Aircraft scanning antenna system with inter-element isolators

Claim 2

An antenna system construction mounted in the wing of an airfoil comprising: a leading H-plane array of directional elements mounted in the leading edge of an aircraft wing, a trailing H-plane array of directional elements mounted in the trailing edge of the aircraft wing, a plurality of parasitic reflecting rods, said rods being interposed in spaced relation to said elements in each of said forward and said trailing H-plane arrays, said rods being dimensioned and spaced from said H-plane directional elements as to regulate the mutual coupling between elements of said H-plane arrays such that high interelement isolation is maintained throughout a broad angular sector, an E-plane array of directional elements mounted in the leading edge of the aircraft wing adjacent to said leading H-plane array, an E-plane array of directional elements mounted in the trailing edge of the aircraft wing adjacent to said trailing H-plane array, means for applying electrical signals to each of said arrays, and means for shifting the relative phase of said signals in response to a desired direction of scan.

Claim 3

An antenna system construction mounted in the wing of an airfoil comprising: an H-plane array of directional elements mounted in the leading edge of an aircraft wing, a pluality of parasitic reflecting rods, said rods being interposed in spaced relation to said elements in said H-plane array, said rods being dimensioned and spaced from said H-plane directional elements as to regulate the mutual coupling between elements of said H-plane array such that high inter-element isolation is maintained throughout a broad angular sector, an E-plane array of directional elements mounted in the leading edge of the aircraft wing adjacent to said H-plane array, means for applying electrical signals to each of said arrays, and means for shifting the relative phase of said signals in response to a desired direction of scan.

Claim 4

An antenna system construction mounted in the wing of an airfoil comprising: an H-plane array of directional elements mounted in the leading edge of an aircraft wing, a pluality of parasitic reflecting rods, said rods being interposed in spaced relation to said elements in said H-plane array, said rods being dimensioned and spaced from said H-plane directional elements as to regulate the mutual coupling between elements of said H-plane array such that high inter-element isolation is maintained throughout a broad angular sector, an E-plane array of directional elements mounted in the leading edge of the aircraft wing adjacent to said H-plane array, means for applying electrical signals to each of said arrays, and means for shifting the relative phase of said signals in response to a desired direction of scan.

Claim 5

An antenna system construction mounted in the wing of an airfoil comprising: an H-plane array of directional elements mounted in the trailing edge of an aircraft wing, a plurality of parasitic reflecting rods, said rods being interposed in spaced relation to said elements in said H-plane array, said rods being dimensioned and spaced from said H-plane directional elements as to regulate the mutual coupling between elements of said H-plane array such that high interelement isolation is maintained throughout a broad angular sector, an E-plane array of directional elements mounted in the trailing edge of the aircraft wing adjacent to said H-plane array, means for applying electrical signals to each of said arrays, and means for shifting the relative phase of said signals in response to a desired direction of scan.

Claim 6

An antenna system construction mounted in the wing of an airfoil comprising: an H-plane array of directional elements mounted in the trailing edge of an aircraft wing, a plurality of parasitic reflecting rods, said rods being interposed in spaced relation to said elements in said H-plane array, said rods being dimensioned and spaced from said H-plane directional elements as to regulate the mutual coupling between elements of said H-plane array such that high interelement isolation is maintained throughout a broad angular sector, an E-plane array of directional elements mounted in the trailing edge of the aircraft wing adjacent to said H-plane array, means for applying electrical signals to each of said arrays, and means for shifting the relative phase of said signals in response to a desired direction of scan.

Claim 7

The system as recited in claim 2 or 3 wherein said directional elements comprise a plurality of yagi end-fire elements, each of said end-fire elements, including an excitable driver, a plurality of parasitic directors and a common reflector, said reflectors and said driver being arranged in a longitudinally parallel manner in a common plane and spaced a predetermined distance from each other and from said common reflector.

Claim 8

The system as recited in claim 2 or 3 wherein said parasitic reflecting rods are offset from said common reflector a distance approximating that between said driver and said common reflector, said rods also being oriented parallel to said drivers.

Claim 9

The system as recited in claim 2 or 3 further including means for adjusting the length and spacial orientation of said rods as to control the phase and amplitude of said mutual coupling energy.

Claim 10

The system as recited in claim 2 or 3 wherein said drivers are hooked on their longitudinal ends.

Claim 11

The system as recited in claim 2 or 3 wherein said parasitic reflecting rods are positioned in the same vertical plane as said drivers.

Claim 12

The system as recited in claim 2 or 3 further including adjustable spacing means to permit the adjustment of the spacing between said common reflector and said parasitic reflecting rods.

Claim 13

The system as recited in claim 2 or 3 further including means for adjusting the length of said parasitic reflecting rods.

Claim 14

The system as recited in claim 2 or 3 wherein the length of said parasitic reflecting rods and the distance between said common reflector and said rods are adjustable to values which in the operation of said system regulate a scattering field in the vicinity of said rods, said field being variable in phase and amplitude in response to said length and distance adjustments as to increase inter-element isolation.

Claim 15

The system as recited in claim 2 or 3 further including means for adjusting the length of said rods and the spacing between said rods and said common reflector so as to regulate a scattering field at the antenna aperture, said field being variable in phase and amplitude as to increase isolation between said elements.

Claim 16

The system as recited in claim 2 or 3 further including means for adjusting the length of said rods and means for adjusting the spacing between said rods and said common reflector, said first and second means being adjustable in combination so as to create an electronic scattering field when said elements are excited, said scattering field serving to enhance inter-element isolation and to increase the angular sector scannable by said system.

Claim 17

The system as recited in claim 2 or 3 wherein said parasitic reflecting rods are electrically isolated from said elements.

Claim 18

An antenna system construction mounted in the wings of an airfoil comprising: a forward H-plane array of directional elements mounted in the forward edge of each wing, a trailing H-plane array of directional elements mounted in the trailing edge of each wing, a plurality of parasitic reflecting rods, said rods being interposed in spaced relation to said elements in each of said forward and said trailing H-plane arrays, a pair of forward E-plane arrays of directional elements mounted in the forward edge of each wing in spaced parallel relation on opposite sides of said forward H-plane arrays, a pair of trailing E-plane arrays of directional elements mounted in the trailing edge of each wing in spaced parallel relation on opposite sides of said trailing H-plane arrays, means for applying electrical signals to each of said arrays, means for shifting the relative phase of said signals in response to a desired direction of scan, and means for varying the length and spacial orientation of said rods as to regulate the mutual coupling energy between elements of said H-plane arrays such that high inter-element isolation is maintained throughout a broad angular scanning sector.

Claim 19

An antenna system construction mounted in the wings of an airfoil comprising: a forward H-plane array of directional elements mounted in the forward edge of each wing, a trailing H-plane array of directional elements mounted in the trailing edge of each wing, a plurality of parasitic reflecting rods, said rods being interposed in spaced relation to said elements in each of said forward and said trailing H-plane arrays, a pair of forward E-plane arrays of directional elements mounted in the forward edge of each wing in spaced parallel relation on opposite sides of said forward H-plane arrays, a pair of trailing E-plane arrays of directional elements mounted in the trailing edge of each wing in spaced parallel relation on opposite sides of said trailing H-plane arrays, means for applying electrical signals to each of said arrays, means for shifting the relative phase of said signals in response to a desired direction of scan, and means for varying the length and spacial orientation of said rods as to regulate the mutual coupling energy between elements of said H-plane arrays such that high inter-element isolation is maintained throughout a broad angular scanning sector.