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.
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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 |
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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