发明名称 Improvements relating to compression nozzles for gas flow at supersonic speeds
摘要 <p>665,333. Jet propulsion plant. AKTIEBOLAGET BOFORS. Sept. 9, 1949 [Sept. 11, 1948], No. 23350/49. Class 110(iii) A compression nozzle forming the inlet of an athodyd or ram jet consisting of an inner gas deflecting body 1 projecting through a jacket 2 and so arranged that the space between the jacket and the body decreases toward the inlet edge of the jacket has an attachment jacket 4 fitted in front of and spaced from the jacket 2. The attachment jacket is so shaped that the air resistance is a minimum and is spaced from the outer part so as to minimise the disturbance to gas flow within the jacket. The diameter of the inlet edge of the jacket 4 should be approximately equal to the diameter of the inlet edge of the jacket 2 and the maximum external diameter is slightly smaller than the maximum external diameter of the jacket 2. Arrangements in which the nozzles are rectangular and not annular are described.</p>
申请公布号 GB665333(A) 申请公布日期 1952.01.23
申请号 GB19490023350 申请日期 1949.09.09
申请人 AKTIEBOLAGET BOFORS 发明人
分类号 F02C7/04;F02K7/10 主分类号 F02C7/04
代理机构 代理人
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