发明名称 AIRCRAFT ENGINE RUN-UP HANGAR
摘要 PURPOSE: An aircraft engine run-up hangar is provided to have a building defining a test chamber and having a roof structure with an air inlet, to change air currents flowing toward an aircraft housed in the building through the air inlet, and to straighten the air currents flowing into the building, not needing an exhaust duct. CONSTITUTION: An aircraft engine run-up hangar(1) comprises a building(4) defining a test chamber(3) capable of receiving an aircraft; an air inlet structure(6); and an exhaust structure(7). The air inlet structure is formed in a front-end part of a roof structure(14) corresponding to a front-end part of the building. The exhaust structure is connected to a rear end part of the building and the exhaust structure defines an exhaust passage extending obliquely upward from the back end of the building. One or a plurality of current deflecting members are disposed near a lower end of the air inlet structure to deflect air currents flowing through the air inlet structure into the building toward an aircraft housed in the building.
申请公布号 KR20020079534(A) 申请公布日期 2002.10.19
申请号 KR20020019210 申请日期 2002.04.09
申请人 KAWASAKI JUKOGYO KABUSHIKI KAISHA 发明人 AKIMOTO KAZUYUKI;HIRAKAWA HAJIME;KAWASHIMA TAKASHI;OGAWA KAZUSHI;SAITO YASUO;SATOMI TAKAYUKI;YOSHIDA HIDENORI
分类号 B64F1/26;B64F5/00;E04H6/44;(IPC1-7):E04H6/44 主分类号 B64F1/26
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