Gas Turbine Overhaul

Description: The Siemens SGT-800 industrial gas turbine combines a reliable robust design with high efficiency and low emissions. This makes the SGT-800 an excellent choice for Industrial, Refinery and Oil & Gas applications in simple cycle, cogeneration or combined cycle installations. Over

Description: This SAE Aerospace Recommended Practice (ARP) provides to the aerospace industry a procedure for the consistent and accurate calculation of fuel flow using turbine flowmeters during development, production, and post overhaul/repair gas turbine engine testing.

Description: This SAE Aerospace Recommended Practice (ARP) provides to the aerospace industry a procedure for the consistent and accurate calculation of fuel flow using turbine flowmeters during development, production, and post overhaul/repair gas turbine engine testing.

Description: review, theoretical fundamentals, and design guide. The subject matter is primarily piston aeroengine superchargers - developed in Germany during the Second World War (WWII) - which are centrifugal compressors driven either by the main engine crankshaft or by an exhaust gas turbine.

Description: review, theoretical fundamentals, and design guide. The subject matter is primarily piston aeroengine superchargers - developed in Germany during the Second World War (WWII) - which are centrifugal compressors driven either by the main engine crankshaft or by an exhaust gas turbine.

Description: ISO 18888:2017 specifies standard rules for preparing, conducting, evaluating and reporting thermal performance tests on combined cycle and cogeneration power plants driven by gas turbines for base and part load operation with or without supplementary firing. ISO 18888:2017 is

Description: General purpose dynamometers, lightweight, portable, quick overhaul

• Application: General Purpose, Aircraft / Aerospace, Chain / Belt Drives, Gearboxes, Fluid Power Systems, Gas / Diesel Engines, Transmissions, Turbines
• Data Acquisition / Logging: Yes
• Dynamometer Interface: Separate Controller
• Maximum Power Absorption: 1000 HP

Description: Tough and durable, with field-proven head design to maximize time between overhauls. CG137 engines are equipped with ADEM A4 technology that brings performance, uptime, and low operating cost to your operation. CG137 engines meet the most demanding continuous duty gas compression

• Application: Industrial
• Displacement: 18.01 liters
• Engine Type: Internal Combustion
• Fuel Type: CNG

Description: The Froude HS range of Aerospace and Gas Turbine Engine Test Equipment has been developed over the years to meet the needs of testing new engines in R&D facilities. These state-of-the-art products are utilized in subsequent production facilities and the engine overhaul sector.

• Application: Aircraft / Aerospace, Gas / Diesel Engines, Industrial, Turbines
• Maximum Power Absorption: 2252 to 40207 HP
• Maximum Rotary Speed: 30000 rpm
• Technology: Hydraulic / Water Brake

Description: Tough and durable, with field-proven head design to maximize time between overhauls. CG137 engines are equipped with ADEM A4 technology that brings performance, uptime, and low operating cost to your operation. CG137 engines meet the most demanding continuous duty gas compression

• Application: Industrial
• Displacement: 27.01 liters
• Engine Type: Internal Combustion
• Fuel Type: CNG

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

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

Description: maintenance operations. Depending on the variant, Time Between Overhaul (TBO) is between 3,000 and 4,000 hours. It comprises a single-stage centrifugal compressor, a single-stage turbine and a power turbine. Earlier variants have a hydro-mechanical control system while more

• Application: Aviation
• Engine Type: Internal Combustion
• Horse Power: 450 to 750 HP

Description: Improving Workforce Efficiency • Standard factory certifications improve worksite safety • - Class I Division 2 (NEC 500) • - Class I Zone 2 (NEC 505) • - ATEX Directive (94/9/EC) Group II • - 3G Environments (Zone 2) with Gas Group IIA

• Application: Industrial
• Displacement: 15.21 liters
• Engine Type: Internal Combustion
• Features: EPA Certified, EPA Tier 2/EU Stage II