发明名称 Turbojet for aircraft, aircraft equipped with such a turbojet, and method for mounting such a turbojet on an aircraft
摘要 The disclosed embodiments relates to a jet engine for an aircraft, characterized in that it bears at least one stabilizer, the stabilizer being fastened on the rigid structure of said jet engine so as to form a one-piece assembly. The jet engine can also bear one or more auxiliary devices required for the operation of the jet engine. The disclosed embodiments also relates to an aircraft provided with such a jet engine, and to a method of mounting such a jet engine on an aircraft.
申请公布号 US2009078819(A1) 申请公布日期 2009.03.26
申请号 US20060067748 申请日期 2006.09.05
申请人 AIRBUS FRANCE 发明人 GUERING BERNARD;TEULOU OLIVIER
分类号 B64D27/20;B64D27/16 主分类号 B64D27/20
代理机构 代理人
主权项
地址