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ALVANOS IOANNIS

Overview
  • Total Patents
    21
About

ALVANOS IOANNIS has a total of 21 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, environmental technology and machines are FARINEAU THOMAS JOSEPH, HK TURBINE CO LTD and HOLZWARTH HANS DR ING E H.

Patent filings in countries

World map showing ALVANOS IOANNISs patent filings in countries
# Country Total Patents
#1 United States 21

Patent filings per year

Chart showing ALVANOS IOANNISs patent filings per year from 1900 to 2020

Top inventors

# Name Total Patents
#1 Alvanos Ioannis 21
#2 Suciu Gabriel L 13
#3 Dye Christopher M 5
#4 Agrawal Rajendra K 3
#5 Levasseur Glenn 3
#6 Merry Brian D 2
#7 Pinero Hector M 2
#8 Levasseur Glenn N 1
#9 Rugg Kevin L 1
#10 Riehl John D 1

Latest patents

Publication Filing date Title
US2013119617A1 Turbomachinery seal
US2013000324A1 Integrated case and stator
US2012321453A1 Non-mechanically fastened TOBI heat shield
US2012301303A1 Hybrid Ceramic Matrix Composite vane structures for a gas turbine engine
US2012301314A1 Hybrid rotor disk assembly with a ceramic matrix composite airfoil for a gas turbine engine
US2012301305A1 Integrated ceramic matrix composite rotor disk hub geometry for a gas turbine engine
US2012301317A1 Hybrid rotor disk assembly with ceramic matrix composites platform for a gas turbine engine
US2012297790A1 Integrated ceramic matrix composite rotor disk geometry for a gas turbine engine
US2012301315A1 Ceramic matrix composite airfoil for a gas turbine engine
US2012301306A1 Hybrid rotor disk assembly for a gas turbine engine
US2012301269A1 Clearance control with ceramic matrix composite rotor assembly for a gas turbine engine
US2011206522A1 Rotating airfoil fabrication utilizing cmc
US2009257877A1 Asymmetrical rotor blade fir-tree attachment
US2009180864A1 Gas turbine engine case
US2009148271A1 Bearing mounting system in a low pressure turbine
US2008260522A1 Gas turbine engine with integrated abradable seal and mount plate
US2008260523A1 Gas turbine engine with integrated abradable seal
US2008095616A1 Fluid brush seal with segment seal land
US2007059158A1 Turbine cooling air sealing
US2006275106A1 Blade neck fluid seal