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Supplier: Accuris
Description: COMPRESSOR ROTOR BLADES, GAS TURBINE TANK ENGINE, PROCESSING, INSPECTION, AND INDENTIFICATION OF
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Supplier: Siemens Energy Sector
Description: Plant 1x1 2x1 Net Plant Power Output (MW) 253 512 Net Plant Efficiency (%) 52,5 53,1 Heat Rate (kj/kWh) 6857 6780 Heat Rate (Btw/kWh) 6499 6426 Condenser Pressure (bar) not published not published Gas Turbine Gross Power (kW) 168,000 336,000 Steam Turbine Gross Power (kW) 89,000
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Supplier: Siemens Energy Sector
Description: applications. Its state-of-the-art technology is based on proven design features. Annular, walk-in combustion chamber with 24 hybrid burners Ceramic combustion chamber tiles 15-stage axial flow compressor with optimized flow distribution (controlled diffusion airfoils) Single-crystal
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Supplier: Siemens Energy Sector
Description: drive design, derived from proven standards, can be used e.g. for the production of Liquified Natural Gas (LNG) – either as a direct mechanical compressor drive or as an all-electric generator version. The fleet of more than 90 turbines is in commercial operation since 1989 and
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Supplier: Siemens Energy Sector
Description: The powerful and reliable SGT6-5000F enables you to get the full potential from all components and achieve maximum cost efficiency whether in peak-, intermediate-, or base-load duty. The SGT6-5000F gas turbine continues to break reliability and continuous operation records. With more
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Supplier: Universal Wire Works Inc.
Description: oxidation resistance in gas turbine atmospheres and is recommended for turbine blades, shafts, turbine and compressor disc, spacers, fasteners and miscellaneous jet engine hardware. Waspalloy is suitable n replacing Nimonc 90 alloy in selected applications.
- Specifications: AMS
- Applications: Aerospace / Aircraft (AQ)
- Type: Alloy, Alloy Steel (UNS G)
- Features: Corrosion Resistant, Ferrous / Iron Based - Any Type, Other
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Supplier: Washington Alloy Co.
Description: properties at temperature up to 1400oF with good oxidation and corrosion resistance at temperatures as high as 1600oF. Washington Alloy Waspaloy? is commonly used in gas turbine atmospheres; turbine blades, shafts, turbine and compressor discs, spacers,
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Supplier: ASME Standards and Certification
Description: areas include: fluid dynamics and heat transfer phenomena in compressor and turbine components of gas turbine engines, turbinem blade and measurement advancements, and the impact on cavity leaking flows on performance. Published: Monthly Subscriptions currently
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Supplier: ASME
Description: areas include: fluid dynamics and heat transfer phenomena in compressor and turbine components of gas turbine engines, turbinem blade and measurement advancements, and the impact on cavity leaking flows on performance. Published: Monthly Subscriptions currently
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Supplier: Safran Helicopter Engines
Description: single-stage axial compressor, a single-stage centrifugal compressor, a two-stage gas generator turbine and a single-stage power turbine. The Arriel 2 is a significant development of the Arriel 1, offering greater power and a simpler single-stage turbine
- Horse Power: 590 to 990 HP
- Application: Aviation
- Engine Type: Internal Combustion
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Supplier: SAE International
Description: This document discusses, in broad general terms, typical present instrumentation practice for post-overhaul gas turbine engine testing. Production engine testing and engine development work are outside the scope of this document as they will typically use many more channels of
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Supplier: SAE International
Description: This document discusses, in broad general terms, typical present instrumentation practice for post-overhaul gas turbine engine testing. Production engine testing and engine development work are outside the scope of this document; they will use many more channels of instrumentation, and
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Supplier: IHS ESDU
Description: documents that provide methods for estimating noise are referenced at the point where those components are discussed. The propulsion system is first considered. In the case of gas turbine engines the contributions from the jet, fan, compressor, turbine and core are
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Supplier: Scanivalve Corporation
Description: include pressure inputs from the front of the DSA3016 pressure module (FA) or from the rear of the enclosure (RA). These applications include measuring gas pressures in wind tunnel tests, gas turbine tests, steam turbine tests, compressor tests as well as other
- Measurement Type: Absolute
- Device Category: Sensor
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Supplier: Alfa Laval Inc.
