Cascade Test Rig

Cascade Test Rigs are specialized test setups used to measure the aerodynamic performance of fan, compressor, and turbine blades. Cascade Test Rigs simulate the actual operating conditions of the blades to optimize blade profiles. In these systems, the test article consists of either a single blade or a specific number of blades within a defined angle. With Cascade Test Rigs, blade profiles are analyzed for pressure distribution,[…]
Details

Fan Test Rig

Fan Test Rigs are primarily used to determine the aerodynamic, structural, and aeroacoustic characteristics of aviation engine fans. These test rigs can be resized (re-sizing) according to the stage, speed, power, and diameter values of the fans to be tested, or they can be designed in full scale based on the infrastructure capacity. The testing processes for fans, which are critical main components of aviation engines, are[…]
Details

Compressor Test Rig

Compressor Test Rigs are complex test systems used to measure the performance of axial, radial, or mixed-flow (axial-radial) compressors in aviation engines, generate compressor maps, and measure Tip Clearances and Blade Tip Timing. When designing Compressor Test Rigs, they can be resized based on the number of stages, rotational speed, power, and diameter of the compressor to be tested, or they can be designed in full scale[…]
Details

Combustion Chamber Test Rig

Combustion Chamber Test Rigs are primarily used to observe pressure losses, flow distributions, combustion acoustics, combustion efficiencies, emission values, and material or coating durability of combustion chambers in aviation engines. Combustion Chamber Test Rigs can be designed to test either full-scale combustion chambers or specific sections, depending on the type of combustion chamber and infrastructure capabilities. Combustion chambers are systems that require a wide range of[…]
Details

Turbine Test Rig

Turbine Test Rigs are used to observe pressure losses, power outputs, tip clearances, blade tip vibration (Blade Tip Timing) values, material or coating durability, and blade cooling performance of turbines in aviation engines. To perform these tests reliably, in addition to air conditioning systems, intensive instrumentation integration on the test article is required. Customized instrumentation designs, precise data acquisition, and control capabilities play a crucial role in[…]
Details