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ALSTOM TECHNOLOGY LTD BADEN

Overview
  • Total Patents
    170
About

ALSTOM TECHNOLOGY LTD BADEN has a total of 170 patent applications. Its first patent ever was published in 1996. It filed its patents most often in Germany and China. Its main competitors in its focus markets engines, pumps and turbines, thermal processes and electrical machinery and energy are SOLAR TURBINES INC, MITSUBISHI HITACHI POWER SYS and ALSTOM SWITZERLAND LTD.

Patent filings in countries

World map showing ALSTOM TECHNOLOGY LTD BADENs patent filings in countries
# Country Total Patents
#1 Germany 167
#2 China 3

Patent filings per year

Chart showing ALSTOM TECHNOLOGY LTD BADENs patent filings per year from 1900 to 2020

Top inventors

# Name Total Patents
#1 Paschereit Christian Oliver 10
#2 Kappis Wolfgang 9
#3 Savic Sasha 9
#4 Bachofner Rene 8
#5 Lacaze Alain 6
#6 Griffin Timothy 6
#7 Dittmann Rolf 6
#8 Doebbeling Klaus 5
#9 Althaus Rolf 5
#10 Fried Reinhard 5

Latest patents

Publication Filing date Title
DE102005052106A1 Fluid flow machine e.g. gas turbine has stator with blades which are detachably installed on stator and blades are secured over tensioned spring with safety lock pins at stator
DE102005047569A1 Thermal power process for hybrid turbine plant involves supplying heat to second process fluid before expansion
DE102005040802A1 Operation of a turbo compressor, with a turbine, measures the pressures at two different points for a rapid detection of an overload to trigger counter measures
DE102005040794A1 Telemetry system for transferring data between stationary and rotating components of gas turbine, comprises transmitters arranged on moving component for transferring data to receiver arranged on the stationary component
DE102005024696A1 Component part of especially turbo-engine has protective shroud installed around sleeve element to protect section of sleeve element protruding from cooling passage against effects of surrounding flow
DE102005024697A1 Arrangement for surface coating a region of a turbomachine blade comprises a recess for receiving a section of a gripping element for fixing a covering unit to a turbomachine blade in each side surface
DE102005020376A1 Humidifier for gas flow has means to determine fluid mass flow separated in droplet separator, and regulator to control atomizing pressure as regulating variable and position of operating component as correcting variable
DE102005014565A1 Method for preventing ice build up especially in air intake of gas turbine engine has controlled feedback of heated compressed air into the air intake to match computed expected icing levels
DE102004051260A1 Gas turbine assembly for a power plant comprises, downstream of a pump, a line leading to a spraying device that branches off from a line leading from the pump to a liquid injection site
DE102004049491A1 premix
DE102004042951A1 Machine unit e.g. sound absorber, holding device, has clamp arrangement with retainer, which is attached to machine units by retainer unit at one end and to support by connection region at other end
DE102004041794A1 Device for flame stabilizing in burner has catalyser assembly upstream of flame and through which flows air/pilot fuel mixture separate from air/fuel mixture, whereby catalyser assembly has at least two stages located in series
DE102004040890A1 Power station installation, has heat supply device arranged in waste gas path of gas turbo-group, upstream of heat transmission equipment
DE102004041275A1 Steam turbine arrangement, has high, medium and low pressure steam cylinders provided along combined shaft that is impelled with rated speed, and another high-pressure cylinder provided on separate shaft that is connected to compressor unit
DE102004041273A1 drilling
DE102004041271A1 Device and method for cooling a housing of a gas turbine or a combustion chamber
DE102004040577A1 Method for starting power station installation in deactivated electricity network, involves forming connection between generator of pressure store-relaxation turbine and start device of gas turbine group
DE102004040428A1 Power unit with gas turbine and compressed air store has stored fluid heat supply unit upstream from the pressure release device
DE102004040183A1 Gas turbine with heat recovery system has two discharge pipes fro compressor
DE102004040184A1 Rotor for a generator, in particular a turbogenerator of great power