Design and validation of hydraulic pump system driven by the electromotor under the high-power and long-Time working state in an airborne

Huijun Jiang; Zhenshui Li; Hong Liu; Zongxia Jiao; Yaoxing Shang; Xiaochao Liu

doi:10.1109/AUS.2016.7748177

Design and validation of hydraulic pump system driven by the electromotor under the high-power and long-Time working state in an airborne

Huijun Jiang
, Zhenshui Li
, Hong Liu
, Zongxia Jiao
, Yaoxing Shang
, Xiaochao Liu

School of Automation Science and Electrical Engineering

AVIC The First Aircraft Institute

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

1 Scopus citations

Abstract

This paper introduced a type of aircraft electric hydraulic pump system working principle, the key points of the system are analyzed and described, including calculation of boost pressure, system oil temperature control design, environmental temperature checking, starting logic design, the system validation and verification methods are expounded. This system passed through the ground test and flight time Validation, and worked well and reliably.

Original language	English
Title of host publication	AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	874-878
Number of pages	5
ISBN (Electronic)	9781509010875
DOIs	https://doi.org/10.1109/AUS.2016.7748177
State	Published - 17 Nov 2016
Event	2016 IEEE/CSAA International Conference on Aircraft Utility Systems, AUS 2016 - Beijing, China Duration: 10 Oct 2016 → 12 Oct 2016

Publication series

Name	AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems

Conference

Conference	2016 IEEE/CSAA International Conference on Aircraft Utility Systems, AUS 2016
Country/Territory	China
City	Beijing
Period	10/10/16 → 12/10/16

Access to Document

10.1109/AUS.2016.7748177

Cite this

Jiang, H., Li, Z., Liu, H., Jiao, Z., Shang, Y., & Liu, X. (2016). Design and validation of hydraulic pump system driven by the electromotor under the high-power and long-Time working state in an airborne. In AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems (pp. 874-878). Article 7748177 (AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/AUS.2016.7748177

Jiang, Huijun ; Li, Zhenshui ; Liu, Hong et al. / Design and validation of hydraulic pump system driven by the electromotor under the high-power and long-Time working state in an airborne. AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems. Institute of Electrical and Electronics Engineers Inc., 2016. pp. 874-878 (AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems).

@inproceedings{ef8321926dc2427489396e78db52b1ab,

title = "Design and validation of hydraulic pump system driven by the electromotor under the high-power and long-Time working state in an airborne",

abstract = "This paper introduced a type of aircraft electric hydraulic pump system working principle, the key points of the system are analyzed and described, including calculation of boost pressure, system oil temperature control design, environmental temperature checking, starting logic design, the system validation and verification methods are expounded. This system passed through the ground test and flight time Validation, and worked well and reliably.",

author = "Huijun Jiang and Zhenshui Li and Hong Liu and Zongxia Jiao and Yaoxing Shang and Xiaochao Liu",

note = "Publisher Copyright: {\textcopyright} 2016 IEEE.; 2016 IEEE/CSAA International Conference on Aircraft Utility Systems, AUS 2016 ; Conference date: 10-10-2016 Through 12-10-2016",

year = "2016",

month = nov,

day = "17",

doi = "10.1109/AUS.2016.7748177",

language = "英语",

series = "AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems",

publisher = "Institute of Electrical and Electronics Engineers Inc.",

pages = "874--878",

booktitle = "AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems",

address = "美国",

}

Jiang, H, Li, Z, Liu, H, Jiao, Z , Shang, Y & Liu, X 2016, Design and validation of hydraulic pump system driven by the electromotor under the high-power and long-Time working state in an airborne. in AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems., 7748177, AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems, Institute of Electrical and Electronics Engineers Inc., pp. 874-878, 2016 IEEE/CSAA International Conference on Aircraft Utility Systems, AUS 2016, Beijing, China, 10/10/16. https://doi.org/10.1109/AUS.2016.7748177

Design and validation of hydraulic pump system driven by the electromotor under the high-power and long-Time working state in an airborne. / Jiang, Huijun; Li, Zhenshui; Liu, Hong et al.
AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems. Institute of Electrical and Electronics Engineers Inc., 2016. p. 874-878 7748177 (AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

TY - GEN

T1 - Design and validation of hydraulic pump system driven by the electromotor under the high-power and long-Time working state in an airborne

AU - Jiang, Huijun

AU - Li, Zhenshui

AU - Liu, Hong

AU - Jiao, Zongxia

AU - Shang, Yaoxing

AU - Liu, Xiaochao

PY - 2016/11/17

Y1 - 2016/11/17

N2 - This paper introduced a type of aircraft electric hydraulic pump system working principle, the key points of the system are analyzed and described, including calculation of boost pressure, system oil temperature control design, environmental temperature checking, starting logic design, the system validation and verification methods are expounded. This system passed through the ground test and flight time Validation, and worked well and reliably.

AB - This paper introduced a type of aircraft electric hydraulic pump system working principle, the key points of the system are analyzed and described, including calculation of boost pressure, system oil temperature control design, environmental temperature checking, starting logic design, the system validation and verification methods are expounded. This system passed through the ground test and flight time Validation, and worked well and reliably.

UR - https://www.scopus.com/pages/publications/85006804275

U2 - 10.1109/AUS.2016.7748177

DO - 10.1109/AUS.2016.7748177

M3 - 会议稿件

AN - SCOPUS:85006804275

T3 - AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems

SP - 874

EP - 878

BT - AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems, AUS 2016

Y2 - 10 October 2016 through 12 October 2016

ER -

Jiang H, Li Z, Liu H, Jiao Z , Shang Y , Liu X. Design and validation of hydraulic pump system driven by the electromotor under the high-power and long-Time working state in an airborne. In AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems. Institute of Electrical and Electronics Engineers Inc. 2016. p. 874-878. 7748177. (AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems). doi: 10.1109/AUS.2016.7748177

Design and validation of hydraulic pump system driven by the electromotor under the high-power and long-Time working state in an airborne

Abstract

Publication series

Conference

Access to Document

Other files and links

Fingerprint

Cite this