The present invention relates to low-profile antennas, and more particularly to low-profile antennas with multi-band capabilities.
Vehicles are receiving an increasing number of wireless services, such as cellular phone service, satellite radio, terrestrial radio, and Global Positioning System (GPS) service. As additional wireless services become available, a vehicle must be equipped to accommodate the different types of signals. Multi-band antennas are widely used in vehicles. When designing multi-band antennas, designers focus on cost, aesthetics, and aerodynamics.
Conventional multi-band antennas have a single receiving element with a broad bandwidth and are designed to receive signals from all bands of interest. However, it is difficult to make a single receiving element receive multiple bands because each wireless service requires a different radiation pattern.
Other multi-band antennas have a single module that includes multiple antenna receiving elements. Each antenna element receives a different service at a given frequency. The signals received by each antenna element are sent to different receivers using separate cables. However, as the number of cables increases, the cost increases. Additionally, certain combinations of antenna receiving elements can cause interference.
In addition to cost, the overall dimensions of the antenna are important. A large number of antenna receiving elements increases the size of the antenna module. As the size increases, the aerodynamic drag increases, which may cause wind noise and/or reduce fuel economy.
A low-profile multi-band antenna module according to the present invention includes a first antenna that transmits first radio frequency (RF) signals in a first RF band. A second antenna transmits second RF signals in a second RF band. A first RF multiplexer combines the first and second RF signals for transmission. The first antenna, second antenna, and first RF multiplexer are arranged on a panel.
In other features, a transmission line has a first end that communicates with the first RF multiplexer and transmits the first and second RF signals. A second RF multiplexer communicates with a second end of the transmission line and separates the first and second RF signals. The first and second RF multiplexer implement out-of-band rejection to minimize interference between the first and second RF signals. The first RF signals are transmitted from the second RF multiplexer to a first transceiver and the second RF signals are transmitted from the second RF multiplexer to a second transceiver. At least one of the first antenna and the second antenna communicates with at least one amplifier. The transmission line supplies direct current (DC) power to at least one amplifier.
In still other features of the invention, the first and second antenna are arranged on the panel in an orientation that minimizes electrical interference between the first and second antenna. A combination of the first and second antenna minimizes interference between the first and second RF band. At least one of the first antenna and the second antenna radiates circular polarization and vertical polarization that is ideal for satellite radio communication. At least one of the first antenna and the second antenna radiates circular polarization that is ideal for global positioning system (GPS) satellite communication. At least one of the first antenna and the second antenna radiates vertical polarization that is ideal for terrestrial communication.
In yet other features, the first RF band is an industrial, scientific, and medicine (ISM) band, the second RF band is a satellite radio band, and the second antenna suppresses interference from the ISM band and is located adjacent to the first antenna. The first RF band is a personal communications services (PCS) band, the second RF band is a satellite radio band, and the second antenna suppresses interference from the PCS band and is located adjacent to the first antenna. The first RF band is a PCS band, the second RF band is a GPS band, and the first and second antenna are located at opposite ends of the panel to minimize coupling between the first and second antenna. The first RF band is a satellite radio band and the first antenna is located near a center of the panel. The first RF band is a first ISM band at a first frequency, the second RF band is a second ISM band at a second frequency, the first antenna is located adjacent to the second antenna, the first antenna suppresses interference from the second ISM band, and the second antenna suppresses interference from the first ISM band. The first RF band is a GPS band, the second RF band is an ISM band, and the first antenna suppresses interference from the ISM band and is located adjacent to said second antenna.
Further areas of applicability of the present invention will become apparent from the detailed description provided hereinafter. It should be understood that the detailed description and specific examples, while indicating the preferred embodiment of the invention, are intended for purposes of illustration only and are not intended to limit the scope of the invention.
The present invention will become more fully understood from the detailed description and the accompanying drawings, wherein:
The following description of the preferred embodiment(s) is merely exemplary in nature and is in no way intended to limit the invention, its application, or uses. For purposes of clarity, the same reference numbers will be used in the drawings to identify similar elements.
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The GPS band antenna 44 radiates circular polarization directed overhead. This enables the GPS band antenna 44 to communicate with satellites. The GPS band antenna 44 is preferably a dielectric-loaded patch antenna. The first ISM band antenna 46, the second ISM band antenna 48, and the PCS band antenna 52 radiate vertical polarization directed toward the horizon and no signal towards zenith. This radiation pattern is ideal for terrestrial communication and is similar to that of a monopole antenna. The first ISM band antenna 46, the second ISM band antenna 48, and the PCS band antenna 52 are preferably center-fed patch antennas, such as the antenna described in “Low-Profile Antenna”, U.S. Ser. No. 10/408,004 filed Apr. 4, 2003, which is hereby incorporated by reference in its entirety. Center-fed patch antennas are low-profile and preferably constructed using low-cost stamped sheet metal or printed circuit techniques. An important feature of the multi-band antenna module 42 is that it is low-profile. All of the antennas 44, 46, 48, 50, and 52 are less than six millimeters tall and are optimized to produce the radiation pattern for their required services.
The positioning of the antennas 44, 46, 48, 50, and 52 on the panel 54 is important because of interference and coupling between the antennas 44, 46, 48, 50, and 52. The PCS band antenna 52 and the GPS band antenna 44 are located at opposite ends of the panel 54 due to their high coupling. The satellite radio band antenna 50 is located in the center of the panel 54 due to its large size. The first ISM band antenna 46 is located adjacent to the second ISM band antenna 48 because a receiver for either antenna is typically designed to allow for interference from the other. The first ISM band antenna 46 and the second ISM band antenna 48 are located adjacent to the satellite radio band antenna 50. The satellite radio band antenna 50 has unique suppression capabilities in the ISM band at 2450 MHz and is narrow-band enough to suppress most of the radiation from the ISM band at 5800 MHz. The satellite radio band antenna 50 also suppresses radiation from and is located adjacent to the PCS band antenna 52. The first ISM band antenna 46 and the second ISM band antenna 48 do not receive significant interference from and are located adjacent to the GPS band antenna 44.
The positioning of the antennas 44, 46, 48, 50, and 52 on the panel 54 is also important because one or more of the antennas 44, 46, 48, 50, and 52 may contain built-in amplifiers. This is especially true for the satellite radio band antenna 50 and the GPS band antenna 44, which are receive-only antennas. The satellite radio band antenna 50 and the GPS band antenna 44 receive weak signals from distant satellites and typically include integrated low-noise amplifiers. The integrated low-noise amplifiers can easily be saturated and require the antennas 44, 46, 48, 50, and 52 to have low inter-element coupling. The input to low-noise amplifiers is often unfiltered and relies upon the inherent out-of-band rejection capabilities of the antenna. The amplified signal may need further filtering, so out-of-band signals are rarely a problem in the receiver system. Therefore, the signals from the antennas 44, 46, 48, 50, and 52 may be combined onto a single cable using an RF multiplexer.
A first RF multiplexer 56 is mounted on the bottom side of the panel 54 in
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Those skilled in the art can now appreciate from the foregoing description that the broad teachings of the present invention can be implemented in a variety of forms. Therefore, while this invention has been described in connection with particular examples thereof, the true scope of the invention should not be so limited since other modifications will become apparent to the skilled practitioner upon a study of the drawings, specification, and the following claims.