Many end users view a factory performance test as an insurance policy to prevent performance issues that may be detected only after the machine is installed. This concern is certainly valid, but in today’s world, experienced compressor manufacturers rarely fail tests, especially if the application falls well within the manufacturer’s expertise. In certain cases, problems do not arise from aerodynamic performance but from rotordynamic performance— exactly the area not typically verified in standard factory aerodynamic tests unless a significantly more expensive factory test at site operating conditions (ASME PTC 10 Type 1 or full-load string test) is performed. These conditions can often be more easily and cost-effectively replicated in a site performance test.
Of course, if problems occur, they are often easier to remedy in a factory setting than onsite, especially if the site is remote or offshore, or if the machine is very large and heavy. The logistics of removing and shipping parts, e.g., a bundle, can be challenging. Therefore, lost time may be a factor to consider. However, the potential to lose time due to site problems must be balanced with the certainty of the additional time required for a factory test. Additionally, consideration should be given to the time needed to build or modify parts, which applies regardless of the test’s location.
The cost of the test is significantly higher for a factory test compared to a site test by at least an order of magnitude. The reason is that a factory test requires the machine to be fully installed and commissioned at the factory, which is a costly process. This is true even if temporary instrumentation must be installed onsite, such as instrumented spool pieces. Similarly, conducting a factory test takes a considerable amount of time, often several months. One significant issue in field testing is that not all sites permit freely adjusting the compressor operating conditions to the desired contractual values, or, if they do, they cannot accommodate the required duration of steady-state operating conditions. This challenge can often be mitigated by utilizing existing recycle loops or by adjusting other machines on-site.
Lastly, performance verification often pertains to the performance of the entire train. This can be expressed through requirements that specify the fuel or electricity consumption needed to operate under certain conditions, defined by isentropic head and mass flow. Another question is whether the train has enough power (at specified ambient conditions) to operate at a given operating condition (again specified by isentropic head and mass flow, and thus power). Many tests are most conveniently performed onsite, with the contract driver, and ideally, operating conditions for the compressor should be as close as possible to the contractual ones.
The intent of this text is not to convince end users to conduct factory tests, but rather to outline that in certain situations, a site performance test might be a worthwhile addition and sometimes an even more appropriate method for verifying contractual conditions. As a baseline for condition monitoring and plant optimization, field test data, assuming it is accurate enough, is certainly preferable to factory test data. While a factory test offers significant assurance that the machine will operate without issues in the field, it does not necessarily provide greater confidence in the actual machine’s efficiency and power requirements. Lastly, the argument for site tests would be considerably weaker if centrifugal compressors frequently failed performance tests. However, due to the design practices and accumulated knowledge of established manufacturers, a compressor very rarely fails a performance test.
Klaus Brun is the Director of R&D at Ebara Elliott Energy. He is also the past Chair of the Board of Directors of the ASME International Gas Turbine Institute and the IGTI Oil & Gas Applications Committee.
Rainer Kurz is a recent retiree as Manager of Gas Compressor Engineering at Solar Turbines Inc. in San Diego, CA. He is an ASME Fellow and has published over 200 articles and papers in the turbomachinery field.