Development of the Subsurface Process and Reinjection Compressor

J. Brady, K. Passmore, F. Paskvan, Jason C. Wilkes, T. Allison, E. Swanson, M KleinJohn
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Abstract

This paper discusses component developments, validation testing, and yard testing of the subsurface process and reinjection compressor (SPARC) prototype tool approaching downhole flowing conditions (≈1200 psig and > 225°F). This is the first time a compressor and turbo expander have been built small enough to be run through tubing and operated autonomously from the surface. A brief review of the overall system design and critical component design and testing are followed by a detailed review of the surface testing of the entire prototype machine at simulated downhole conditions. The SPARC concept uses the excess production pressure (energy) that is usually wasted across a choke or elsewhere in the production system to generate power through a downhole turbo-expander that runs a downhole gas compressor to reinject a portion of the gas stream. The system consists of a downhole separator, compressor, turbo-expander and other standard downhole equipment for the necessary plumbing. The successful test results of the bearing and thrust disk component testing at up to 1,000 psig and > 450°F are provided, followed by the successful yard test results of the entire SPARC prototype machine at downhole flowing conditions, including all the rotating equipment (turbo expander, compressor, and shaft), in situ process-lubrication system, and autonomous controls. This equipment will allow for the reduction of costly surface facilities to process, compress, and reinject produced gas into North Slope fields and some oil and condensate fields elsewhere globally, which are limited in liquid hydrocarbon production because of surface gas processing facility limitations. Another potential use of the SPARC technology is as an artificial lift mechanism for gas reservoirs. Using the SPARC as a gas well artificial lift system would require a redesign of the SPARC with an electric motor as its power source in place of the turbo-expander. However, no new technology breakthroughs are necessary because the technology has already been developed with the SPARC design. To date, there have been no small gas compressors, turbo expanders, and other necessary equipment built and tested that can be run through 4 1/2-in. tubing/casing and operate autonomously at downhole conditions. This technology opens up the possibilities of additional relatively inexpensive gas recycling on the North Slope and other condensate fields worldwide.
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地下工艺与回喷压缩机的发展
本文讨论了组件的开发、验证测试和井下过程的现场测试,以及接近井下流动条件(≈1200 psig, > 225°F)的再注入压缩机(SPARC)原型工具。这是首次将压缩机和涡轮膨胀器设计得足够小,可以通过油管下入,并在地面自动操作。简要回顾了整个系统设计和关键部件的设计与测试,然后详细回顾了整个原型机在模拟井下条件下的地面测试。SPARC概念利用通常浪费在节流管或生产系统其他地方的多余生产压力(能量),通过井下涡轮膨胀器产生电力,该膨胀器运行井下气体压缩机,重新注入一部分气流。该系统由井下分离器、压缩机、涡轮膨胀器和其他标准井下设备组成,用于必要的管道。提供了轴承和推力盘组件在高达1000 psig和> 450°F条件下的成功测试结果,随后是整个SPARC原型机在井下流动条件下的成功测试结果,包括所有旋转设备(涡轮膨胀器、压缩机和轴)、现场过程润滑系统和自主控制。由于地面天然气处理设备的限制,北坡油田和全球其他地方的一些油田和凝析油田的液态烃产量有限,因此该设备可以减少昂贵的地面设施对产出的天然气进行处理、压缩和再注入。SPARC技术的另一个潜在用途是作为气藏的人工举升机制。使用SPARC作为气井人工举升系统需要对SPARC进行重新设计,用电动机代替涡轮膨胀器作为动力源。然而,没有新的技术突破是必要的,因为该技术已经与SPARC设计一起发展。到目前为止,还没有小型气体压缩机、涡轮膨胀器和其他必要的设备可以运行在4 1/2英寸的管道中。油管/套管在井下条件下自动操作。这项技术为北坡和全球其他凝析气田提供了相对廉价的天然气回收利用的可能性。
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