发明名称 |
SEMIFREE-JET TESTING APPARATUS |
摘要 |
PROBLEM TO BE SOLVED: To lower the back pressure of a supersonic nozzle and to enhance a starting property without making the capacity and the size of a pump or an exhauster large. SOLUTION: In this semifree-jet testing apparatus, a supersonic diffuser 6 is connected to the exit part 2b of a supersonic nozzle 2 which takes into a supersonic airflow, The extrance part 10a of a subsonic diffuser 10 is made to communicate with the exit part of the supersonic diffuser 6. A turbo-engine 11 is connected to the exit part 10b of the subsonic diffuser 10. A cowl external bypass part 14 is formed on the side of a cowl 7a which becomes the surface of the supersonic diffuser 6. A cowl external bypass part 15 which changes the opening area of the cowl external bypass part 14 is equipped at the part.
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申请公布号 |
JP2000230882(A) |
申请公布日期 |
2000.08.22 |
申请号 |
JP19990031216 |
申请日期 |
1999.02.09 |
申请人 |
ISHIKAWAJIMA HARIMA HEAVY IND CO LTD;NATL AEROSPACE LAB |
发明人 |
KOMI JUNSUKE;ITAHARA KANJI;YANAGI RYOJI |
分类号 |
G01M9/06;F01D25/00;F02C7/04;F02K9/96;G01M15/00;G01M15/14;(IPC1-7):G01M9/06 |
主分类号 |
G01M9/06 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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