The VECTRA 40 power turbine was developed to match with the GE LM2500+ gas generator. Together, they offer the most effective power package available for high-speed operation. As part of a complete package with the GE LM2500+, the VECTRA turbine has an ISO rating of 40,200 horsepower (30 megawatts). Thermal efficiency is 39.9 percent at full load, with a corresponding mass flow to 180 pounds per second. The VECTRA 40 has a maximum continuous operating speed of 6,500 RPM. It is the highest speed power turbine available for the GE LM2500+.

The new VECTRA 40 modular design improves serviceability while reducing downtime. The VECTRA power turbine can be installed and removed as a unit, either separate from, or with the gas generator. These design advantages will produce significant operational savings to the customer over the extended life cycle of the power turbine.

VECTRA power design features include:

  • Two-stage overhung rotor 
  • Rolling element bearings 
  • Center tie and curvic couplings

In addition, Dresser-Rand will optionally package new equipment with a Dry Low Emissions (DLE) combustion system to reduce the amount of NOx, CO and unburned hydrocarbons when burning natural gas fuel.

 

VECTRA 40 Performance Summary
Design Speed: 6,200 RPM
Maximum Continuous Speed: 6,500 RPM
Power: 40,200 HP  30,000 KW
Efficiency: 39.9%
Mass Flow: 180 lbs/sec


The DR-61 was developed as an efficient, cost-effective, and reliable power turbine for the GE LM2500 gas generator. The DR-61 is an industrial, heavy duty, mechanical drive turbine with an output shaft design speed of 5500 rpm. The LM2500 is an industrial derivative of the CF6 high efficiency turbofan engine installed on wide body commercial aircraft.

The DR-61 is a two-stage power turbine that is bolted rigidly to the LM2500. The resulting short power turbine inlet diffuser reduces the total pressure loss and improves overall efficiency. To avoid thermal distortion, which can lower efficiency, all turbine casing components are symmetrical, unsplit rings from the gas generator discharge to the power turbine diffuser exhaust.

The two-stage rotor has cooled discs and tip shrouded blades for durability. In addition, the tip shrouds run against abradable honeycomb seals in the casing to minimize leakage and improve efficiency. All elements of the rotor have been designed for a creep life of over 100,000 hours at full load. The materials utilized are modern super-alloys specifically developed for service at the temperatures encountered.

The power turbine shaft is designed to insure the first bending critical speed of the rotor is well above the maximum operating speed. The shaft is supported in two tilting pad journal bearings. A tilting shoe thrust bearing in mounted in the same housing as the aft journal bearing.

An optional shaft driven accessory gearbox can be provided which is bolted to the coupling end on the bearing housing. The gearbox has three shafts that can be used for oil pumps or other accessory drives.

The DR-61 package can be supplied with either a standard combustion system or a GE Dry Low Emissions system designed to reduce the amount of NOx, CO, and unburned hydrocarbons in the exhaust.

DR-61 Design Summary

Package

  • GE LM2500 gas generator
  • DLE or standard package

Power Turbine

  • Heavy duty industrial design
  • Oil film bearings
  • Two-stage overhung rotor
  • Tip shrouded blades
  • Design life of 100,000 hours
DR-61 Performance Summary
Design Speed: 5,500 RPM
Maximum Continuous Speed: 5,775 RPM
Power: 31,000 HP  23,100 KW
Efficiency: 37.5%

 

 

© Dresser-Rand 2008 All Rights Reserved. Privacy Policy & Terms of Use