Process used for coating a blade of a gas turbine comprises exciting the base material during coating in an ultrasound frequency range using a transmitting head connected to a vibrator
DE10001297A1
Spring loaded water spray valve has angled jets to spray onto vertical plates and with the rate of spraying determined by the number of jets opened through the water pressure
DE19963714A1
Method for repairing rotating components of gas turbine uses focussed material jet of water to separate predeterminable interface over an area of a component and then locking on replacement part with keyed engagement
DE19963377A1
Turbine blade with actively cooled cover band element
DE19963375A1
Cooling for the paddle tip at a gas turbine has a system to generate coolant air eddies at the gap between the paddle tip and the housing section where the hot gas flows through
DE19963373A1
Device for cooling a flow channel wall surrounding a flow channel with at least one rib train
DE19963346A1
Blade assembly in a turbo-engine and method for fitting blades on a rotor fits blades on a rotor crosswise to their operating orientation with a butt end in a perimeter recess for twisting them into their operating orientation.
DE19963349A1
Blade for gas turbines with throttle cross section at the rear edge
DE19961565A1
Coolant flow at a turbine paddle is adjusted by an inserted body into an opening in the coolant channel which reduces its cross section to give the required coolant flow vol
DE19961384A1
Process for the thermal treatment of rust ash from waste incineration plants
DE19959343A1
Sealing device to seal gap between two components, sealing grooves of which have wedge-shaped cross section
DE19959342A1
Heat recovery steam generator, especially for gas turbine unit of combined generation plant; has several parallel flow channels each assigned to section of catalyst unit to shut off individual channel
DE19953612A1
Horizontal heat exchanger with reversal chamber uses line venting chamber descending from topmost possible geodetic point through second medium chamber to chamber on input and output side.
DE19953123A1
Turbo assembly for steam power plant has high and mean pressure turbines on common shaft each with thrust compensating pistons where mean pressure piston is at outlet side on high pressure turbine to be fed direct with high pressure steam
DE19952884A1
Operation method for carbon dioxide gas turbine system, involves using combustion chamber in which fuel is burnt with oxygen, with at least one turbine and one generator
DE19938443A1
Fastening and fixing device
EP1076119A1
Apparatus and method for manufacture a directionally solidified columnar grained article
