|Table of Contents|

(PDF)

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]

Issue:
2009年06期
Page:
31-36
Research Field:
研究与设计
Publishing date:

Info

Title:
-
Author(s):
-
Keywords:
-
PACS:
V434
DOI:
-
Abstract:
In this paper，the principle and structures of a flow- regulator used for liquid rocket engines is introduced. The main problems in the development process are introduced in detail. Based on statistic mechanical analysis under the working condition of the regulator，the reasons are analyzed. The improved structures have been put forward and have been tested. The results of tests show that the reliability of the regulator has been improved after structures improvement

References:

[1]张贵田． 高压补燃液氧煤油发动机[M]． 北京: 国防工业出版社, 2005.
[2]格列克曼Б Ф. 液体火箭发动机自动调节[M]. 顾明初 译 北京: 宇航出版社, 1995.
[3]休泽尔D K. 液体火箭发动机现代工程设计[M]. 朱宁昌译. 北京: 宇航出版社, 1993.
[4]王昕. 流量调节器动态特性研究[J]. 火箭推进, 2004, 30(3): 19-23.
[5]赵双龙. 滑阀液动力的计算与分析[J]. 火箭推进, 2006, 32(3):18-23.

Memo

Memo:
-
Last Update: 1900-01-01