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High Temperature Exhaust Gas Testing
High Temperature Exhaust Gas Testing-3D Cover (1)

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High Temperature Exhaust Gas Testing-3D Cover (1)

High Temperature Exhaust Gas Testing

Full-scale engine testing is not only expensive, complex, and time-consuming, but is also not typically available in the design and development phases of a new engine project. Test Devices' subscale turbine test rig offers a more affordable, qualitative, and accessible alternative for performing early stage validation tests. It also bridges the information gap that exists within testing capabilities available to aerospace propulsion designers and engineers.

In our eBook, High Temperature Exhaust Gas Testing, we highlight the benefits of subscale turbine testing along with various topics such as:

  • Our state-of-the-art TOAST Facility
  • Benefits of our TOAST Facility
  • Case Study: High Temperature Coating Test
  • Case Study: Exhaust Gas Flow Visualization Test
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Introduction

During the development of advanced aerospace structures and materials, having access to relevant test data significantly improves the success of the first article and overall confidence in designs. For both commercial jet engines and rocket engine parts, full-scale engine testing offers the most comprehensive data; however, it is very expensive, complex, and time consuming. Full-scale tests are also typically not available in the design and development phase of a new engine project.

Full-scale engine testing requires extensive modification to the engine to allow for instrumentation, the fitting of test parts, and the use of non-standard operating protocols within the testing (ex. overriding the built-in safety features). The complexity of the project, estimated timelines, and costs pile up quickly. The number of tests is also limited to the number of component copies that are available. Alternative testing methods such as gas burner or torch test can provide some relevant data, but are often limited and cannot fully simulate an engine-like environment.

Test Devices‘ subscale turbine test rig (TOAST: Turbine Operational Aero-thermal Subscale Test) offers an affordable and accessible alternative for performing the early stage validation test (or investigation) and bridging the information gap that currently exists within the testing capabilities available to aerospace propulsion designers and engineers.

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