Learn more

LUCAS AEROSPACE LTD

Overview
  • Total Patents
    355
About

LUCAS AEROSPACE LTD has a total of 355 patent applications. Its first patent ever was published in 1968. It filed its patents most often in Germany, Italy and United States. Its main competitors in its focus markets engines, pumps and turbines, machines and mechanical elements are JANSEN S AIRCRAFT SYSTEMS CONT, GARRETT CORP and WILLIAMS INT CORP.

Patent filings in countries

World map showing LUCAS AEROSPACE LTDs patent filings in countries

Patent filings per year

Chart showing LUCAS AEROSPACE LTDs patent filings per year from 1900 to 2020

Top inventors

# Name Total Patents
#1 Lewis Geoffrey Arthur 19
#2 Smith Trevor Stanley 16
#3 Bloom Joseph Louis 12
#4 Bottoms Harry Simister 8
#5 Glaze Stanley George 7
#6 Craven Donald 6
#7 Lloyd Arthur Leslie 6
#8 Capewell Terence John 5
#9 Thomas Alan 4
#10 Heath Ronald Alfred 4

Latest patents

Publication Filing date Title
US4154425A Throttle valve for use in a gas turbine engine fuel control system
US3981646A Gear pumps and motors
US4069767A Pneumatically controlled hydromechanical railway car stabilizing apparatus
US3955164A Electromagnetic force applying device
US3919923A Fluid flow control valve
DE2445293A1 FUEL CONTROL SYSTEM FOR GAS TURBINE ENGINE
DE2444594A1 DEVICE FOR TRANSMISSION OF ROTATING MOTION THROUGH A SEALING MEMBRANE
DE2442452A1 FUEL CONTROL SYSTEM FOR GAS TURBINE
US3995883A Land vehicle wheel suspension arrangements
DE2434051A1 FUEL CONTROL SYSTEM FOR GAS TURBINE
DE2434029A1 FUEL CONTROL SYSTEM FOR GAS TURBINE
DE2417130A1 FUEL SPRAYING DEVICE
US3931944A Thrust reversal system for jet aircraft engines
DE2413244A1 AUTOMATIC BRAKING DEVICE
DE2411692A1 LIQUID FILTER
DE2409150A1 AUTOMATIC BRAKING DEVICE
DE2404807A1 ACCELERATION CONTROL VALVE FOR MEDIUM FLOW AND ACTUATOR SYSTEM WITH SUCH A VALVE
DE2364258A1 Flame tube for a gas turbine - assembled from silicon nitride ring elements with various, mating profiles
DE2363430A1 Tubular liquid atomizer - has nozzle behind swirl unit and second duct with offset openings above first nozzle
DE2362633A1 Flame tube for gas turbine combustion chamber - has number of ceramic rings formed of silicon nitride tiles