Invention Grant
- Patent Title: Global navigation satellite system antenna with a hollow core
- Patent Title (中): 全球导航卫星天线带有空心芯
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Application No.: US14772281Application Date: 2014-01-16
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Publication No.: US09520651B2Publication Date: 2016-12-13
- Inventor: Andrey Vitalievich Astakhov , Dmitry Vitalievich Tatarnikov , Pavel Petrovich Shamatulsky
- Applicant: LLC “Topcon Positioning Systems”
- Applicant Address: US CA Livermore
- Assignee: Topcon Positioning Systems, Inc.
- Current Assignee: Topcon Positioning Systems, Inc.
- Current Assignee Address: US CA Livermore
- Agency: Chiesa Shahinian & Giantomasi PC
- International Application: PCT/RU2014/000021 WO 20140116
- International Announcement: WO2015/108436 WO 20150723
- Main IPC: H01Q13/10
- IPC: H01Q13/10 ; H01Q1/48 ; H01Q9/04 ; H01Q21/30

Abstract:
Disclosed is a dual-band Global Navigation Satellite System antenna with a hollow core. The antenna includes a conductive cylindrical tube with a longitudinal axis. A ground plane, a low-frequency radiator, and a high-frequency radiator are annuli orthogonal to the longitudinal axis. The inner peripheries of the ground plane and the low-frequency radiator are electrically connected to the outer surface of the cylindrical tube. The outer periphery of the high-frequency radiator is electrically connected to the low-frequency radiator. A vertical low-frequency radiating gap is configured between the ground plane and the outer periphery of the low-frequency radiator. A horizontal high-frequency radiating gap is configured between the inner periphery of the high-frequency radiator and the outer surface of the cylindrical tube. In an embodiment, the inner diameter of the cylindrical tube has a value from about 27 mm to about 102 mm, permitting insertion of a post or pole.
Public/Granted literature
- US20160020521A1 Global Navigation Satellite System Antenna with a Hollow Core Public/Granted day:2016-01-21
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