发明名称 Supersonic high altitude flight simulator for air driven generators
摘要 Apparatus to simulate supersonic high altitude flight for air driven electrical generators. First and second air-tight chambers are provided, as are means for evacuating the chambers to a preselected pressure. The air driven generator has both air inlet means and air outlet means. The air inlet means of the air driven generator is in fluid communication with the second air-tight chamber, and the air outlet means of the air driven generator is in fluid communication with the first air-tight chamber. Adjustable orifice means are provided. Valve controlled air inlet means for allowing air to enter the second air-tight chamber through the adjustable orifice means are also provided.
申请公布号 US4581999(A) 申请公布日期 1986.04.15
申请号 US19840599379 申请日期 1984.04.12
申请人 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE ARMY 发明人 CAMPAGNUOLO, CARL J.;LEE, HENRY C.
分类号 F03D9/00;F42C21/00;(IPC1-7):F42C21/00 主分类号 F03D9/00
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