Patent GB-712265-A (GB)
Title: Improvements in or relating to aerials
Inventor: CARY REX HENRY JOHN
IPC: H01Q1/28
Filed: 1952-02-14
Abstract: 712,265. Aerial coupling arrangements ;aerials. NATIONAL RESEARCH DEVELOPMENT CORPORATION. Jan. 28. 1953 [Feb. 14, 1952], No. 3999/52. Classes 40 (5) and 40 (7) A base fed aerial has its distributed base capacity arranged to form part of a resonant transmission line which presents, at the feeder connection, an impedance high relative to the input impedance of the aerial. A wideband aerial, in the form of a triangular fin 1, Fig. 2. arranged above an earth plane 2 has the inner conductor 4 of the coaxial feeder 3 connected to the base 5 at the point 6. The ends B, F, of the base 5 are connected to the plane 2 by connections BC and FG and the space 13 contains dielectric material arranged so that the shortcircuited transmission lines formed by paths ABCD and EFGH are quarter-wavelength resonant lines at the mid-band frequency of the aerial 1, having a high impedance across the points AD and EH. When the member 1 is a quarter-wavelength high, the transmission line and aerial reactances mutually compensate over a band extending each side of the mid-band frequency. When a fin aerial 1, Fig. 5, is fixed in the conducting body 2 of an aircraft, a slot 13 is formed in the body 2, the space 13 containing dielectric material. When the feed point 6 is towards the front of fin 1 which is towards the rear end of the space 13, the aerial has a forward-looking polar diagram in a plane perpendicular to the fin, Fig. 5a. The opposite conditions produce a backward-looking polar diagram, Figs. 6 and 6a (not shown), while a double-lobed sideways-looking diagram is produced by a trapezoidal fin extending beyond each end of the space 13, Figs. 7 and 7a (not shown). An arrangement giving the twin-lobe polar diagram of Fig. 8a comprises a fin aerial 1, Fig. 8, fed at two points 6, 6a, one feed having a phase change introduced by device 14. Separate slots 13, in the body 2 are formed at each feed, and determine resonant transmission lines as previously described. An aerial 1a, Fig. 9, forming the tail-fin of an aircraft is fed at a point 6a, from the inner conductor 4a of a coaxial feeder 3a, a slot 13 a being formed in the base of the fin and containing dielectric material to give the resonant transmission lines each side of the feed point 6a. In one practical embodiment, for high-speed aircraft, a flanged dish member 15. Fig. 14, supports a fin aerial 19, the base of which is cut away to provide a space 21 containing a dielectric 29 such as polythene or polytetrafluorethylene and two end lugs secured to member 15 by screws 30 forming the shortcircuited ends of the two transmission lines. The centre of the base is connected to the conductor 22 of a coaxial terminal 23. The dielectric filling 29 protrudes above the member 15 to reach the outer surface of the aircraft. A heating element 26 in a hole 25 provides means for de-icing the aerial. In a modified form of fin 19, Fig. 15, the base is fastened at one end only by screw 30A and the feeder 22A is connected to the other end, the fin being confined to the right-hand half of the supporting dish member. A slot 31 on each side of the base of the fin provides a key for the dielectric material which is moulded round it.