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turbine compressor
Vibration-gas-abrasive wear resistance of turbine compressor blades
      
The scheme of gas-abrasive wear test of turbine compressor blades under free vibration of blades, including at high temperatures, is proposed.
      
Ti-N vacuum-plasma coatings for turbine compressor blades
      
Ti-N three-layer vacuum-plasma coatings 50-60-μm thick deposited on VT3- and OT4-alloy turbine compressor blades by a high-energy technology were studied.
      
Effect of the end clearances in a turbine compressor stage on its efficiency of operation
      
Fibre reinforced titanium matrix composites (TMCs) are being considered for use in future aeronautical gas-turbine compressor discs.
      
Using surface plastic deformation to increase the fatigue strength of aircraft gas-turbine compressor disks
      
We study the cyclic strength and durability of service-exposed turbine blades made of IN-738, ZMI-3U, and éP539LM nickel alloys, some of them with a protective coating, upon a long operating time in gas turbine compressor sets.
      
This is a report of an experiment performed on a test disk which was geometrically similar to a typical aircraft gas-turbine compressor disk.
      
Accelerated salt testing was found to be an effective method to systematically deteriorate gas turbine compressor performance.
      
An off line combustion turbine compressor water wash system is provided to help maintain plant performance between maintenance outages.
      
Figure 1a illustrates a typical forged turbine compressor blade, whilst figure 1b shows a blade cross-section.
      
High preheat temperatures representative of gas turbine compressor discharge temperatures were used.
      
In order to carry out this more realistic calculation a complete Turbine Compressor model is required and the modeling effort is in progress.
      
In the first cycle, natural gas and compressed air from a combustion turbine compressor are mixed and burned in a combustion chamber.
      
Note the evaporative cooler to reduce the temperature and to increase the density of the air entering the gas turbine compressor.
      
Pressurized combustion air is supplied by the turbine compressor to fluidize the bed.
      
Tables 38 and 39 provide the corresponding information for natural gas-fuelled turbine compressor engines.
      
Testing was based on fire incident histories, at medium to high airflow conditions in a gas turbine compressor.
      
This is accomplished by directing air flow from the gas turbine compressor through the bed preheating combustor.
      
 

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