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
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