Analysis of the Impact of Low Temperature on Constant Output Pressure for Civil Aircraft Engine Driven Pump

Analysis of the Impact of Low Temperature on Constant Output Pressure for Civil Aircraft Engine Driven Pump

WU Tong

Hydraulics Pneumatics & Seals ›› 2025, Vol. 45 ›› Issue (10) : 114-118.

PDF(1199 KB)

PDF(1199 KB)

Hydraulics Pneumatics & Seals ›› 2025, Vol. 45 ›› Issue (10) : 114-118. DOI: 10.3969/j.issn.1008-0813.2025.10.017

System & Application

Analysis of the Impact of Low Temperature on Constant Output Pressure for Civil Aircraft Engine Driven Pump

{{article.zuoZhe_EN}}

Author information +

History +

HeighLight

{{article.keyPoints_en}}

Abstract

{{article.zhaiyao_en}}

Key words

QR code of this article

Cite this article

Download Citations

{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 2025, 45(10): 114-118 https://doi.org/10.3969/j.issn.1008-0813.2025.10.017

References

Publishing order | Descend order by publishing year | Descend order by cited within

References

{{article.reference}}

Funding

RIGHTS & PERMISSIONS

{{article.copyrightStatement_en}}

{{article.copyrightLicense_en}}

PDF(1199 KB)

Accesses

Citation

Detail

Sections

Recommended

/

〈

〉