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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: compressor 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
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Supplier: Siemens Energy Sector
Description: Four stage turbine All blades removable with rotor in place Hybrid burners for premix and diffusion mode operation with natural gas, fuel oil and special fuels such as heavy oil and refinery residues Low-NOx combustion system Siemens Gas Turbine Packages are
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Supplier: Siemens Energy Sector
Description: ,000,000 hours of fleet operation, the SGT6-5000F is designed for combined cycle and simple cycle applications as well as for integrated gasification (IGCC) applications. 16 can-type combustors 13-stage high efficiency compressor, advanced 3D blading 4-stage turbine
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Supplier: Siemens Energy Sector
Description: airfoils) Single-crystal turbine blades with thermal barrier coating and film cooling Advanced cooling technology Optional multiple fuels capability Low-NOx combustion system Siemens Gas Turbine Packages are the combination of standardized design with a
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Supplier: ASME Standards and Certification
Description: specific topic 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
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Supplier: ASME
Description: specific topic 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
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Supplier: Washington Alloy Co.
Description: exhibit excellent mechanical 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
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Supplier: Universal Wire Works Inc.
Description: and 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: Aerospace / Aircraft (AQ), Other
- Metal / Alloy Types: Alloy Steel (UNS G)
- Shape / Form: Wire / Shaped Wire
- Specialty Features: Corrosion Resistant
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Supplier: Washington Alloy Co.
Description: , petrochemical and aircraft industry. Aircraft uses would include the airframes; turbine engine parts such as the blades, discs, wheels and spacer rings. Other applications would include industrial fans, pressure vessels, compressor blades and rocket motor cases.
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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: 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: Safran Helicopter Engines
Description: maintenance. It comprises a 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
- Application: Aviation
- Engine Type: Internal Combustion
- Horse Power: 590 to 990 HP
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Supplier: Safran Helicopter Engines
Description: of this engine, Makila 1K2, was selected to power South Africa's Denel Aviation Rooivalk attack helicopter. At the end of the 90s, Turbomeca launched the 2,000-shp Makila 2. This variant incorporates a new axial/centrifugal compressor and a two-stage power turbine with reinforced
- Application: Aviation
- Engine Type: Internal Combustion
- Horse Power: 1800 to 2100 HP
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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: 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
- Applications: Other
- Maximum Working Pressure: 87.02 psi
- Primary Exchanger Material: Aluminum, Copper
- Type: Air-Cooled, Shell and Tube
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Supplier: Scanivalve Corporation
Description: , gas turbine tests, steam turbine tests, compressor tests as well as other turbomachinery testing. Industrial tests include pressure profiles on fan blades, or other surfaces. Overview Model DSA3016, Digital Sensor Array, is a rack mounted pressure module designed
- Device Category: Sensor
- Pressure Reading: Absolute
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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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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.