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MCCAFFREY MICHAEL G

Overview
  • Total Patents
    26
  • GoodIP Patent Rank
    228,939
About

MCCAFFREY MICHAEL G has a total of 26 patent applications. Its first patent ever was published in 2007. It filed its patents most often in United States. Its main competitors in its focus markets engines, pumps and turbines, machines and environmental technology are ROLLS ROYCE CORP, BELMONTE OLIVIER and BEECK ALEXANDER R.

Patent filings in countries

World map showing MCCAFFREY MICHAEL Gs patent filings in countries
# Country Total Patents
#1 United States 26

Patent filings per year

Chart showing MCCAFFREY MICHAEL Gs patent filings per year from 1900 to 2020

Top inventors

# Name Total Patents
#1 Mccaffrey Michael G 26
#2 Hudson Eric A 4
#3 Gagnon Ronald R 1
#4 Allen George E 1
#5 Magge Shankar S 1
#6 Hasko Gregory H 1
#7 Hill James D 1
#8 Moore Christopher 1
#9 Almy Thomas 1
#10 Wagner Joel H 1

Latest patents

Publication Filing date Title
US2016084101A1 Gas turbine engine blade outer air seal assembly
US2014186152A1 Blade outer air seal system for controlled tip clearance
US2014023480A1 Radial position control of case supported structure
US2014017072A1 Blade outer air seal with cooling features
US2013323073A1 Assembled blade platform
US2013240304A1 Low conductivity brake pad
US2013209240A1 Adjustable blade outer air seal apparatus
US2013142660A1 Ceramic matrix composite airfoil structure with trailing edge support for a gas turbine engine
US2013115089A1 Rotatable component with controlled load interface
US2013094951A1 Mid turbine frame (MTF) for a gas turbine engine
US2013052030A1 Ceramic matrix composite vane structure with overwrap for a gas turbine engine
US2013022469A1 Turbine rotor non-metallic blade attachment
US2013004326A1 CMC blade with integral 3D woven platform
US2013004325A1 Hybrid part made from monolithic ceramic skin and CMC core
US2013000314A1 Variable cycle turbine engine
US2012275898A1 Blade clearance control using high-CTE and low-CTE ring members
US2012051920A1 Root region of a blade for a gas turbine engine
US2010290898A1 Knife edge seal assembly
US2010226760A1 Turbine engine sealing arrangement
US2009257875A1 Platformless turbine blade