Inventor
MARRA JOHN J
US37 patents
⚠️ This page may combine multiple inventors who share the name “MARRA JOHN J”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
LEE CHING-PANG
9 patentsUS8920111B2Dec 30, 2014
Airfoil incorporating tapered cooling structures defining cooling passageways
LEE CHING-PANG7 citations84
US8714926B2May 6, 2014
Turbine component cooling channel mesh with intersection chambers
LEE CHING-PANG13 citations84
US8668453B2Mar 11, 2014
Cooling system having reduced mass pin fins for components in a gas turbine engine
LEE CHING-PANG13 citations84
US9022736B2May 5, 2015
Integrated axial and tangential serpentine cooling circuit in a turbine airfoil
LEE CHING-PANG10 citations83
US8894367B2Nov 25, 2014
Compound cooling flow turbulator for turbine component
LEE CHING-PANG15 citations83
US8764394B2Jul 1, 2014
Component cooling channel
LEE CHING-PANG10 citations83
US8926267B2Jan 6, 2015
Ambient air cooling arrangement having a pre-swirler for gas turbine engine blade cooling
LEE CHING-PANG9 citations82
US8894363B2Nov 25, 2014
Cooling module design and method for cooling components of a gas turbine system
LEE CHING-PANG7 citations82
US9017014B2Apr 28, 2015
Aft outer rim seal arrangement
LEE CHING-PANG5 citations71
MARRA JOHN J
8 patentsUS9726028B2Aug 8, 2017
Ductile alloys for sealing modular component interfaces
MARRA JOHN J20 citations91
US8540488B2Sep 24, 2013
Turbine blade damping device with controlled loading
MARRA JOHN J7 citations84
US8523525B2Sep 3, 2013
Snubber assembly for turbine blades
MARRA JOHN J8 citations84
US8485787B2Jul 16, 2013
Turbine airfoil fabricated from tapered extrusions
MARRA JOHN J12 citations84
US8292583B2Oct 23, 2012
Turbine blade having a constant thickness airfoil skin
MARRA JOHN J14 citations84
US8500411B2Aug 6, 2013
Turbine airfoil with outer wall thickness indicators
MARRA JOHN J6 citations73
US8684666B2Apr 1, 2014
Low pressure cooling seal system for a gas turbine engine
MARRA JOHN J0 citations41
US8646511B2Feb 11, 2014
Component with inspection-facilitating features
MARRA JOHN J0 citations41
UNITED TECHNOLOGIES CORP
5 patentsUS4784012ANov 15, 1988
Rotor balance system
UNITED TECHNOLOGIES CORP54 citations96
US4835827AJun 6, 1989
Method of balancing a rotor
UNITED TECHNOLOGIES CORP52 citations92
US6625507B1Sep 23, 2003
Method and system for designing a low pressure turbine shaft
UNITED TECHNOLOGIES CORP26 citations90
US6587741B1Jul 1, 2003
Method and system for designing a spline coupling
UNITED TECHNOLOGIES CORP45 citations90
US5141393AAug 25, 1992
Seal accommodating thermal expansion between adjacent casings in gas turbine engine
UNITED TECHNOLOGIES CORP19 citations74
CAMPBELL CHRISTIAN X
3 patentsUS8579593B2Nov 12, 2013
Damping element for reducing the vibration of an airfoil
CAMPBELL CHRISTIAN X9 citations84
US8714920B2May 6, 2014
Turbine airfoil to shround attachment
CAMPBELL CHRISTIAN X8 citations83
US8939727B2Jan 27, 2015
Turbine blade and non-integral platform with pin attachment
CAMPBELL CHRISTIAN X5 citations72