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New Design Method of a Supersonic Steam Injection Nozzle and Its Numerical Simulation Verification

[Image: see text] Steam huff-n-puff in horizontal wells often had limitations, such as uneven steam injection and low reservoir utilization. To improve steam injection efficiency, a new method for designing a supersonic nozzle was proposed based on the principles of aerodynamics and thermodynamics....

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Autores principales: Wang, Qianhui, Pang, Zhanxi, Tian, Cong, Chen, Jiajie
Formato: Online Artículo Texto
Lenguaje:English
Publicado: American Chemical Society 2023
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC10688040/
https://www.ncbi.nlm.nih.gov/pubmed/38046301
http://dx.doi.org/10.1021/acsomega.3c01835
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author Wang, Qianhui
Pang, Zhanxi
Tian, Cong
Chen, Jiajie
author_facet Wang, Qianhui
Pang, Zhanxi
Tian, Cong
Chen, Jiajie
author_sort Wang, Qianhui
collection PubMed
description [Image: see text] Steam huff-n-puff in horizontal wells often had limitations, such as uneven steam injection and low reservoir utilization. To improve steam injection efficiency, a new method for designing a supersonic nozzle was proposed based on the principles of aerodynamics and thermodynamics. The nozzle featured a tapering section, a throat, and a diverging section. The best geometric shape of the tapering section was the Witoszynski curve. A set of nozzle size designs were established, and the size parameters were optimized. The results showed that the nozzle could inject steam into the formation at supersonic speed and it had the characteristics of constant flow rate and uniform development of the steam chamber. According to the steam Reynolds number and the good aggregation distribution characteristics of the size design model, three sequential nozzles of 3.0, 5.0, and 6.5 mm were formed based on the throat. When the throat diameter was 5.0 mm, the tapering length was 4.3 mm, the diverging length was 5.5 mm, the throat length was 3.0 mm, the inlet diameter was 9.8 mm, and the outlet diameter was 6.2 mm. Numerical simulations indicated that the pressure drop loss during steam huff-n-puff injection in horizontal wells was within 10%. It was of great significance to establish the nozzle size design model of the steam injection effect of horizontal wells.
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spelling pubmed-106880402023-12-01 New Design Method of a Supersonic Steam Injection Nozzle and Its Numerical Simulation Verification Wang, Qianhui Pang, Zhanxi Tian, Cong Chen, Jiajie ACS Omega [Image: see text] Steam huff-n-puff in horizontal wells often had limitations, such as uneven steam injection and low reservoir utilization. To improve steam injection efficiency, a new method for designing a supersonic nozzle was proposed based on the principles of aerodynamics and thermodynamics. The nozzle featured a tapering section, a throat, and a diverging section. The best geometric shape of the tapering section was the Witoszynski curve. A set of nozzle size designs were established, and the size parameters were optimized. The results showed that the nozzle could inject steam into the formation at supersonic speed and it had the characteristics of constant flow rate and uniform development of the steam chamber. According to the steam Reynolds number and the good aggregation distribution characteristics of the size design model, three sequential nozzles of 3.0, 5.0, and 6.5 mm were formed based on the throat. When the throat diameter was 5.0 mm, the tapering length was 4.3 mm, the diverging length was 5.5 mm, the throat length was 3.0 mm, the inlet diameter was 9.8 mm, and the outlet diameter was 6.2 mm. Numerical simulations indicated that the pressure drop loss during steam huff-n-puff injection in horizontal wells was within 10%. It was of great significance to establish the nozzle size design model of the steam injection effect of horizontal wells. American Chemical Society 2023-11-15 /pmc/articles/PMC10688040/ /pubmed/38046301 http://dx.doi.org/10.1021/acsomega.3c01835 Text en © 2023 The Authors. Published by American Chemical Society https://creativecommons.org/licenses/by-nc-nd/4.0/Permits non-commercial access and re-use, provided that author attribution and integrity are maintained; but does not permit creation of adaptations or other derivative works (https://creativecommons.org/licenses/by-nc-nd/4.0/).
spellingShingle Wang, Qianhui
Pang, Zhanxi
Tian, Cong
Chen, Jiajie
New Design Method of a Supersonic Steam Injection Nozzle and Its Numerical Simulation Verification
title New Design Method of a Supersonic Steam Injection Nozzle and Its Numerical Simulation Verification
title_full New Design Method of a Supersonic Steam Injection Nozzle and Its Numerical Simulation Verification
title_fullStr New Design Method of a Supersonic Steam Injection Nozzle and Its Numerical Simulation Verification
title_full_unstemmed New Design Method of a Supersonic Steam Injection Nozzle and Its Numerical Simulation Verification
title_short New Design Method of a Supersonic Steam Injection Nozzle and Its Numerical Simulation Verification
title_sort new design method of a supersonic steam injection nozzle and its numerical simulation verification
url https://www.ncbi.nlm.nih.gov/pmc/articles/PMC10688040/
https://www.ncbi.nlm.nih.gov/pubmed/38046301
http://dx.doi.org/10.1021/acsomega.3c01835
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