High-Temperature RF Smart Node With Thermal Component Segmentation
Find Innovative SolutionsGenerate Solutions
Solution Overview
Problem
Radio frequency communication systems face challenges in high temperature environments, leading to impaired operation and communication with devices such as sensors and actuators.
Innovation Solution
A communication system with a high temperature logic circuit, power supply, and transponder components assembled on a silicon on insulator substrate, utilizing radio frequency waveguides to maintain communication and power transmission across temperature gradients.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Reliability
If conventional components are used in high temperature environments, then device complexity is reduced, but reliability deteriorates due to component failure above 125°C
Solution Approach 1:
The node is divided into distinct high temperature components (logic circuit, power supply) and low temperature components (transponder), with each segment optimized for its temperature range. The substrate acts as a physical separator that isolates thermal effects between components, allowing reliable operation in high temperature environments without requiring entirely new device architectures.
Solution Approach 2:
Different regions of the node are assigned different thermal characteristics - the first side operates at high temperature (125-500°C) while the second side operates at low temperature (-40-125°C). This local quality approach allows each component to operate in its optimal temperature range, with the substrate providing thermal management and isolation.
2Temperature
If high temperature components are used, then operating temperature range is improved, but manufacturing precision deteriorates due to material limitations
Solution Approach 1:
The node employs composite material construction, combining silicon on insulator substrate with high temperature capable components (logic circuit, power supply) and low temperature components (transponder). This composite approach leverages the thermal stability of the substrate while integrating components with different temperature requirements, achieving broad operating temperature range without sacrificing manufacturability.
3Stability of the object's composition
If components are isolated on different sides of the substrate, then temperature gradient stability is improved, but device complexity increases due to separate component placement
Solution Approach 1:
The node is segmented into distinct high temperature and low temperature sides on the substrate, with components placed according to their thermal requirements. This segmentation provides stable temperature gradients while maintaining a unified device structure, avoiding the need for entirely separate device assemblies.
Solution Approach 2:
The substrate serves multiple functions simultaneously: it provides mechanical support, electrical isolation, and thermal management by separating hot and cold components. This multi-functionality reduces overall device complexity despite the segmented component placement, as the substrate handles multiple roles that would otherwise require separate elements.
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
Enables reliable communication and power transmission in extreme temperature conditions, reducing cable complexity and weight while increasing system reliability and flexibility.
Implementation Method 1
a high temperature logic circuit, a power supply, wherein the high temperature logic circuit and the power supply are disposed on a first side of the node in a high temperature environment, and a transponder disposed on a second side of the node
Implementation Method 2
communicates with one of a sensor and an actuator via a radio frequency waveguide
Data Source
AI summary
An aircraft includes a communication system having a node and includes a method of operating the aircraft with the communication system. The communication system includes a waveguide and the node. The node is located in a high temperature environment. The node includes a high temperature logic circuit, a power supply, wherein the high temperature logic circuit and the power supply are disposed on a first side of the node in a high temperature environment, and a transponder disposed on a second side of the node. A sensor and/or an actuator can be operated via communication with the node via the waveguide.


