Monolithic IRTRM Sintering for AESA RF Leakage Reduction

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

The existing methods for fabricating Active Electronically Scanned Arrays (AESAs) face challenges in aligning and mating radiator aperture plates with quad-pack transmit/receive modules, leading to RF leakage, mismatch losses, and increased manufacturing costs due to separate fabrication and subsequent alignment issues.

Innovation Solution

The method involves forming integrated radiator-transmit/receive modules (IRTRMs) using metalized ceramic material, with sintered monolithic structures that include RF waveguides and radiators, and coupling RF circuitry, allowing for simultaneous fabrication and alignment to prevent misalignments and air gaps, thereby reducing RF leakage and manufacturing costs.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of manufacture

If radiator aperture plates and quad-pack transmit/receive modules are fabricated separately and then aligned, then manufacturing flexibility is maintained, but manufacturing precision deteriorates due to alignment issues causing RF leakage and mismatch losses

Engineering Contradiction:
Improvemanufacturing flexibilityVSAvoidalignment precision
Core Design Contradiction:
Ease of manufactureVSManufacturing precision

Solution Approach 1:

The patent merges the radiator aperture plate and transmit/receive modules into a single integrated radiator-transmit/receive module (IRTRM) fabricated as one monolithic structure using HTCC material. This eliminates the separate fabrication and alignment steps, resolving the contradiction by combining two previously separate manufacturing processes into one unified process that achieves both ease of manufacture and high manufacturing precision simultaneously

Inventive Principle:
Principle #5Merging (Combining)

2Productivity

If radiator aperture plates are made smaller to facilitate denser spacing, then productivity improves by preventing grating lobes, but manufacturing precision deteriorates due to difficulty in maintaining alignment at smaller scales

Engineering Contradiction:
Improveradiating element spacing densityVSAvoidalignment precision
Core Design Contradiction:
ProductivityVSManufacturing precision

Solution Approach 1:

By integrating the radiator aperture plate with the transmit/receive modules into a monolithic IRTRM structure, the patent enables precise fabrication of smaller radiating elements with denser spacing. The single-step HTCC fabrication process maintains manufacturing precision even at reduced scales, allowing denser element spacing to prevent grating lobes without sacrificing alignment accuracy

Inventive Principle:
Principle #5Merging (Combining)

3Reliability

If Duroid material with dielectric constant of 4 is used for radiating elements, then reliability improves by achieving impedance matching with free space, but manufacturing precision deteriorates due to incompatibility with high temperature HTCC fabrication process

Engineering Contradiction:
Improveimpedance matching performanceVSAvoidfabrication compatibility
Core Design Contradiction:
ReliabilityVSEase of manufacture

Solution Approach 1:

The patent changes the dielectric material parameter from Duroid (dielectric constant of 4) to HTCC material (dielectric constant of 9-10). This parameter change enables compatibility with high temperature HTCC fabrication processes while maintaining reliable RF performance through the different dielectric properties of the HTCC material

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The patent uses HTCC material as a composite solution that integrates both structural and RF functional requirements. The HTCC material serves as both the substrate and dielectric filling material, combining mechanical support and electromagnetic performance in a single material system that is compatible with high temperature fabrication

Inventive Principle:
Principle #40Composite materials

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 approach results in improved RF performance, reduced manufacturing costs, and increased reliability by eliminating misalignments and air gaps, allowing for mass production of AESAs with factory-tuned and repeatable performance without additional post-manufacturing procedures.

Implementation Method 1

The method further comprises sintering the metalized ceramic material to create a monolithic structure

Methodology Applied
Scientific EffectSintering: Sintering

Data Source

PatentUS10854984B2Air-filled quad-ridge radiator for AESA applications
Publication Date: 2020.12.01 THE BOEING CO
  • US10854984B2 patent drawing
  • US10854984B2 patent drawing
  • US10854984B2 patent drawing

AI summary

A method of manufacturing an integrated radio frequency (RF) module, comprising structurally forming at least one RF waveguide and at least one RF radiator of a metalized ceramic material. The RF waveguide(s) and the RF radiator(s) are connected and operatively coupled with each other. Each of the RF radiator(s) comprises a metalized outer wall and at least one metalized axial ridge extending along an inner surface of the outer wall. The method further comprises sintering the metalized ceramic material to create a monolithic structure comprising the RF waveguide and RF radiator, and operatively coupling RF circuitry to the RF waveguide(s).