Gridless RF Detection Surface for Hypervelocity Impact Location

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Solution Overview

Problem

Existing methods for detecting hypervelocity impacts, such as those from ballistic missile intercepts or micrometeoroids, face challenges due to the transitory nature of high-frequency signals and the need for extensive sensor networks, leading to large, power-intensive data acquisition systems that are impractical for operational vehicles or structures.

Innovation Solution

A gridless detection surface utilizing RF emissions and Time Of Arrival (TOA) measurements with multiple sensors to determine precise impact locations, employing an electronically conductive surface with an inner conductor layer between dielectric layers and conductive ground planes, allowing for efficient detection and processing of RF pulses generated by hypervelocity impacts.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If a grid-based detection system with wire mesh is used to detect impact points, then impact location can be determined by detecting wire breaks, but the system requires extensive sensor networks and large data acquisition electronics leading to increased size, complexity, and power consumption

Engineering Contradiction:
Improveimpact location determinationVSAvoidsensor network and data acquisition system
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The patent extracts only the essential function of impact detection from the complex grid-based system. Instead of using a wire mesh grid that requires breaking detection, the invention uses a gridless detection surface with RF emissions that can be detected without physical disruption to the surface structure. This eliminates the need for extensive sensor networks while maintaining impact location determination capability.

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The patent replaces the mechanical wire break detection system with an electromagnetic RF emission-based detection system. The detection surface generates RF emissions that are modulated by hypervelocity impacts, allowing electronic detection without mechanical contact or physical disruption. This substitution eliminates the need for physical sensor networks and reduces data acquisition complexity.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

2Reliability

If high-speed data acquisition electronics are used to capture transient impact signals, then impact detection capability is improved, but power consumption increases significantly

Engineering Contradiction:
Improveimpact detection capabilityVSAvoidpower consumption of data acquisition system
Core Design Contradiction:
ReliabilityVSUse of energy by moving object

Solution Approach 1:

The patent employs periodic RF emissions from the detection surface that are continuously present but only modulated during impact events. This allows the system to maintain detection readiness without continuously operating high-power data acquisition electronics at full speed. The RF emissions provide a continuous reference that can be processed at lower power levels, with high-speed acquisition only activated when impacts occur.

Inventive Principle:
Principle #19Periodic action

Solution Approach 2:

The patent changes the detection parameter from direct high-speed signal capture to RF emission frequency analysis. By detecting impacts through changes in RF emission frequency rather than direct high-speed voltage sampling, the system achieves reliable impact detection with significantly reduced power consumption. The RF modulation approach allows for energy-efficient signal processing while maintaining detection reliability.

Inventive Principle:
Principle #35Parameter changes

3Measurement precision

If multiple sensors are distributed throughout the structure to monitor for transient signals, then damage detection accuracy is improved, but the size and complexity of the system increases

Engineering Contradiction:
Improvedamage detection accuracyVSAvoidsystem mass
Core Design Contradiction:
Measurement precisionVSWeight of moving object

Solution Approach 1:

The patent makes the detection surface itself universal by integrating multiple functions into a single structure. The gridless detection surface simultaneously serves as the structural component and the sensing element, eliminating the need for separate sensor networks. The RF emission capability is embedded in the detection surface material, allowing it to function as both structure and sensor without adding mass.

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

Solution Approach 2:

The patent introduces RF emissions as an intermediary between the impact event and the detection system. Instead of requiring direct contact with multiple physical sensors, the RF emissions serve as a mediator that carries impact information across the detection surface. This intermediary approach allows for distributed detection without the need for physical sensor networks, reducing overall system mass.

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

This approach significantly reduces size, cost, and power consumption while achieving precise impact location determination with commercially available electronics, overcoming the limitations of traditional grid-based systems.

Implementation Method 1

utilizes multiple sensors that directly measure RF emissions generated by hypervelocity impacts

Methodology Applied
Scientific EffectElectromagnetic radiation: Electromagnetic Induction

Implementation Method 2

Time Of Arrival (TOA) position measurements for determining the precise impact location

Methodology Applied
Scientific EffectTime of arrival measurement: Time of Flight

Data Source

PatentUS8307694B1Hypervelocity impact detection method and system for determining impact location in a detection surface
Publication Date: 2012.11.13 INVOCON INC
  • US8307694B1 patent drawing
  • US8307694B1 patent drawing
  • US8307694B1 patent drawing

AI summary

A hypervelocity impact detection method and system for determining the precise impact location in a detection surface, of impacts such as ballistic missile intercepts, micrometeoroids and orbital debris (MMOD) or other shock events, utilizes a gridless detection surface capable of propagating radio frequency (RF) impact detection signals responsive to receiving hypervelocity impacts from objects, and multiple sensors on the detection surface that directly measure radio frequency RF emissions generated by the hypervelocity impacts on the surface, and a time of arrival (TOA) position measurement technique for determining the precise impact location in the detection surface.