Wideband DF Aperture Layout for Low-Drag Wide-Frequency Coverage

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Solution Overview

Problem

Traditional radar antenna systems require multiple apertures to cover large frequency bands, which increases weight and drag, limiting their range and suitability for missile and unmanned aircraft systems.

Innovation Solution

A single planar array with four or more antenna elements of varying sizes, configured in a specific pattern for wide frequency bandwidth signal reception, using correlative interferometry to resolve ambiguities and enable direction finding capabilities.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If multiple apertures are used to cover a wide frequency band, then the frequency coverage is improved, but the weight and drag increase, reducing the range

Engineering Contradiction:
Improvefrequency coverageVSAvoidantenna weight
Core Design Contradiction:
Adaptability or versatilityVSWeight of moving object

Solution Approach 1:

The patent combines multiple aperture functions into a single planar array by using antenna elements of varying sizes. The first antenna element is sized for lower frequencies while the second antenna element is smaller for higher frequencies, allowing one physical structure to perform what traditionally required multiple separate apertures.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

Different regions of the single planar array have different antenna element sizes tailored to specific frequency ranges. The first antenna element has a larger size optimized for lower frequencies, while the second antenna element has a smaller size optimized for higher frequencies, creating local specialization within a unified structure.

Inventive Principle:
Principle #3Local quality

2Adaptability or versatility

If multiple apertures are used to cover a wide frequency band, then the frequency coverage is improved, but the drag increases, reducing the range

Engineering Contradiction:
Improvefrequency coverageVSAvoiddrag
Core Design Contradiction:
Adaptability or versatilityVSObject-generated harmful factors

Solution Approach 1:

The patent merges multiple aperture functions into a single planar array structure, eliminating the need for multiple separate antenna assemblies. This consolidation reduces the overall physical footprint and aerodynamic profile, thereby reducing drag on missile and UAS platforms.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The single planar array is designed to perform multiple frequency coverage functions that traditionally required separate apertures. By making one structure universal across a wide frequency band through varying antenna element sizes, the system eliminates redundant structures that would increase drag.

Inventive Principle:
Principle #6Universality (Multi-functionality)

3Weight of moving object

If a single planar array with varying antenna element sizes is used, then the weight and form factor are reduced, but the direction finding performance across extreme wide band may be compromised

Engineering Contradiction:
Improveantenna weightVSAvoiddirection finding performance
Core Design Contradiction:
Weight of moving objectVSReliability

Solution Approach 1:

The patent applies local quality by having different antenna elements optimized for different frequency ranges within the single planar array. The first antenna element's larger size provides better performance at lower frequencies, while the second antenna element's smaller size maintains performance at higher frequencies, ensuring reliable direction finding across the entire extreme wide band.

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The patent changes the physical parameter of antenna element size to optimize performance across different frequency ranges. By varying the size parameter of different antenna elements within the single planar array, the system maintains reliable direction finding performance across the extreme wide frequency band while keeping the overall structure lightweight.

Inventive Principle:
Principle #35Parameter changes

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

This design provides a lightweight, compact antenna system capable of covering a wide frequency range with reduced ambiguities, allowing for confident direction finding and target tracking, while minimizing weight and drag, thus enhancing the range and performance of aerial vehicles.

Implementation Method 1

configured, with each of the antenna elements working in tandem, for a signal reception of a wide frequency bandwidth

Methodology Applied
Scientific EffectElectromagnetic radiation reception: Electromagnetic Induction

Data Source

PatentUS20220349989A1Low swap aperture for direction finding across extreme wide band
Publication Date: 2022.11.03 RAYTHEON CO
  • US20220349989A1 patent drawing
  • US20220349989A1 patent drawing
  • US20220349989A1 patent drawing

AI summary

A wideband direction finding (WBDF) aperture employs a limited number of extreme wideband end-fire antenna elements capable of covering a wide frequency bandwidth. Arranging variable sized antenna elements in a specific pattern, the WBDF aperture enables direction finding capability covering an extreme wide frequency band. The pattern arrangement of variable sized elements offers the signal discernment to limit ambiguities in signal angle of arrival. This small form factor design enables the WBDF aperture to be mounted on the surface of a missile, munition, or small UAS wing or fuselage. The WBDF aperture offers a combination of differing sized antenna elements arranged in a specific pattern, combined with direction finding and signal tracking to provide an unambiguous relative azimuth and elevation angle of the target.