发明名称 Aircraft engine run-up hangar
摘要 An aircraft engine run-up hangar comprises a building defining a test chamber capable of receiving an aircraft therein, an air inlet structure, and an exhaust structure. The air inlet structure is formed in a front end part of a roof structure corresponding to a front end part of the building. The exhaust structure is connected to a rear end part of the building and defines an exhaust passage extending obliquely upward from the back end of the building. A ceiling included in the building has an inclined section sloping down backward to straighten air currents, and a groove is formed in a middle part, with respect to width, of the inclined section to permit a vertical tail fin of an aircraft to pass when the aircraft is carried into or out of the test chamber.
申请公布号 US6560936(B2) 申请公布日期 2003.05.13
申请号 US20020114256 申请日期 2002.04.03
申请人 KAWASAKI JUKOGYO KABUSHIKI KAISHA 发明人 SATOMI TAKAYUKI;OGAWA KAZUSHI;KAWASHIMA TAKASHI;YOSHIDA HIDENORI;SAITO YASUO;HIRAKAWA HAJIME;AKIMOTO KAZUYUKI
分类号 B64F1/26;B64F5/00;E04H6/44;(IPC1-7):E01F9/00 主分类号 B64F1/26
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