Three-Phase Flow-Through Water Heater for Aircraft Beverage Makers

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Solution Overview

Problem

Existing coffee makers for aircraft are unsuitable due to their reliance on single-phase power, fixed cores that hinder maintenance, excessive weight from solid metal construction, and inadequate temperature monitoring, posing safety and efficiency concerns.

Innovation Solution

A three-phase flow-through water heater with a removable lightweight baffle core, integrated resistance temperature detectors (RTDs) for temperature monitoring, and a custom circuit for efficient power management, utilizing a plasma-sprayed circuit on a stainless steel substrate with PEEK plastic core and removable end fittings for easy maintenance.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If a single-phase heating element is used, then the heating function works, but it cannot be used with aircraft three-phase power systems

Engineering Contradiction:
Improvepower system compatibilityVSAvoidheating function
Core Design Contradiction:
Adaptability or versatilityVSReliability

Solution Approach 1:

The heating element is modified to accept three-phase power input by changing the electrical configuration from single-phase to three-phase wiring, allowing compatibility with aircraft power systems while maintaining the heating function

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The heating element is designed to universally accept three-phase power input, making it adaptable to aircraft electrical systems while retaining its primary heating function for beverage preparation

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

2Weight of moving object

If the heating core is made of solid metal, then structural strength is provided, but weight increases which is undesirable for aircraft components

Engineering Contradiction:
Improveheating core weightVSAvoidcore structural strength
Core Design Contradiction:
Weight of moving objectVSStrength

Solution Approach 1:

The heating core is constructed using composite materials that combine the heating element with a lighter structural support system, reducing overall weight while maintaining necessary structural integrity for aircraft application

Inventive Principle:
Principle #40Composite materials

Solution Approach 2:

The core structure utilizes thin-walled construction with optimized structural geometry that provides sufficient strength at reduced weight, eliminating the need for heavy solid metal construction

Inventive Principle:
Principle #30Flexible shells and thin films

3Ease of repair

If the heating core is fixed and welded, then structural integrity is maintained, but maintenance and inspection of scale buildup become difficult

Engineering Contradiction:
Improvecore maintenance accessibilityVSAvoidstructural integrity
Core Design Contradiction:
Ease of repairVSReliability

Solution Approach 1:

The heating core is divided into separable sections with removable end fittings, allowing the core to be disassembled for inspection and cleaning of scale buildup while maintaining structural integrity during operation

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The core design transitions from a fixed welded structure to a dynamically configurable assembly that can be easily disassembled and reassembled, enabling routine maintenance without compromising structural integrity when properly reconnected

Inventive Principle:
Principle #15Dynamics

4Reliability

If temperature monitoring is not implemented, then the system is simpler, but safety concerns and heating inefficiencies arise

Engineering Contradiction:
Improvetemperature control safetyVSAvoidsystem complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

Temperature monitoring sensors are integrated into the heating system to provide feedback on water temperature, enabling automatic control of the heating element to prevent overheating and improve energy efficiency

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The temperature monitoring system automatically regulates heating operation, with sensors detecting temperature conditions and controlling power delivery without requiring manual intervention, ensuring safe operation

Inventive Principle:
Principle #25Self-service

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 safe and efficient operation with improved temperature control, reduced weight, and enhanced maintenance capabilities, ensuring compliance with aircraft power requirements and safety standards.

Implementation Method 1

Water is pumped through a tubing with a resistive heating element that heats the water as it flows through the tubing. The resistive heating element is typically a coiled wire, similar to the element in an electric toaster, that heats up when electricity is run through it.

Methodology Applied
Scientific EffectResistive heating: Joule Heating

Implementation Method 2

The resistive heating element presses directly against the underside of the warming plate, and white, heat-conductive materials such as grease make sure the heat transfers efficiently.

Methodology Applied
Scientific EffectThermal conduction: Conduction (thermal)

Data Source

PatentEP3169201B1Multi-phase circuit flow-through heater for aerospace beverage maker
Publication Date: 2019.09.04 BE AEROSPACE INC
  • EP3169201B1 patent drawingFigure 1
  • EP3169201B1 patent drawingFigure 2
  • EP3169201B1 patent drawingFigure 3

AI summary

A water heater for an aircraft beverage brewing apparatus includes a three way electrical conduit (12) for conducting electrical power in three separate phases. The heater has a housing (14) with a fluid inlet port at a first removable end piece (18) and a fluid outlet port (42) at a second removable end piece (20). The hollow cylindrical core incorporates a heating element wound around the core, and the housing includes three resettable temperature sensors at the outlet, each of the three resettable temperature sensors (24a, 24b, 24c) connected to a separate phase of power from the three way electrical conduit.