Multi-filar helix antennae

Details Multi-filar helix antennae Multi-filar helix antennae

1998-11-17

2001-05-15

Le, Hoanganh (Department: 2821)

Communications: radio wave antennas

Antennas

Spiral or helical type

C343S702000

Reexamination Certificate

active

06232929

ABSTRACT:

FIELD OF THE INVENTION
The present invention relates to multi-filar helix antennae and in particular, though not necessarily, to quadrifilar helix antennae.
BACKGROUND OF THE INVENTION
A number of satellite communication systems are today in operation which allow users to communicate via satellite using only portable communication devices. These include the Global Positioning System (GPS) which provides positional and navigational information to earth stations, and telephone systems such as INMARSAT (TM). Demand for this type of personal communication via satellite (S-PCN) is expected to grow significantly in the near future.
One area which is of major importance is the development of a suitable antenna which can communicate bi-directionally with a relatively remote orbiting satellite with a satisfactory signal to noise ratio. Work in this area has tended to concentrate on the quadrifilar helix (QFH) antenna (K. Fujimoto and J. K. James, “Mobile Antenna Systems Handbook”, Norwood, 1994, Artech House), pp. 455, 457. As is illustrated in
FIG. 1
, the QFH antenna
1
comprises four regular and identical inter-wound resonant helical elements
2
a
to
2
d,
centered on a common axis A and physically offset from one another by 90°. In reception mode, signals received from the four helical elements are phase shifted by 0°, 90°, 180°, and 270° respectively prior to combining them in the RF receiving unit of the mobile device. Similarly, in transmission mode, the signal to be transmitted is split into four components, having relative phase shifts of 0°, 90°, 180°, and 270° respectively, which are then applied to the helical elements
2
a
to
2
d.
The QFH antenna has proved suitable for satellite communication for three main reasons. Firstly it is relatively compact (compared to other useable antennae), a property which is essential if it is to be used in a portable device. Secondly, the QFH antenna is able to transmit and receive circularly polarised signals so that rotation of the direction of polarisation (due to for example to movement of the satellite) does not significantly affect the signal energy available to the antenna. Thirdly, it has a spatial gain pattern (in both transmission and reception modes) with a main forward lobe which extends over a generally hemispherical region. This gain pattern is illustrated in
FIG. 2
for the antenna of
FIG. 1
, at an operating frequency of 1.7 GHz. Thus, the QFH antenna is well suited for communicating with satellites which are located in the hemispherical region above the head of the user.
A problem with the QFH antenna however remains it's large size. If this can be reduced, then the market for mobile satellite communications devices is likely to be increased considerably. One way to reduce the length of a QFH antenna for a given frequency band is to reduce the pitch of the helical elements. However, this tends to increase the horizontal gain of the antenna at the expense of the vertical gain, shifting the gain pattern further from the ideal hemisphere. Another way to reduce the length of the antenna is to form the helical elements around a solid dielectric core. However, this not only increases the weight of the antenna, it introduces losses which reduce the antenna gain.
SUMMARY OF THE INVENTION
It is an object of the present invention to improve the design flexibility of multi-filar helix antennae to allow gain patterns to be tailored for particular applications. It is also an object of the present invention to reduce the length of QFH antennae used for satellite communication.
According to a first aspect of the present invention there is provided a multi-filar helix antenna having a plurality of inter-wound helical antenna elements, each helical element being defined by an axial coefficient z, a radial coefficient r, and an angular coefficient &thgr;, wherein d&thgr;/dz for at least one of the helices is non-linear with respect to the axial coefficient z.
The present invention introduces into the design of multi-filar helix antennae a variable which has not previously been applied. By carefully introducing non-linear changes into the structure of a helical element of the multi-filar helix antenna, the spatial gain pattern of the antenna may be optimised. Moreover, the axial length of the antenna may be reduced.
Preferably, d&thgr;/dz for all of the helical elements is non-linear with respect to the axial coefficient z. More preferably, d&thgr;/dz varies, with respect to z, substantially identically for all of the helical elements.
Preferably, d&thgr;/dz for said at least one helical element varies periodically. More preferably, the period of this variation is an integer fraction of one turn length of the helical element. Alternatively, the period may be an integer multiple of the turn length.
Preferably, the axial coefficient z is a sinusoidal function of the angular coefficient &thgr;, i.e. z=k
0
&thgr;+ƒ sin(k
1
&thgr;) where k
0
and k
1
are constants. The axial coefficient z may be a sum of multiple sinusoidal functions of the angular coefficient, i.e. z=k
0
&thgr;+ƒ
1
sin(k
1
&thgr;)+ . . . +ƒ
n
sin(k
n
&thgr;). The functions ƒ may be multiplying constants.
Preferably, the radial coefficient r is constant with respect to the axial coefficient z for all of the helical elements. The helical elements may be provided around the periphery of a cylindrical core. Alternatively, r may vary with respect to z. For example, r may vary linearly with respect to z for one or more of the helical elements, e.g. by providing the or each helical element around the periphery of a frusto-cone. In either case, the core may be solid, but is preferably hollow in order to reduce the weight of the antenna. A hollow core may comprise a coiled sheet of dielectric material. The helical elements may be metal wire strands wound around the core, metal tracks formed by etching or growth, or have any other suitable structure. The properties of the antenna may be adjusted by forming throughholes in the core or by otherwise modifying the dielectric properties of the core.
Preferably, the multi-filar helix antenna is a quadrifilar helix antenna, having four helical antenna elements. The antenna elements are preferably spaced at 90° intervals although other spacings may be selected. Non-linearity may be introduced into one or more of the helical elements in order to improve the approximation of the main frontal lobe of the antenna gain pattern to a hemisphere, and to reduce back lobes of the gain pattern, or to tailor the gain pattern to any other desired shape. The invention applies also to other multi-filar antennae such as bi-filar antennae.
Multi-filar antennae embodying the present invention may be arranged in use to be either back-fired or end-fired by appropriate phasing of the helical elements.
According to a second aspect of the present invention there is provided a mobile communication device comprising a multi-filar antenna according to the above first aspect of the present invention. The device is preferably arranged to communicate with a satellite. More preferably, the device is a satellite telephone.
According to a third aspect of the present invention there is provided a method of manufacturing a multi-filar helical antenna having a plurality of helical antenna elements, the method comprising the steps of:
forming a plurality of elongate conducting antenna elements on a surface of a substantially planar dielectric sheet, at least one of said elements being non-linear; and
subsequently coiling said sheet into a cylinder with said antenna elements being on the outer surface of the cylinder.


REFERENCES:
patent: 4148030 (1979-04-01), Foldes
patent: 4998078 (1991-03-01), Hulkko
patent: 5134422 (1992-07-01), Auriol
patent: 5276920 (1994-01-01), Kuisma
patent: 5341149 (1994-08-01), Valimaa et al.
patent: 5489916 (1996-02-01), Waterman et al.
patent: 5561439 (1996-10-01), Moilanen
patent: 5581268 (1996-12-01), Hirshfield
patent: 5627550 (1997-05-01), Sanad
patent: 5657028 (1997-08-01), San

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