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Publication numberUS3192529 A
Publication typeGrant
Publication dateJun 29, 1965
Filing dateMar 20, 1961
Priority dateMar 20, 1961
Publication numberUS 3192529 A, US 3192529A, US-A-3192529, US3192529 A, US3192529A
InventorsChatelain Maurice G
Original AssigneeRyan Aeronautical Co
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Multi-helix antenna on inflatable satellite
US 3192529 A
Abstract  available in
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Claims  available in
Description  (OCR text may contain errors)

June 29, 1965 M. G. CHATELAIN MULTI-HELIX ANTENNA 0N INFLATABLE SATELLITE Filed March 20, 1961 INVENTOR.

MAURICE G. CHATELAI N BY Fig. 2

United States Patent 3,192,529 MULTI-HELIX ANTENNA N INFLATABLE SATELLITE Maurice G. Chatelain, San Diego, Calif., assignor to The Ryan Aeronautical Co., San Diego, Calif. Filed Mar. 20, 1961, Ser. No. 97,064 3 Claims. (Cl. 343844) The present invention relates generally to antennas and more particularly to a multi-helix antenna.

Various types of antennas have been used in space vehicles to direct or reflect radio frequency signals to ground based receivers, both rigid antennas mounted on an instrumented package and inflated, reflector type antennas. In order to be efiective at great distances, the reflective antenna must be of considerable size, the most practical configuration being a spherical balloon with a metallized surface, since this structure is light and can be packed in a small space and inflated after being placed in orbit. A spherical reflector is, however, of low efficiency due to the scattering of most of the incident energy and absence of directivity. It is desirable to construct an antenna of minimum weight, suitable for launching as a satellite vehicle, having means for control of directivity and being capable of reflecting a considerable portion of the incident energy.

The primary object of this invention, therefore, is to provide an inflatable antenna having a plurality of substantially radially directed elements each being in the form :of a conical helix and being effective over a wide range of frequencies.

Another object of this invention is to provide a multihelix antenna having means for interconnecting various elements individually or in groups to obtain the required directivity and beamwidth.

A further object of this invention is to provide a multihelix antenna constructed as an inflatable body of thin flexible material in generally spherical form and incorporating the conical elements integrally therewith, the spherical body portion being metallized and forming a ground plane for the elements.

Finally, it is an object to provide a multi-helix antenna of the aforementioned character which is simple and convenient to construct and which will give generally eflicient and durable service.

With these and other objects definitely in view, this invention consists in the novel construction, combination and arrangement of elements and portions, as will be hereinafter fully described in the specification, particularly pointed out in the claims, and illustrated in the drawing which forms a material part of this disclosure, and in which:

FIGURE 1 is a side elevation view of the antenna; and

FIGURE 2 is an enlarged, fragmentary sectional view taken on the line 2-2 of FIGURE 1.

Similar characters of reference indicate similar or identical elements and portions throughout the specification and throughout the views of the drawing.

The antenna comprises a substantially spherical body of thin, flexible material, such as plastic 12. Extending radially from the body 10 are a plurality of truncated cones 14, also of thin, flexible material. The cones 14 are preferably integral with the body 10 to be inflated as a unit therewith, but could be made individually inflatable to avoid collapse of the entire antenna from puncture of one cone. Various means have been devised for inflating ballon structures in space and need not be discussed in detail.

On each cone 14 is a helical antenna element 16, which is a metallic strip painted, vacuum deposited, or otherwise applied to the surface of the cone. The entire outer surhas.

face of the body 10 also has a metallic coating 18, which serves as a ground plane for the elements 16. The cones 14 are arranged in a suitable geometric pattern, the number of cones depending on the size of the antenna, the specific function and the degree of directivity required.

Radio frequency energyintercepted by the antenna will be reflected by the helical elements 16, the total reflected energy being considerably more than that obtainable from a plain sphere and with more directivity. To provide control of directivity, the elements 16 may be connected to a switching unit 20, as indicated diagrammatically in FIGURE 2, the switching unit being of mechanical, electronic, or any other suitable type. By interconnecting two elements 16, through the switching unit 20, a signal can be received from one direction and re-transmitted or reflected in another specific direction to a predetermined received location. Thus communications can be established between widely separated locations for which radio communication is otherwise diflicult due to the curvature of the earth obstructing ground transmission. For more precise directivity, the elements 16 may be connected in groups to reduce beamwidth, the phenomenon being well known.

The arrangement and action of the switching unit 20 will depend on the number of antenna elements, the degree of directivity required and various other factors, the design of a suitable unit being a simple matter for those skilled in the art. The switching action can be according to a predetermined program or selectively controlled by command signals, according to requirements.

