Ram Air Inlet Radar Absorbing Material

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Solution Overview

Problem

Conventional ram air inlets made of metal reflect electromagnetic energy from radar systems, degrading radar performance due to their positioning on aircraft pods.

Innovation Solution

A ram air inlet structure made of or coated with radar absorbing material, such as those sold by Arc Technologies, Inc., is disposed on a flange of the pod shell facing the radar field, extending toward or into the radar field to minimize reflections.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If conventional metal ram air inlets are used, then structural strength and durability are maintained, but radar signal reflection increases degrading radar performance

Engineering Contradiction:
Improveradar performanceVSAvoidradar signal reflection
Core Design Contradiction:
ReliabilityVSObject-generated harmful factors

Solution Approach 1:

The patent changes the material parameter of the ram air inlet from conventional metal to radar absorbing material (RAM), fundamentally altering the electromagnetic properties. This parameter change allows the inlet to absorb radar signals instead of reflecting them, resolving the contradiction between maintaining structural integrity and reducing radar reflection.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The patent employs composite materials by combining the structural function of the ram air inlet with the electromagnetic absorption properties of RAM. The inlet structure integrates both mechanical strength requirements and radar absorption capabilities through the use of composite or coated material systems.

Inventive Principle:
Principle #40Composite materials

2Reliability

If radar absorbing material is used for the ram air inlet, then radar signal reflection is reduced, but manufacturing complexity increases

Engineering Contradiction:
Improveradar performanceVSAvoidinlet structure fabrication
Core Design Contradiction:
ReliabilityVSEase of manufacture

Solution Approach 1:

The patent applies segmentation by separating the ram air inlet into distinct functional zones: the structural framework and the radar absorbing material layers. This allows each component to be manufactured and tested independently before assembly, simplifying the overall manufacturing process despite the introduction of RAM.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent uses intermediary materials such as adhesives, coatings, or bonding agents to attach the radar absorbing material to the inlet structure. These intermediaries facilitate the integration of RAM into existing manufacturing workflows without requiring complete redesign of the fabrication process.

Inventive Principle:
Principle #24Intermediary (Mediator)

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

The use of radar absorbing materials reduces radar signal returns, thereby improving radar quality and performance by minimizing the impact of the ram air inlet on the radar system.

Implementation Method 1

The use of radar absorbing materials reduces radar signal returns, thereby improving radar quality and performance by minimizing the impact of the ram air inlet on the radar system

Methodology Applied
Scientific EffectRadar absorbing material absorption: Absorption (EM radiation)

Data Source

PatentEP3539862B1Ram air inlets having radar absorbing material
Publication Date: 2022.05.04 GOODRICH CORP
  • EP3539862B1 patent drawingFigure 1~2

AI summary

An aircraft pod can include a pod shell (105) defining a window (107), a radar system (109) disposed within the shell and in optical communication with the window in the shell, and configured to send and/or receive radar signals away from the pod shell in a radar field of regard, and a ram air inlet structure (101) disposed on an outer surface of the shell in optical communication with the radar field of regard, wherein the ram air inlet structure is made of or coated with a radar absorbing material.