ⎘