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PROPHETER-HINCKLEY TRACY A

Overview
  • Total Patents
    28
  • GoodIP Patent Rank
    227,121
About

PROPHETER-HINCKLEY TRACY A has a total of 28 patent applications. Its first patent ever was published in 2006. It filed its patents most often in United States. Its main competitors in its focus markets engines, pumps and turbines, materials and metallurgy and environmental technology are LEE CHING-PANG, AHMAD FATHI and SPANGLER BRANDON W.

Patent filings in countries

World map showing PROPHETER-HINCKLEY TRACY As patent filings in countries
# Country Total Patents
#1 United States 28

Patent filings per year

Chart showing PROPHETER-HINCKLEY TRACY As patent filings per year from 1900 to 2020

Top inventors

# Name Total Patents
#1 Propheter-Hinckley Tracy A 28
#2 Fisk Benjamin T 5
#3 Devore Matthew A 5
#4 Tracy Anita L 4
#5 Piggush Justin D 3
#6 Cherolis Anthony P 3
#7 Xue Yongxiang D 3
#8 Letizia Eric P 3
#9 Ramlogan Amarnath 3
#10 Shi Jun 2

Latest patents

Publication Filing date Title
US2014072447A1 Ceramic and refractory metal core assembly
US2013343878A1 Turbine engine variable area vane with feather seal
US2013280074A1 Airfoil support method and apparatus
US2013276456A1 Airfoil including member connected by articulated joint
US2013280081A1 Gas turbine engine airfoil geometries and cores for manufacturing process
US2013276461A1 Airfoil having internal lattice network
US2013276460A1 Airfoil having minimum distance ribs
US2013280091A1 Gas turbine engine airfoil impingement cooling
US2013280082A1 Airfoil with powder damper
US2013243591A1 Gas turbine engine airfoil cooling circuit
US2013216361A1 Vane assembly for a gas turbine engine
US2013156601A1 Gas turbine engine airfoil cooling circuit
US2013034435A1 Vane assembly for a gas turbine engine
US2013034434A1 Vane assembly for a gas turbine engine
US2012189424A1 Mateface cooling feather seal assembly
US2015027657A1 Method and casting core for forming a landing for welding a baffle inserted in an airfoil
US2012163992A1 Drill to flow mini core
US2012163975A1 Platform with cooling circuit
US2010232946A1 Divoted airfoil baffle having aimed cooling holes
US2010189556A1 Segmented ceramic matrix composite turbine airfoil component