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
    • 8. 发明申请
    • AIRCRAFT CONFIGURATION
    • 飞机配置
    • US20070176047A1
    • 2007-08-02
    • US11307271
    • 2006-01-30
    • Matthew MooreKelly BorenEdward Marques
    • Matthew MooreKelly BorenEdward Marques
    • B64D27/00
    • B64D27/20B64C5/08B64C39/12
    • An aircraft configuration that may reduce the level of noise, infrared radiation, sonic boom, or combination thereof directed towards the ground from an aircraft in flight. In accordance with an embodiment of the present invention, an aircraft includes a tubular fuselage, two delta wings, at least one engine mounted to the aircraft and higher than the wings, and vertical stabilizers mounted on each wing outboard of the outermost engine. Each wing may include a wing strake at the leading edge of the wing and extending to the fuselage and an aft deck. The leading edge of the wing may extend forward of the intake of the engine, and the trailing edge of the aft deck may extend aft of the engine exhaust. The aft deck may include an upwardly rotatable pitch control surface at the trailing edge of the deck.
    • 一种飞行器配置,其可以降低来自飞行中的飞行器的噪声,红外辐射,声波起重臂或其组合的指向地面的水平。 根据本发明的实施例,飞行器包括管状机身,两个三角翼,至少一个安装在飞行器上并且高于翼的发动机,以及安装在最外侧发动机的每个翼外侧的垂直稳定器。 每个机翼可以在翼的前缘处包括翼片,并延伸到机身和后甲板上。 机翼的前缘可能会延伸到发动机进气口的前方,后甲板的后缘可能会延伸到发动机排气后面。 后甲板可以包括在甲板的后缘处的可向上旋转的俯仰控制表面。