发明名称 Aircraft engine run-up hangar
摘要 An aircraft engine run-up hangar (1) comprises a building defining a test chamber (3) capable of receiving an aircraft (2) therein, an air inlet structure, and an exhaust structure . The air inlet structure (6) is formed in a front end part of a roof structure (14) corresponding to a front end part (10) of the building (4), the exhaust structure (7) is connected to a rear end part of the building (4) and defines an exhaust passage extending obliquely upward from the back end of the building (4), and one or a plurality of current deflecting members are disposed near a lower end of the air inlet structure (6) to deflect air currents flowing through the air inlet structure (6) into the building (4) toward an aircraft (2) housed in the building (4). A current-straightening structure (18) is incorporated into the air inlet structure. A current-straightening space (19) is defined under the air inlet structure (6). A first current-straightening member (20), a second current-straightening member (22), a third current-straightening member (23) and a fourth current-straightening member (24) are disposed in a region in and around the current-straightening space. <IMAGE>
申请公布号 EP1249393(A2) 申请公布日期 2002.10.16
申请号 EP20020007942 申请日期 2002.04.09
申请人 KAWASAKI JUKOGYO KABUSHIKI KAISHA 发明人 SATOMI, TAKAYUKI;OGAWA, KAZUSHI;KASASHIMA, TAKASHI;YOSHIDA, HIDENORI;SAITO, YASUO;HIRAKAWA, HAJIME;AKIMOTO, KAZUYUKI
分类号 B64F1/26;B64F5/00;E04H6/44;(IPC1-7):B64F1/22 主分类号 B64F1/26
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