Influence Of Axial Compressor Fouling On Gas Turbine Unit Performance Based On Different Schemes And With Different Initial Parameters Asme 98 Gt 416
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Author | : A. P. Tarabrin |
Publisher | : |
Total Pages | : 0 |
Release | : 1998 |
Genre | : |
ISBN | : |
Presented at the International Gas Turbine & Aeroengine Congress & Exhibition, Stockholm, Sweden, Jun 2-5, 1998.
Author | : A. P. Tarabrin |
Publisher | : |
Total Pages | : 6 |
Release | : 1998 |
Genre | : |
ISBN | : |
Author | : Michael Forsthoffer |
Publisher | : Butterworth-Heinemann |
Total Pages | : 206 |
Release | : 2018-11-16 |
Genre | : Technology & Engineering |
ISBN | : 0128097728 |
Forsthoffer's Component Conditioning Monitoring Handbook is dedicated to the condition monitoring of all rotating equipment. It describes the Forsthoffer Associates method of Component Condition Monitoring (CCM) and gives the reader detailed instructions on what to monitor for each component type. The author's easy and approachable style makes this a very practical reference for any level of technical background. This represents the latest addition to a set that includes volumes on 1. Fundamentals of Rotating Equipment; 2. Pumps; 3. Compressors; 4. Auxiliary Systems; 5. Reliability Optimization through Component Condition Monitoring and Root Cause Analysis'. - Contains separate chapters that address each of the 5 major components of all rotating machinery - Covers what parameters must be monitored when action is required to prevent unplanned shutdown - Describes how to use specific spreadsheets for condition monitoring tasks that can be downloaded from a companion website
Author | : Ahmed F. El-Sayed |
Publisher | : CRC Press |
Total Pages | : 396 |
Release | : 2022-04-27 |
Genre | : Science |
ISBN | : 1000546241 |
Foreign Object Debris and Damage in Aviation discusses both biological and non-biological Foreign Object Debris (FOD) and associated Foreign Object Damage (FOD) in aviation. The book provides a comprehensive treatment of the wide spectrum of FOD with numerous cost, management, and wildlife considerations. Management control for the debris begins at the aircraft design phase, and the book includes numerical analyses for estimating damage caused by strikes. The book explores aircraft operation in adverse weather conditions and inanimate FOD management programs for airports, airlines, airframe, and engine manufacturers. It focuses on the sources of FOD, the categories of damage caused by FOD, and both the direct and indirect costs caused by FOD. In addition, the book provides management plans for wildlife, including positive and passive methods. The book will interest aviation industry personnel, aircraft transport and ground operators, aircraft pilots, and aerospace or aviation engineers. Readers will learn to manage FOD to guarantee air traffic safety with minimum costs to airlines and airports.
Author | : |
Publisher | : |
Total Pages | : 412 |
Release | : 2001 |
Genre | : Mechanical engineering |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 414 |
Release | : 2001 |
Genre | : Mechanical engineering |
ISBN | : |
Author | : Inam U. Haq |
Publisher | : |
Total Pages | : 0 |
Release | : 1998 |
Genre | : |
ISBN | : |
Presented at the International Gas Turbine & Aeroengine Congress & Exhibition, Stockholm, Sweden, June 2 - June 5, 1998.
Author | : Michael Blaswich |
Publisher | : |
Total Pages | : 0 |
Release | : 1998 |
Genre | : |
ISBN | : |
Presented at the International Gas Turbine & Aeroengine Congress & Exhibition, Stockholm, Sweden, Jun 2-5, 1998.
Author | : Jonathan D. Baker |
Publisher | : |
Total Pages | : 76 |
Release | : 2002-09-01 |
Genre | : |
ISBN | : 9781423514671 |
This thesis presents a simple, meanline analysis of the impact of blade roughness on the mass flow, work coefficient, and efficiency of a three- stage axial compressor as a function of the location of fouling. First, an extensive review is presented on the state-of-the-art of measuring compressor degradation and on the impact of roughness on loss and deviation in a compressor cascade. The performance of a baseline, three-stage compressor, which has hydrodynamically smooth blades, is predicted. Using this baseline geometry, the influence of roughness in the front, middle and rear stages is calculated using empirical data for the enhanced losses and increased deviation, with a stage stacking technique. Influence coefficients that relate percentage changes in one parameter to percentage changes in other parameters are calculated. This analysis predicts that the most sensitive parameter for predicting fouling in the front stages is the percentage change in mass flow and the most sensitive parameter for predicting fouling in the rear stages is the efficiency.
Author | : Peter D. Silkowski |
Publisher | : |
Total Pages | : 0 |
Release | : 1998 |
Genre | : |
ISBN | : |
Presented at the International Gas Turbine & Aeroengine Congress & Exhibition, Stockholm, Sweden, Jun 2-Jun 5, 1998.