Description: cooling, turbine cooling, oil cooling and various other processes (transformers, air compressors, etc.). Standard configuration Finned coil F5 - Cu-tubes ø 12.7 mm - corrugated Al-fins 0.14 mm, no turbulators - fin spacing 2.3 mm Two casing widths (SEM=1630 mm, SED=2400 mm) Flanges
- Maximum Working Pressure: 87.02262 psi
- Technology: Air-Cooled, Shell and Tube
- Primary Material: Aluminum, Copper
- Features: Other
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Oil and Gas: Used in valves, pumps, and compressors requiring high-performance seals. (read more)
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and labyrinth seal applications, even in temperatures up to 1400F [760C]. With over 30 years of successful operation and over 1,000,000,000 hours of operation, it’s no wonder that major gas turbine manufacturers have adopted FELTMETAL™ Abradable Seals for flow path efficiency (read more)
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and labyrinth seal applications, even in temperatures up to 1400F [760C]. With over 30 years of successful operation and over 1,000,000,000 hours of operation, it’s no wonder that major gas turbine manufacturers have adopted FELTMETAL™ Abradable Seals for flow path efficiency (read more)
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Control system design and process or plant engineers in search of a fuel gas measurement solution for natural gas compressor skids will find that the economical, low-maintenance Wafer-Cone® Flow Meter (read more)
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Gaumer Process provides standard fuel gas conditioning systems (in accordance with Gaumer standard specifications) and custom engineered (in accordance with customer specifications) to meet the desired requirements of gas turbines, engines, burners and compressors of different makes. The (read more)
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Some Peculiarities of Fatigue Crack Growth at Various Stages of Its Development
V. T. Troshchenko and A. V. Prokopenko, “Fatigue strength of gas turbine compressor blades ,” Eng. Failure Analysis, 7, 209–220 (2000).
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Fatigue strength and life of compressor blades for marine gas turbine engines
The main factors which influence the threshold stress intensity factor Kth and the parameters n and A of the Paris equation as applied to the materials of marine gas turbine compressor blades is the medium (the vapors of a sea-salt solution…
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Vibration and Crack Detection in Gas Turbine Engine
Compressor Blades using Eddy Current Sensors
Ritchie explored the growth of high cycle fatigue cracks in gas turbine compressor blades .
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Cranfield University
Therefore, this PhD research has as its objective to obtain a model to predict the fouling in gas turbine compressor blades .
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Dynamic test and fatigue life evaluation of compressor blades
A fatigue life design procedure for the gas turbine compressor blade was established on the basis of the design, analysis, and test processes implemented in a previous study.
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Investigation of Fatigue Failures of Titanium Alloy Blades Used in Compressor Modules of Aeroderivative Industrial Gas Turbines
In this paper two failure case-studies of titanium alloy used for aeroderivative gas turbine compressor blades are pre- sented.
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Failure Analysis and Repair of a Catastrophically Damaged Gas Turbine Compressor Disk Using SEM Technique and CFD Analysis
Kermanpur et al. [15] investigated the fracture of gas turbine compressor blades , which occurred in Hesa power plant in Isfahan and found that the fracture initiated at the contact between the disk and blades in the dovetail region and because of weak…
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A New Approach to Characterization of Gas Turbine Components Affected by Pitting Corrosion
During their operation, inade- quate filtering systems or lack of proper maintenance of the inlet air can contribute to the occurrence of pitting corro- sion and, as a consequence, can lead to failure of gas turbine compressor blades .
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Physical phenomena in the polishing of compressor blades for gas-turbine engines
Since titanium alloys are generally used in the pro duction of gas turbine compressor blades , we investi gate the polishing of VT3 1 and VT8 M titanium alloy blades in the present work.