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Inventor profile of:

Matthew A. Devore

City:

Cromwell, Connecticut

Country:

United States

Published Applications:

Last publication date:

2020-01-23

Top Assignees for applications by Matthew A. Devore

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

UNITED TECHNOLOGIES CORPORATION 12 Hartford, CT United States
UNITED TECHNOLOGIES CORPORATION 7 Farmington, CT United States
Raytheon Technologies Corporation 2 Farmington, CT United States
United Technologies Corporation 1 East Hartford, CT United States
RAYTHEON TECHNOLOGIES CORPORATION 1 Farmngton, CT United States

Recent patent applications by Devore Matthew A.

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

#1 | 2020-01-23

US20200024963A1

Mechanical engineering

Component core with shaped edges

#2 | 2018-02-08

US20180038236A1

Mechanical engineering

GAS TURBINE ENGINE STATOR VANE BAFFLE ARRANGEMENT

#3 | 2016-11-10

US20160326883A1

Mechanical engineering

Fan cooling hole array

#4 | 2016-09-01

US20160251974A1

Mechanical engineering

Incident tolerant turbine vane cooling

#5 | 2016-05-12

US20160130950A1

Mechanical engineering

Gas turbine engine component with rib support

#6 | 2016-03-17

US20160076382A1

Mechanical engineering

Component core with shaped edges

#7 | 2016-01-14

US20160010463A1

Mechanical engineering

Gas turbine engine high lift airfoil cooling in stagnation zone

#8 | 2016-01-07

US20160003071A1

Mechanical engineering

GAS TURBINE ENGINE STATOR VANE BAFFLE ARRANGEMENT

#9 | 2016-01-07

US20160003053A1

Mechanical engineering

GAS TURBINE ENGINE COMPONENT HAVING TRANSVERSELY ANGLED IMPINGEMENT RIBS

#10 | 2015-11-12

US20150322801A1

Mechanical engineering

Airfoil leading edge film array

#11 | 2014-09-18

US20140271101A1

Mechanical engineering

Modulated turbine vane cooling

#12 | 2014-07-17

US20140199177A1

Mechanical engineering

Airfoil and method of making

#13 | 2014-07-17

US20140196433A1

Mechanical engineering

GAS TURBINE ENGINE COMPONENT PLATFORM COOLING

#14 | 2014-05-06

US13180819

Microcircuit skin core cut back to reduce microcircuit trailing edge stresses

#15 | 2014-04-03

US20140090384A1

Mechanical engineering

Gas turbine engine cooling hole with circular exit geometry

#16 | 2014-01-09

US20140010666A1

Mechanical engineering

Airfoil cooling circuits

#17 | 2013-10-24

US20130280091A1

Performing operations; transporting

Gas turbine engine airfoil impingement cooling

#18 | 2013-10-24

US20130280081A1

Mechanical engineering

GAS TURBINE ENGINE AIRFOIL GEOMETRIES AND CORES FOR MANUFACTURING PROCESS

#19 | 2013-09-12

US20130236329A1

Mechanical engineering

ROTOR BLADE WITH ONE OR MORE SIDE WALL COOLING CIRCUITS

#20 | 2013-08-01

US20130195675A1

Performing operations; transporting

Ceramic core tapered trip strips

#21 | 2013-06-20

US20130156602A1

Mechanical engineering

FILM COOLED TURBINE COMPONENT

#22 | 2011-11-24

US20110286857A1

Performing operations; transporting

Ceramic core tapered trip strips

#23 | 2011-11-10

US20110274559A1

Mechanical engineering

Turbine airfoil with body microcircuits terminating in platform

#24 | 2011-09-29

US20110236178A1

Mechanical engineering

Branched airfoil core cooling arrangement

InventorID:

298302 ⎘