FT8A, a New High Performance 25 MW Mechanical Drive Aero Derivative Gas Turbine

doi 10.1115/90-gt-287
Full Text
Abstract

Available in full text

Date
Authors
Publisher

American Society of Mechanical Engineers

Related search

Energy Saving II. High Efficiency Gas Turbine Power Generation Systems Using Aero-Derivative Gas Turbines.

JAPAN TAPPI JOURNAL
1997English

Aero-Elastic Optimization of a 10 MW Wind Turbine

2015English

Aero Gas Turbine Flight Performance Estimation Using Engine Gas Path Measurements

Journal of Propulsion and Power
SpacePlanetary ScienceFuel TechnologyMechanical EngineeringAerospace Engineering
2015English

Developments Leading to an Axial Flow Compressor for a 25 MW Class High Efficiency Gas Turbine

1990English

Marine Support Concepts for Aero Derivative Turbine Engines

1990English

Remote Operation and Monitoring of a Micro Aero Gas Turbine

Aeronautical Journal
Aerospace Engineering
2017English

Turbine Rebuild Effects on Gas Turbine Performance

1992English

Logistic Support of Aero Derivative Marine Gas Turbines in the Royal Navy

1976English

Length Reduction and the Performance Improvement of a High-Pressure Gas Turbine Combustor.

Nihon Kikai Gakkai Ronbunshu, B Hen/Transactions of the Japan Society of Mechanical Engineers, Part B
Condensed Matter PhysicsMechanical Engineering
1989English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2024 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy