US2298880A - Rotation symmetric reflector - Google Patents

Rotation symmetric reflector Download PDF

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Publication number
US2298880A
US2298880A US369441A US36944140A US2298880A US 2298880 A US2298880 A US 2298880A US 369441 A US369441 A US 369441A US 36944140 A US36944140 A US 36944140A US 2298880 A US2298880 A US 2298880A
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reflecting surface
reflector
lobes
support member
stray
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US369441A
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Gartenmeister Walter
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    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q15/00Devices for reflection, refraction, diffraction or polarisation of waves radiated from an antenna, e.g. quasi-optical devices
    • H01Q15/14Reflecting surfaces; Equivalent structures
    • H01Q15/16Reflecting surfaces; Equivalent structures curved in two dimensions, e.g. paraboloidal

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  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Aerials With Secondary Devices (AREA)

Description

Oct. 13, 1942. i GARTENMESTER 2,298,880
ROTATION SYMMETRIC REFLECTOR Filed Dec. 10, 1940 INVENTORY WALTER EARTH/M5575? BY hg wuu,
ATTORNEY Patented Oct. 13., 1942 I ROTATION SYMMETRIC REFLECTOR Walter Gartenmeister, Bergfeld, Germany; vested in the Alien Property Custodian Application December 10, 1940, Serial No. 369,441 In Germany March 16,1939
6 Claims.
Now, ways and means are demanded in practice which in a simple manner will insure a change in the focal length with a View to obviating these undesired lobes or ears as far as feasible.
The reflector presenting rotational symmetry of the invention satisfies this requirement by providing a supporting construction for the reflector which comprises two or more coaxial rings I and radial struts or braces inter-connecting the various rings and being of variable length. The coaxial rings, for instance, could consist of tubular rings. The effective reflecting surface or area is then placed into the supporting means adjustable as stated and secured and held therein by ways and means known in the prior art.
An exemplified embodiment of the basic idea of the invention is illustrated by way of example in Figs. 1 and 2. Fig. l is a sectional view of the rotation symmetric reflector of the invention, while Fig. 2 is an elevation thereof. In the exemplified embodiment here shown, only two tubular rings a and b are provided for the sake of simplicity. The radial connector struts or braces are indicated at c. For the purpose of changing the length, struts c are bipartite, the two constituent parts being connected with each other and guided inside each other by bolts and keyways. The latter serve to alter the length of the braces. To change the focal distance of the reflector surfaces h to be placed in this supporting structure, all that is necessary is to change the spacing between the two rings a and b. In order that the devices f mounted in the posterior part of the supporting means and the supporting or bearing means g for the rotary parabola structure may be adjustable at the same time to the desired extent, intermediary means 6 are provided which are designed to compensate for such changes in the distance as may otherwise occur in position.
Where such changes in focal length are frequent and where it is thus desirable to avoid substitution or replacement of the reflecting surface h, it will be expedient to make the reflecting surface it of a wire grate construction of such a nature that it will partake of the change in form occasioned upon a variation of the distances of the various co-axially disposed annuli.
While the basic idea of the invention has been hereinbefore described as applied to a reflector designed for the transmission or reception of electromagnetic oscillations of ultra-short wavelength, the same idea will be found useful similarly in connection with all reflector arrangements of this kind which are designed to insure focusing of any mechanical or electrical oscillations at all, no matter of what wave-length.
What is claimed is:
1. An electro-magnetic reflector subjected to undesirable secondary stray lobes in the normal operation thereof comprising a curved electromagnetic reflecting surface, a first annular support member located adjacent the outside of said reflecting surface, a second annular support member coaxially arranged with respect to said first support member, and means interposed between said support members for adjusting the curvature of said reflecting surface to prevent occurrence of said undesirable stray lobes.
2. An electro-magnetic reflector subjected to undesirable secondary stray lobes in the normal operation thereof, comprising a curved electromagnetic reflecting surface, a first annular support member located adjacent the outside of said reflecting surface, a second annular support member coaxially arranged with respect to said first support member, and means including a plurality of radially mounted braces interposed between said support members for adjusting the curvature of said reflecting surface to prevent occurrence of said undesirable stray lobes.
3. An electro-magnetic reflector subjected to undesirable secondary stray lobes in the normal operation thereof, comprising a curved electromagnetic reflecting surface, means for changing the focal length of said reflecting surface including a plurality of coaxial rings, and a plurality of radially mounted braces having adjusting means for adjusting the curvature of said reflecting surface to prevent occurrence of said undesirable stray lobes.
4. An electro-magnetic reflector subjected to undesirable secondary stray lobes in the normal operation thereof, comprising a curved electromagnetic reflecting surface, means for changing the focal length of said reflecting surface including a plurality of coaxial rings of variable length, and a plurality of radially mounted braces having adjusting means for adjusting the curvature of said reflecting surface to prevent occurrence of said undesirable stray lobes.
5. An electro-magnetic reflector subjected to undesirable secondary stray lobes in the normal operation thereof, comprising a curved electromagnetic reflecting surface, a first annular support member located adjacent the outside of said reflecting surface, a second annular support member coaxially arranged with respect to said first support member, means including a plurality of radially mounted braces interposed be tween said support members for adjusting the curvature of said reflecting surface, and intermediary means for supporting a box-like member located in the rear of said reflecting surface to prevent occurrence of said undesirable stray lobes.
6. An electro-magnetic reflector subjected to undesirable secondary stray lobes in the normal operation thereof, comprising a curved electromagnetic reflecting surface of Wire grate construction, a first annular support member located adjacent the outside of said reflecting 'sur-" face, a second annular support member coaxially arranged with respect to said first support member, a plurality of radially mounted braces, said braces having a plurality of slots with binding means for adjusting the distance between said support members to change the curvature of said reflecting surface to prevent occurrence of said undesirable stray lobes.
WALTER GARTENMEISTER.
US369441A 1939-03-16 1940-12-10 Rotation symmetric reflector Expired - Lifetime US2298880A (en)

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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2572430A (en) * 1946-05-17 1951-10-23 Breeze Corp Antenna structure
US2985881A (en) * 1958-12-05 1961-05-23 Holland Herman A reflector utilizing pre-stressed elements
US3153789A (en) * 1957-06-07 1964-10-20 Edward L Ashton Large aperture steerable trunnionmounted paraboloidal antenna
US4506271A (en) * 1982-09-27 1985-03-19 Gonzalez Brian L Portable antenna with wedge-shaped reflective panels
US4598297A (en) * 1983-10-21 1986-07-01 Hawkins Joel W Mounting apparatus for satellite dish antennas
US8890757B1 (en) * 2009-07-31 2014-11-18 Trivec-Avant Corporation Antenna system for satellite communication

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2572430A (en) * 1946-05-17 1951-10-23 Breeze Corp Antenna structure
US3153789A (en) * 1957-06-07 1964-10-20 Edward L Ashton Large aperture steerable trunnionmounted paraboloidal antenna
US2985881A (en) * 1958-12-05 1961-05-23 Holland Herman A reflector utilizing pre-stressed elements
US4506271A (en) * 1982-09-27 1985-03-19 Gonzalez Brian L Portable antenna with wedge-shaped reflective panels
US4598297A (en) * 1983-10-21 1986-07-01 Hawkins Joel W Mounting apparatus for satellite dish antennas
US8890757B1 (en) * 2009-07-31 2014-11-18 Trivec-Avant Corporation Antenna system for satellite communication

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