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UNITED TURBINE AB & CO

Overview
  • Total Patents
    82
About

UNITED TURBINE AB & CO has a total of 82 patent applications. Its first patent ever was published in 1970. It filed its patents most often in United States, Sweden and United Kingdom. Its main competitors in its focus markets engines, pumps and turbines, transport and machines are TURBOKONSULT AB, CENTRAX POWER UNITS LTD and CHAIR R S DE.

Patent filings in countries

World map showing UNITED TURBINE AB & COs patent filings in countries
# Country Total Patents
#1 United States 18
#2 Sweden 17
#3 United Kingdom 13
#4 Japan 12
#5 France 11
#6 Germany 8
#7 Italy 3

Patent filings per year

Chart showing UNITED TURBINE AB & COs patent filings per year from 1900 to 2020

Top inventors

# Name Total Patents
#1 Kronogard Sven-Olof 15
#2 Kronogard S O 10
#3 Suben Orofu Kuronogorudo 8
#4 Kronogard S-O 8
#5 Kronogaard Sven-Olof 7
#6 Kronogard Sven Olof 3
#7 Subennorofu Kuronogorudo 2
#8 Kronogard Sven O 1
#9 Silverqvist K 1
#10 Kurasu Orofu Kuronogaruto 1

Latest patents

Publication Filing date Title
JPS5825521A Gas-turbine power device for automobile
FR2465078A2 Gas turbine engine group having a ceramic rotor elastically mounted on a metal shaft
US4176519A Gas turbine having a ceramic rotor
GB1504430A Gas turbine power plant having three rotors
US4070825A Gas turbine power plant
GB1526026A Gas turbine engine and transmission for vehicle propulsio
US4025221A Automotive gas turbine power plant
DE2559172A1 Gas turbine plant with two turbine impellers - has first turbine wheel under-dimensioned and manufactured from ceramic material
JPS5281408A Gas turbine power equipment
GB1523640A Gas turbine power plant
IT1053270B Gas turbine plant with two turbine impellers - has first turbine wheel under-dimensioned and manufactured from ceramic material
US4064690A Gas turbine power plant
US3958655A Gas turbine engine for vehicle propulsion
DE2458273A1 Compressor with centripetal and centrifugal stages - first stage has adjustable inlet guide vanes and outlet vanes downstream of rotor
DE2458274A1 Gas turbine unit especially for motor vehicle propulsion - has two heat exchangers and power take off on compressor side
GB1461430A Compressor having two or more stages
GB1477648A Gas turbine power plant
JPS5158705A Futatsu mataha soreijonoatsushukudanojusuruatsushukuki
US3941499A Compressor having two or more stages
DE2451741A1 Gas turbine engine for vehicles - has infinitely variable gearing between turbine and compressor