Inventor profile of:

Brian David Keith

City:

Cincinnati, Ohio

Country:

United States

Published Applications:

24

Last publication date:

2025-06-12

Top Assignees for applications by Brian David Keith

The entities that hold a legal rights for patent applications filed by inventor Keith Brian David:

Recent patent applications by Keith Brian David

Brian David Keith from Cincinnati, US has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2025-06-12
US20250188843A1
Mechanical engineering

TURBINE ENGINE AIRFOIL

#2 | 2024-05-23
US20240167385A1
Mechanical engineering

Turbine engine airfoil

#3 | 2024-03-26
US17980134
Mechanical engineering

Airfoil assembly with flow surface

#4 | 2024-02-29
US20240068370A1
Mechanical engineering

Turbine engine airfoil

#5 | 2023-01-19
US20230014436A1
Mechanical engineering

Variable guide vane sealing

#6 | 2021-02-11
US20210040861A1
Mechanical engineering

VARIABLE GUIDE VANE SEALING

#7 | 2019-05-02
US20190128131A1
Mechanical engineering

Variable guide vane sealing

#8 | 2018-12-13
US20180355738A1
Mechanical engineering

Turbine engine with variable effective throat

#9 | 2017-10-19
US20170298747A1
Mechanical engineering

Gas turbine engine transition duct and turbine center frame

#10 | 2017-08-10
US20170226868A1
Mechanical engineering

Gas turbine engine airfoil

#11 | 2014-03-27
US20140086739A1
Mechanical engineering

Transition duct for use in a turbine engine and method of assembly

#12 | 2013-09-26
US20130251520A1
Mechanical engineering

Scalloped surface turbine stage

#13 | 2013-08-29
US20130224027A1
Mechanical engineering

Scalloped surface turbine stage with purge trough

#14 | 2010-09-02
US20100221122A1
Mechanical engineering

Flared tip turbine blade

#15 | 2010-06-24
US20100158696A1
Mechanical engineering

Curved platform turbine blade

#16 | 2009-12-31
US20090324422A1
Mechanical engineering

Cascade tip baffle airfoil

#17 | 2008-05-22
US20080118363A1
Mechanical engineering

Triforial tip cavity airfoil

#18 | 2008-05-01
US20080101959A1
Mechanical engineering

Rotor blade profile optimization

#19 | 2008-02-21
US20080044291A1
Mechanical engineering

Counter tip baffle airfoil

#20 | 2008-02-21
US20080044290A1
Mechanical engineering

Conformal tip baffle airfoil

#21 | 2008-02-21
US20080044289A1
Mechanical engineering

Tip ramp turbine blade

#22 | 2006-03-07
US10375415
-

Gas turbine engine turbine nozzle bifurcated impingement baffle

#23 | 2005-11-29
US10375585
-

Gas turbine engine turbine nozzle segment with a single hollow vane having a bifurcated cavity

#24 | 2005-08-23
US10375441
-

Turbine nozzle segment cantilevered mount

InventorID:

413341 ⎘