Vacuum Spray Boiler Heat Exchanger for Spaceflight Cooling

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Solution Overview

Problem

Existing airplane hydraulic oil coolers are not mass efficient as they do not boil the coolant, which is preferred for spaceflight applications. Additionally, cooling architectures like the Water Spray Boiler (WSB) face issues with coolant freezing in cold space temperatures and have high mass, making them undesirable for repeatable and economical space flight.

Innovation Solution

The development of a vacuum spray boiler heat exchanger system that uses a plate-fin architecture and integrates a coolant spray apparatus to spray boil a coolant in vacuum or atmospheric pressure, preventing coolant freezing through thermal contact with the warm heat exchanger and maintaining vaporized coolant at a temperature above its freezing point.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Temperature

If a water spray boiler is used for cooling in space, then cooling effectiveness is improved, but coolant freezing occurs in cold space temperatures

Engineering Contradiction:
Improvecooling effectivenessVSAvoidcoolant freezing
Core Design Contradiction:
TemperatureVSReliability

Solution Approach 1:

The patent changes the pressure parameter of the coolant system to vacuum pressure, which fundamentally alters the phase change behavior. Under vacuum conditions, the boiling point of water drops significantly, allowing the coolant to boil at lower temperatures and preventing freezing even in cold space environments. This parameter change enables the system to maintain reliability while achieving effective cooling.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The patent exploits phase transitions of water under vacuum conditions. By operating in vacuum, water undergoes rapid evaporation and phase change from liquid to vapor at lower temperatures, enabling efficient heat transfer without freezing. The phase transition mechanism allows the coolant to absorb heat effectively while remaining in a usable state, avoiding the freezing problem that occurs at atmospheric pressure in cold space temperatures.

Inventive Principle:
Principle #36Phase transitions

2Temperature

If a water spray boiler is used for cooling, then cooling capability is improved, but system mass becomes relatively high

Engineering Contradiction:
Improvecooling capabilityVSAvoidsystem mass
Core Design Contradiction:
TemperatureVSWeight of moving object

Solution Approach 1:

The patent uses vacuum as an inert environment to enable efficient phase change cooling. The vacuum condition creates an environment where water vapor can escape freely without condensing or freezing, allowing for highly efficient heat transfer with minimal coolant mass. This inert vacuum environment eliminates the need for heavy insulation and heating systems required to prevent freezing in atmospheric pressure systems.

Inventive Principle:
Principle #39Inert atmosphere (Inert environment)

3Device complexity

If conventional heat exchangers are used without boiling, then system simplicity is maintained, but mass efficiency deteriorates for spaceflight

Engineering Contradiction:
Improvesystem simplicityVSAvoidmass efficiency
Core Design Contradiction:
Device complexityVSWeight of moving object

Solution Approach 1:

The patent introduces phase transition (boiling) of the coolant as the core cooling mechanism. By utilizing vacuum-induced boiling of water, the system achieves superior mass efficiency compared to conventional heat exchangers. The phase change process enables high heat transfer coefficients and efficient cooling with minimal coolant mass, making it ideal for spaceflight applications where mass is critical.

Inventive Principle:
Principle #36Phase transitions

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 vacuum spray boiler effectively cools hot fluids by spray boiling a coolant, preventing freezing in extreme cold temperatures, and offers a more mass-efficient solution for spaceflight applications compared to traditional cooling systems.

Implementation Method 1

The coolant consequently phase changes from a sprayed fluid state to a boiled vapor

Methodology Applied
Scientific EffectPhase change: Phase Change

Implementation Method 2

The sprayed water generally converts to water vapor by the relatively hot tubes

Methodology Applied
Scientific EffectEvaporation: Evaporation

Implementation Method 3

cooling is achieved by spraying water (or some water-based mixture) onto tubes (or channels) that contain flowing fluid to be cooled

Methodology Applied
Scientific EffectSpray: Spray

Implementation Method 4

a heat exchanger that doubles as a container for the cooling liquid

Methodology Applied
Scientific EffectHeat transfer: Heat Exchanger

Implementation Method 5

thermal contact with the warm heat exchanger

Methodology Applied
Scientific EffectThermal conduction: Conduction (thermal)

Implementation Method 6

vacuum spray boiler heat exchanger system that uses a plate-fin architecture and integrates a coolant spray apparatus to spray boil a coolant in vacuum

Methodology Applied
Scientific EffectVacuum: Vacuum

Data Source

PatentUS20250085059A1Vacuum spray boiler
Publication Date: 2025.03.13 BLUE ORIGIN MANUFACTURING LLC
  • US20250085059A1 patent drawing
  • US20250085059A1 patent drawing
  • US20250085059A1 patent drawing

AI summary

A heat exchanger system, in particular a vacuum spray boiler, cools a hot fluid by spraying a coolant onto chambers carrying the hot fluid. This process may be performed in i) a vacuum, as in space, ii) atmospheric pressure, as on a launch pad of a space vehicle, or iii) any pressure therebetween. The heat exchanger system may incorporate a plate-fin heat exchanger. A coolant spray apparatus, used for spraying the coolant, and the heat exchanger are integrated within a vacuum chamber. The coolant, subsequent to changing to a vapor state after being sprayed onto the heat exchanger, may be exhausted to outside the system.