Inventor profile of:

Ricardo Trindade

City:

Coventry, Connecticut

Country:

United States

Published Applications:

16

Last publication date:

2016-05-12

Top Assignees for applications by Ricardo Trindade

The entities that hold a legal rights for patent applications filed by inventor Trindade Ricardo:

Recent patent applications by Trindade Ricardo

Ricardo Trindade from Coventry, US has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2016-05-12
US20160131037A1
Mechanical engineering

Supply duct for cooling air from gas turbine compressor

#2 | 2014-10-30
US20140321961A1
Mechanical engineering

Mate face cooling holes for gas turbine engine component

#3 | 2014-02-20
US20140047844A1
Mechanical engineering

Gas turbine engine component having platform trench

#4 | 2014-02-06
US20140037459A1
Mechanical engineering

Airfoil design having localized suction side curvatures

#5 | 2014-01-02
US20140000282A1
Mechanical engineering

Turbine blade platform with U-channel cooling holes

#6 | 2013-05-02
US20130108416A1
Mechanical engineering

Gas turbine engine component having wavy cooling channels with pedestals

#7 | 2010-05-20
US20100122789A1
Performing operations; transporting

Investment casting cores and methods

#8 | 2009-07-16
US20090180861A1
Mechanical engineering

Cooling arrangement for turbine components

#9 | 2008-11-13
US20080279695A1
Mechanical engineering

Enhanced turbine airfoil cooling

#10 | 2008-03-06
US20080056896A1
Mechanical engineering

HP turbine vane airfoil profile

#11 | 2008-01-10
US20080005903A1
Mechanical engineering

External datum system and film hole positioning using core locating holes

#12 | 2006-06-15
US20060123794A1
Mechanical engineering

Shroud leading edge cooling

#13 | 2006-06-08
US20060120870A1
Mechanical engineering

Internally cooled airfoil for a gas turbine engine and method

#14 | 2006-05-11
US20060099073A1
Mechanical engineering

Aspherical dimples for heat transfer surfaces and method

#15 | 2006-02-23
US20060039786A1
Mechanical engineering

Airfoil cooling passage trailing edge flow restriction

#16 | 2005-12-22
US20050281663A1
Mechanical engineering

Double impingement vane platform cooling

InventorID:

221486 ⎘