Inventor profile of:

BROOKS E. SNYDER

City:

Glastonbury, Connecticut

Country:

United States

Published Applications:

24

Last publication date:

2019-10-17

Top Assignees for applications by BROOKS E. SNYDER

The entities that hold a legal rights for patent applications filed by inventor SNYDER BROOKS E.:

Recent patent applications by SNYDER BROOKS E.

BROOKS E. SNYDER from Glastonbury, US has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2019-10-17
US20190316474A1
Mechanical engineering

Cupped contour for gas turbine engine blade assembly

#2 | 2019-03-21
US20190085719A1
Mechanical engineering

ANTI-DEFLECTION FEATURE FOR ADDITIVELY MANUFACTURED THIN METAL PARTS AND METHOD OF ADDITIVELY MANUFACTURING THIN METAL PARTS

#3 | 2017-02-23
US20170051625A1
Mechanical engineering

BLADE OUTER AIR SEAL COMPONENT WITH VARYING THERMAL EXPANSION COEFFICIENT

#4 | 2017-02-23
US20170051613A1
Mechanical engineering

Cupped contour for gas turbine engine blade assembly

#5 | 2016-12-22
US20160369634A1
Mechanical engineering

Airfoil, and method for manufacturing the same

#6 | 2016-11-17
US20160333702A1
Mechanical engineering

Gas turbine engine component cooling circuit with respirating pedestal

#7 | 2016-10-27
US20160313005A1
Mechanical engineering

ADDITIVE MANUFACTURED COMBUSTOR HEAT SHIELD WITH COOLED ATTACHMENT STUD

#8 | 2016-10-27
US20160313004A1
Mechanical engineering

Additive manufactured combustor heat shield

#9 | 2016-10-27
US20160312624A1
Mechanical engineering

Gas turbine engine component cooling cavity with vortex promoting features

#10 | 2016-10-06
US20160290139A1
Mechanical engineering

Gas turbine engine component cooling passage turbulator

#11 | 2016-09-22
US20160273365A1
Mechanical engineering

Gas turbine engine airfoil with leading edge trench and impingement cooling

#12 | 2016-09-15
US20160265366A1
Mechanical engineering

Gas turbine engine turbine blade tip cooling

#13 | 2016-08-18
US20160237848A1
Mechanical engineering

Anti-deflection feature for additively manufactured thin metal parts and method of additively manufacturing thin metal parts

#14 | 2016-08-04
US20160222793A1
Mechanical engineering

COOLING CONFIGURATION FOR ENGINE COMPONENT

#15 | 2016-07-28
US20160215644A1
Mechanical engineering

Seal for gas turbine engine

#16 | 2016-07-21
US20160208705A1
Mechanical engineering

Bore-cooled film dispensing pedestals

#17 | 2016-06-23
US20160177740A1
Mechanical engineering

Gas turbine engine component with conformal fillet cooling path

#18 | 2016-06-23
US20160177736A1
Mechanical engineering

Cooled airfoil structure

#19 | 2016-06-02
US20160153291A1
Mechanical engineering

Cooling system of a stator assembly for a gas turbine engine having a variable cooling flow mechanism and method of operation

#20 | 2016-01-28
US20160024938A1
Mechanical engineering

Airfoil cooling apparatus

#21 | 2015-11-26
US20150337667A1
Mechanical engineering

Airfoil cooling device and method of manufacture

#22 | 2015-11-12
US20150322860A1
Mechanical engineering

Variable vane segment

#23 | 2015-11-12
US20150322563A1
Chemistry; metallurgy

Fixture for application of coatings and method of using same

#24 | 2015-10-29
US20150307990A1
Chemistry; metallurgy

Method and system for controlling coating in non-line-of-sight locations

InventorID:

1338677 ⎘