The helical elements 16 can be single, as illustrated, or multifilar for greater directivity, with constant or variable width conductors, the radial length of each cone determining the directive characteristics and the apex angle determining the frequency bandwidth. The antenna is suitable for use as a passive reflector or may be used actively with self-contained or attached transmission means.

The operation of this invention will be clearly comprehended from a consideration of the foregoing description of the mechanical details thereof, taken in connection with the drawing and the above recited objects. It will be obvious that all said objects are amply achieved by this invention.

It is understood that minor variation from the form of the invention disclosed herein may be made without departure from the spirit and scope of the invention, and that the specification and drawing are to be considered as merely illustrative rather than limiting.

I claim:

1. An antenna, comprising:

an inflatable, substantially spherical body of thin, flexible material;

a plurality of radially extending antenna elements mounted in spaced relation on said body;

each of said elements consisting of a conical portion integral and inflatable with said body and having a helical conductor thereon.

2. An antenna, comprising:

an inflatable substantially spherical body of thin, flexible material;

a plurality of radially extending antenna elements mounted in spaced relation on said body;

each of said elements consisting of a conical portion integral and inflatable with said body and having a helical conductor thereon; said body having a conductive surface and constituting a ground plane for said elements.

3. An antenna according to claim 2 and including switch means connected to said elements and operable to interconnect selected elements.

(References on following page) Patented June 29, 1965 r '5 References Cited by theExaminer UNITED STATES PATENTS Wohl 343895 X Adcock et a1. 343--895 X Seyfang 343872 X Dyson 343--895 Harris 343-895 Haas 343-705 X Wheeler 343--895 Riblet 343895 4 3,063,048 11/62 Lehan et a1 343-895 X 3,098,229 7/63 Rahb 343705 OTHER REFERENCES 5 Airborne Spiral Antennas Minimize Drag by Philip Klass; Aviation Week, issue of July 14, 1958, pages 75, 77, 79, 81, 82.

Electronic Industries, March 1961, page 7.

1O HERMAN KARL SAALBACH, Primary Examiner.

GEORGE'N. WESTBY, ELI LIEBERMAN, Examiners.

Patent Citations
Cited PatentFiling datePublication dateApplicantTitle
US2575377 *Nov 13, 1945Nov 20, 1951Wohl Robert JShort wave antenna
US2630530 *Nov 15, 1949Mar 3, 1953Adcock Mack DonaldHelical antenna array
US2907875 *Sep 26, 1957Oct 6, 1959Seyfang Frank GEmergency radio transmitter
US2958081 *Jun 30, 1959Oct 25, 1960Univ IllinoisUnidirectional broadband antenna comprising modified balanced equiangular spiral
US2966679 *Nov 13, 1957Dec 27, 1960Harris Edward FUnloaded helical antenna
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US2990548 *Feb 26, 1959Jun 27, 1961Westinghouse Electric CorpSpiral antenna apparatus for electronic scanning and beam position control
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US3063048 *May 4, 1959Nov 6, 1962Space General CorpDiscovery and location system
US3098229 *Jun 17, 1959Jul 16, 1963Gen Mills IncTransmission line erected by pressurized plastic
Referenced by
Citing PatentFiling datePublication dateApplicantTitle
US3594802 *Sep 20, 1968Jul 20, 1971Bolkow GmbhOmnidirectional antenna having circumferentially spaced radiators with orthogonal polarization
US3683393 *Jul 6, 1970Aug 8, 1972Electrotec CorpHelical dipole antenna
US3690801 *Jul 10, 1970Sep 12, 1972Siempelkamp Gmbh & CoDischarge device for platen press
US4208097 *Sep 18, 1978Jun 17, 1980The Kemmerer Coal CompanyReflecting target for electronic distance measuring
US4267217 *Sep 19, 1979May 12, 1981Brooker Bernard FBall
US4357375 *Sep 30, 1980Nov 2, 1982Atkinson Jr Hugh HVacuum ball insulation
US4792808 *Dec 14, 1982Dec 20, 1988Harris Corp.Ellipsoid distribution of antenna array elements for obtaining hemispheric coverage
US5570102 *Dec 29, 1995Oct 29, 1996Nissan Motor Co., Ltd.Energy receiving satellite
US20070057845 *Oct 26, 2004Mar 15, 2007Toshio MiuraDirectional antenna device
WO1994029925A1 *May 24, 1994Dec 22, 1994The United States Of America, Represented By The Secretary Of The ArmyAntennas using novel ceramic ferroelectric materials
Classifications
U.S. Classification343/844, 428/11, D14/233, 343/708, 343/895, 343/915
International ClassificationB64G1/22, H01Q1/08
Cooperative ClassificationH01Q1/082, B64G1/22
European ClassificationB64G1/22, H01Q1/08B1