Original document(24 pages) Authorized document(13 pages) 中文版
    This invention is a electronic and electrically operated sitting module pressure regulator, suitable for army craft. It provides a new adjusting method to solve the various problems of high-speeding fighter craft regulator. For example, the problem of the contradictions between the height flying range and the restriction of the rate of change of module pressue; between the high speeding rotating of ralve required by high-speed take off and landing and the stability of module pressure control, and also solves the problem of using big value adjusting proportion at meet the air-feed charging reguirement in fighter craft. This regulator is also applicable for ordinary plane.
Application Number
申请号
85107740 Application Date
申请日
1985.10.19
Title 名称 Electric and electrically operated sitting module pressure regulator and its adjusting method
Publication Number
公开号
1010570 Publication Date
公开日
1987.04.22
Approval Pub. Date Granted Pub. Date 1991.06.05
International Classification 分类号 B64D13/04
Applicant(s) Name
申请人
Nanjing Aviation College
Address 地址 210016
Inventor(s) Name 发明人 Lin Yucai
Attorney & Agent 代理人
More information 更  多  信  息


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