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MORRISON JAY A

Overview
  • Total Patents
    17
About

MORRISON JAY A has a total of 17 patent applications. Its first patent ever was published in 2005. It filed its patents most often in United States. Its main competitors in its focus markets engines, pumps and turbines, machines and materials and metallurgy are ELIAS LEOPOLD, BST HOLDINGS PTY LTD and HOFFMANN LASZLO.

Patent filings in countries

World map showing MORRISON JAY As patent filings in countries
# Country Total Patents
#1 United States 17

Patent filings per year

Chart showing MORRISON JAY As patent filings per year from 1900 to 2020

Top inventors

# Name Total Patents
#1 Morrison Jay A 17
#2 Merrill Gary B 8
#3 Lane Jay E 4
#4 James Allister W 2
#5 Keller Douglas A 1
#6 Appleby Mike P 1
#7 Paulus John R 1
#8 Crawford Michael E 1
#9 Schiavo Anthony L 1
#10 Stewart John V 1

Latest patents

Publication Filing date Title
US2015033697A1 Regeneratively cooled transition duct with transversely buffered impingement nozzles
US2013239585A1 Tangential flow duct with full annular exit component
US2012237786A1 Process for making a wall with a porous element for component cooling
US2011265406A1 Gusset with fibers oriented to strengthen a CMC wall intersection anisotropically
US2011016717A1 Method of Making a Combustion Turbine Component Having a Plurality of Surface Cooling Features and Associated Components
US2010322774A1 Airfoil Having an Improved Trailing Edge
US2010322760A1 Interlocked CMC airfoil
US2010291348A1 Methodology and tooling arrangements for increasing interlaminar shear strength in a ceramic matrix composite structure
US2010279072A1 Gussets for strengthening CMC fillet radii
US2010054930A1 Turbine vane with high temperature capable skins
US2010047061A1 Grid ceramic matrix composite structure for gas turbine shroud ring segment
US2010047512A1 Methodology and tooling arrangements for strengthening a surface bond in a hybrid ceramic matrix composite structure
US2008280101A1 Patterned reduction of surface area for abradability
US2010251721A1 Stacked laminate gas turbine component
US2012125585A1 CMC wall structure with integral cooling channels
US2005254942A1 Method of joining ceramic parts and articles so formed