会员体验
专利管家(专利管理)
工作空间(专利管理)
风险监控(情报监控)
数据分析(专利分析)
侵权分析(诉讼无效)
联系我们
交流群
官方交流:
QQ群: 891211   
微信请扫码    >>>
现在联系顾问~
热词
    • 4. 发明申请
    • FUSELAGE OF AN AIRCRAFT OR SPACECRAFT AND METHOD OF ACTIVELY INSULATING SUCH A FUSELAGE
    • 飞机或空间的融合和活动绝缘方法
    • WO2008101986A1
    • 2008-08-28
    • PCT/EP2008/052120
    • 2008-02-21
    • AIRBUS DEUTSCHLAND GMBHJOERN, Paul
    • JOERN, Paul
    • B64C1/06B64D13/00
    • B64C1/067B64D13/00Y02T50/44Y02T50/46
    • The present invention relates to a fuselage (1) of an aircraft or spacecraft, with at least one shell element (2) and a structural element (7). An interspace (5; 9) to which air can be admitted by an air stream (10) is provided between the at least one shell element (2) and the structural element (7). The fuselage is distinguished by the fact that, to form the air-admitting air stream (10) as an outgoing/incoming air stream of a pressurized interior space (20) of the fuselage (1), the interspace (5; 9) is connected to a corresponding outgoing/ incoming air connection of the interior space (20). The invention also relates to a corresponding aircraft or spacecraft and to a method of actively insulating such a fuselage (1).
    • 本发明涉及一种具有至少一个壳体元件(2)和结构元件(7)的飞机或航天器的机身(1)。 在所述至少一个外壳元件(2)和所述结构元件(7)之间提供空气(5; 9),空气可由空气流(10)容纳的空间。 机身的特征在于,为了形成空气进入空气流(10)作为机身(1)的加压内部空间(20)的输出/进入空气流,空间(5; 9)是 连接到内部空间(20)的对应的输出/进入空气连接。 本发明还涉及相应的飞机或航天器以及主动地绝缘这种机身(1)的方法。