发明名称 Integral antenna winglet
摘要 Disclosed is a winglet radome assembly, which can include at least one antenna assembly that can send and receive signals, such as radio waves. Some implementations of the winglet radome assembly can be secured to a wing of an aircraft, such as a fixed-wing aircraft. In addition, the winglet radome assembly can be configured to secure to a distal end of the wing and can be securely adapted to a variety of aircraft.
申请公布号 US9457886(B2) 申请公布日期 2016.10.04
申请号 US201314049085 申请日期 2013.10.08
申请人 SIERRA NEVADA CORPORATION 发明人 Hazen Timothy M.
分类号 H01Q1/28;B64C1/36;B64C23/06;H01Q1/48;B64C1/00;H01Q1/42 主分类号 H01Q1/28
代理机构 Mintz Levin Cohn Ferris Glovsky and Popeo, P.C. 代理人 Mintz Levin Cohn Ferris Glovsky and Popeo, P.C.
主权项 1. A winglet radome apparatus, comprising: an aerodynamic body configured to securely mate to a distal end of a wing of an aircraft, wherein the body comprises a leading edge, a trailing edge, a lower skin that extends between the leading edge and the trailing edge and defines a bottom surface of the body, and an upper skin that extends between the leading edge and the trailing edge and defines an upper surface of the body, and wherein the entire body is made entirely out of a material that allows uninterrupted transmission of a wireless signal through the material; an antenna assembly enclosed within the body and configured to at least one of send the wireless signal to or receive the wireless signal from at least one location outside the body, the antenna assembly including a grounding element that enables the antenna assembly to ground to at least the wing of the aircraft.
地址 Sparks NV US