发明名称 |
EXHAUST NOZZLE AND EXHAUST CHANNEL VARIABLE METHOD |
摘要 |
<p>PROBLEM TO BE SOLVED: To provide an exhaust nozzle that reduces noises by using a lightweight simple mechanism without the complication and upsizing of an exhaust nozzle structure and that increases efficiency during supersonic cruise, and an exhaust channel variable method.SOLUTION: A main nozzle piece 110 of an exhaust nozzle 100 is provided in such a manner that a back end side can swing inward and outward directions of an exhaust channel 101 centering on an opening/closing bent part 111 in the rear of an engine. A connecting nozzle piece 120 is connected to the adjacent main nozzle pieces 110 on both sides in a bendable manner. When the main nozzle piece 110 swings in the inward direction of the exhaust channel 101, the connecting nozzle piece 120 forms a protrusion 102 within the exhaust channel 101.</p> |
申请公布号 |
JP2015038339(A) |
申请公布日期 |
2015.02.26 |
申请号 |
JP20130169712 |
申请日期 |
2013.08.19 |
申请人 |
JAPAN AEROSPACE EXPLORATION AGENCY |
发明人 |
AKATSUKA JUNICHI;WATANABE YASUSHI |
分类号 |
F02K1/48;F02K1/12 |
主分类号 |
F02K1/48 |
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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