发明名称 |
SECONDARY TAIL PIPE OF JET ENGINE |
摘要 |
PURPOSE: An auxiliary injection port of a jet engine is provided to reduce fuel consumption by improving the energy efficiency of a jet-propelled aircraft. CONSTITUTION: An auxiliary injection port of a jet engine is installed at the slightly rear of a main injection port through a main tail pipe(2) and multiple support units(4) of a jet engine(1). The auxiliary injection port maximizes energy efficiency by generating driving force two or more times through one time of injection. |
申请公布号 |
KR20110123319(A) |
申请公布日期 |
2011.11.15 |
申请号 |
KR20100042739 |
申请日期 |
2010.05.07 |
申请人 |
KYUNG, CHONG MAN |
发明人 |
KYUNG, CHONG MAN;GYEONG, WON SIK;KYUNG, HOON SIK;KEANG, YOON SIK;LIM, HYUN WOOK |
分类号 |
B64D27/16;B64D27/26;B64D33/04;B64D41/00 |
主分类号 |
B64D27/16 |
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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