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CAMPBELL CHRISTIAN X

Overview
  • Total Patents
    17
About

CAMPBELL CHRISTIAN X has a total of 17 patent applications. Its first patent ever was published in 2008. It filed its patents most often in United States. Its main competitors in its focus markets engines, pumps and turbines, materials and metallurgy and machines are DUROCHER ERIC, FARINEAU THOMAS JOSEPH and FRANCO TOSI MECCANICA S P A.

Patent filings in countries

World map showing CAMPBELL CHRISTIAN Xs patent filings in countries
# Country Total Patents
#1 United States 17

Patent filings per year

Chart showing CAMPBELL CHRISTIAN Xs patent filings per year from 1900 to 2020

Top inventors

# Name Total Patents
#1 Campbell Christian X 17
#2 Morrison Jay A 5
#3 Marra John J 3
#4 James Allister W 3
#5 Eng Darryl 3
#6 Wessell Brian J 2
#7 Lee Ching-Pang 2
#8 Schiavo Anthony L 1
#9 Merrill Gary B 1
#10 Davies Daniel O 1

Latest patents

Publication Filing date Title
US8814507B1 Cooling system for three hook ring segment
US2013149169A1 Component having cooling channel with hourglass cross section
US8720526B1 Process for forming a long gas turbine engine blade having a main wall with a thin portion near a tip
US2013294913A1 Turbine blade with tuned damping structure
US2013064667A1 Turbine blade and non-integral platform with pin attachment
US2011297344A1 Turbine airfoil to shroud attachment method
US2012237358A1 Turbine blade tip
US2011142639A1 Modular turbine airfoil and platform assembly with independent root teeth
US2011243724A1 Turbine airfoil to shround attachment
US2011236221A1 Four-wall turbine airfoil with thermal strain control for reduced cycle fatigue
US2011142684A1 Turbine engine airfoil and platform assembly
US2011110762A1 Damping element for reducing the vibration of an airfoil
US2010183435A1 Gas turbine vane platform element
US2010284822A1 Turbine airfoil with a compliant outer wall
US2010284798A1 Turbine airfoil with dual wall formed from inner and outer layers separated by a compliant structure
US2010056006A1 Multilayered ceramic matrix composite structure having increased structural strength
US2011008154A1 Sealing arrangement for turbine engine having ceramic components