Easy set-up, low profile, vehicle mounted, in-motion tracking, satellite antenna
First Claim
11. A low profile satellite antenna system for mounting on a vehicle, comprising:
- a) two parabolic cylindrical reflectors mounted parallel to each other, each parabolic cylindrical reflector being coupled to a respective waveguide; and
b) means for combining signals from said respective waveguides, wherein said antenna system is adapted to receive signals in the wavelength of communication satellites.
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Accused Products
Abstract
A low profile, vehicle mounted, in-motion tracking, satellite antenna includes a pair of antenna assemblies mounted in parallel on a rotatable platform. Each antenna assembly includes two subreflectors with a plastic matching element. The outputs of the two antenna assemblies are coupled with a single phase shifter. The combined outputs are retransmitted to a receiver inside the vehicle. The satellite antenna also includes a receiver for receiving channel selection data and/or for providing two-way communication with equipment inside the vehicle. The antennae, transmitter and receiver are self-powered by a storage device which is charged by a wind driven generator. A retractable radome lowers to a lower profile when the antenna is not in use.
60 Citations
33 Claims
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11. A low profile satellite antenna system for mounting on a vehicle, comprising:
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a) two parabolic cylindrical reflectors mounted parallel to each other, each parabolic cylindrical reflector being coupled to a respective waveguide; and
b) means for combining signals from said respective waveguides, wherein said antenna system is adapted to receive signals in the wavelength of communication satellites. - View Dependent Claims (12, 13, 14, 15, 16, 17, 18, 19, 20)
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21. A satellite antenna system, comprising:
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a) a first reflector dish;
b) a second reflector dish arranged parallel to said first reflector dish; and
c) elevation aiming means coupled to said first and second reflector dishes for adjusting the elevation angle of said dishes relative to a first plane, said elevation aiming means including means for altering the position of one of said reflector dishes in a direction substantially perpendicular to said first plane. - View Dependent Claims (22, 23, 24, 25, 26, 27)
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28. A satellite antenna, comprising:
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a) a bifurcated reflector dish having a first reflector part and a second reflector part defining a first space therebetween;
b) a bifurcated subreflector having a first subreflector part and a second subreflector part defining a second space therebetween, wherein said first space and said second space are arranged such that satellite signals reflected by said reflector dish and said subreflector mix constructively with unreflected satellite signals passing through said first and second spaces. - View Dependent Claims (1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 30, 31, 32, 33)
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33-1. The antenna according to claim 28, further comprising:
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c) a retractable radome covering said antenna assembly; and
d) means for retracting said radome when said antenna assembly is not in use.
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Specification