Aircraft engine run-up hangar,申请号US20020114256-传众专利搜索

Aircraft engine run-up hangar

申请公布号：US2002144474(A1)

申请号：US20020114256

申请日期：2002.04.03

申请公布日期：2002.10.10

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):E04B1/82;E04D13/18;E04H14/00;E04F17/04;E04B2/02;F24F13/24

主分类号：B64F1/26

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.