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contributor authorBrun, Klaus
contributor authorSimons, Sarah
contributor authorKurz, Rainer
date accessioned2017-11-25T07:15:59Z
date available2017-11-25T07:15:59Z
date copyright2017/21/3
date issued2017
identifier issn0742-4795
identifier othergtp_139_08_082604.pdf
identifier urihttp://138.201.223.254:8080/yetl1/handle/yetl/4233767
description abstractPressure pulsations into a centrifugal compressor can move its operating point into surge. This is concerning in pipeline stations where centrifugal compressors operate in series/parallel with reciprocating compressors. Sparks (1983, “On the Transient Interaction of Centrifugal Compressors and Their Piping Systems,” ASME Paper No. 83-GT-236); Kurz et al. (2006, “Pulsations in Centrifugal Compressor Installations,” ASME Paper No. GT2006-90700); and Brun et al. (2014, “Impact of the Piping Impedance and Acoustic Characteristics on Centrifugal Compressor Surge and Operating Range,” ASME J. Eng. Turbines Power, 137(3), p. 032603) provided predictions on the impact of periodic pressure pulsation on the behavior of a centrifugal compressor. This interaction is known as the “compressor dynamic response” (CDR) theory. Although the CDR describes the impact of the nearby piping system on the compressor surge and pulsation amplification, it has limited usefulness as a quantitative analysis tool, due to the lack of prediction tools and test data for comparison. Testing of compressor mixed operation was performed in an air loop to quantify the impact of periodic pressure pulsation from a reciprocating compressor on the surge margin (SM) of a centrifugal compressor. This data was utilized to validate predictions from Sparks’ CDR theory and Brun’s numerical approach. A 50 hp single-stage, double-acting reciprocating compressor provided inlet pulsations into a two-stage 700 hp centrifugal compressor. Tests were performed over a range of pulsation excitation amplitudes, frequencies, and pipe geometry variations to determine the impact of piping impedance and resonance responses. Results provided clear evidence that pulsations can reduce the surge margin of centrifugal compressors and that geometry of the piping system immediately upstream and downstream of a centrifugal compressor will have an impact on the surge margin reduction. Surge margin reductions of over 30% were observed for high centrifugal compressor inlet suction pulsation.
publisherThe American Society of Mechanical Engineers (ASME)
titleThe Impact of Reciprocating Compressor Pulsations on the Surge Margin of Centrifugal Compressors
typeJournal Paper
journal volume139
journal issue8
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4035822
journal fristpage82604
journal lastpage082604-15
treeJournal of Engineering for Gas Turbines and Power:;2017:;volume( 139 ):;issue: 008
contenttypeFulltext


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