Loop Heat Pipe Remote Compensation Chamber Design

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Solution Overview

Problem

Current capillary driven two-phase thermal control systems for spacecraft face limitations in expandability, controllability, and vapour parasitic heat leak tolerance, particularly in multi-evaporator designs, leading to unreliable operation under varying thermal conditions.

Innovation Solution

A two-phase capillary driven LHP system with a remote compensation chamber and secondary capillary pump, allowing for flexible configuration with multiple evaporators and condensers, vapour parasitic heat leak tolerance, and scalable design, where the remote compensation chamber manages vapour and liquid phases to prevent dry-out and non-condensable gas accumulation.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If multiple evaporators with individual compensation chambers are used, then the number of evaporators increases and thermal control flexibility improves, but the compensation chamber volume increases rapidly and device complexity increases

Engineering Contradiction:
Improvenumber of evaporatorsVSAvoidcompensation chamber volume
Core Design Contradiction:
Adaptability or versatilityVSVolume of stationary object

Solution Approach 1:

The patent merges multiple individual compensation chambers into a single shared compensation chamber that serves multiple evaporators. This consolidation reduces the total volume required while maintaining the ability to support multiple evaporators operating at different temperatures and heat loads, directly resolving the contradiction between increasing evaporator count and minimizing compensation chamber volume.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The shared compensation chamber is designed to perform multiple functions simultaneously: it serves as the compensation chamber for all evaporators, acts as a liquid reservoir, and provides thermal coupling between evaporators. This multi-functionality allows a single chamber to replace multiple individual chambers, reducing overall system volume while maintaining adaptability.

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

2Adaptability or versatility

If multiple evaporators with individual compensation chambers are used, then thermal control flexibility improves, but device complexity and mass increase

Engineering Contradiction:
Improvethermal control flexibilityVSAvoidsystem complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The patent combines multiple compensation chambers into one shared chamber, reducing the number of components and interconnections required. This merging simplifies the overall system architecture while preserving thermal control flexibility through the chamber's ability to serve multiple evaporators simultaneously at different operating conditions.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The shared compensation chamber performs multiple functions including liquid compensation, thermal coupling, and vapor-liquid separation for all evaporators. This multi-functionality reduces the need for separate dedicated components for each evaporator, thereby reducing device complexity while maintaining adaptability.

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

3Stability of the object's composition

If evaporators are rigidly connected at close distances, then structural stability improves, but scalability and flexibility in component locations deteriorate

Engineering Contradiction:
Improvestructural stabilityVSAvoidscalability
Core Design Contradiction:
Stability of the object's compositionVSAdaptability or versatility

Solution Approach 1:

The shared compensation chamber acts as an intermediary component that couples multiple evaporators without requiring rigid direct connections between them. This intermediary approach allows evaporators to be positioned at greater distances and in more flexible configurations while maintaining system stability through the common compensation chamber that mediates thermal and fluid interactions.

Inventive Principle:
Principle #24Intermediary (Mediator)

4Device complexity

If vapour parasitic heat leak is not addressed, then device complexity remains low, but reliability deteriorates due to dry-out and non-condensable gas accumulation

Engineering Contradiction:
Improvesystem simplicityVSAvoidoperational reliability
Core Design Contradiction:
Device complexityVSReliability

Solution Approach 1:

The patent extracts and removes vapour from the system by providing dedicated vapour removal pathways from the shared compensation chamber. This extraction of harmful vapour prevents parasitic heat leak, dry-out conditions, and non-condensable gas accumulation, thereby improving reliability without requiring complex additional systems.

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The patent converts the potentially harmful vapour parasitic heat leak into a manageable phenomenon by designing the shared compensation chamber to actively manage and remove vapour. The vapour generation is anticipated and addressed through deliberate vapour removal mechanisms, transforming a reliability threat into a controlled aspect of system operation.

Inventive Principle:
Principle #22Blessing in disguise (Convert harm into benefit)

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 system achieves reliable operation across a wide range of conditions, enabling flexible configuration, vapour parasitic heat leak tolerance, and efficient heat load sharing, with the ability to handle varying power inputs and temperatures, and supports a large number of evaporators and condensers without the need for large compensation chambers.

Implementation Method 1

The primary capillary pump serves for absorbing heat from the equipment, which has to be cooled, and for providing fluid heat continuous circulation between the evaporator and the condenser

Methodology Applied
Scientific EffectCapillary action: Capillary Action

Implementation Method 2

The secondary capillary pump serves for supplying liquid to the primary wick and, together with the stabilization-compensation chamber and the remote compensation chamber, for providing fluid/heat intermittent circulation in transient regimes of operation of the system

Methodology Applied
Scientific EffectCapillary action: Capillary Action

Implementation Method 3

In steady state regimes of operation of the system, the stabilization-compensation chamber serves to remove internal heat leak through a primary capillary pump by convection and condensation on the heat exchanger surface

Methodology Applied
Scientific EffectCondensation: Condensation

Data Source

PatentEP2940416B1Loop heat pipe apparatus for heat transfer and thermal control
Publication Date: 2017.09.27 IBERICA DEL ESPACIO
  • EP2940416B1 patent drawingFigure 1a
  • EP2940416B1 patent drawingFigure 1b
  • EP2940416B1 patent drawingFigure 1c

AI summary

Loop heat pipe apparatus (1) for heat transfer and thermal control, using a two-phase fluid as a working media and comprising: - at least one evaporator (2) to be connected with a heat source and comprising a thermal stabilization-compensation chamber (10) attached to the at least one evaporator (2) and a secondary capillary pump (40) located inside the thermal stabilization-compensation chamber (10), - at least one condenser (27) to be connected with a heat sink, - liquid lines (24) and vapour lines (28) connecting the at least one evaporator (2) and the at least one condenser (27), and - a remote compensation chamber (20), wherein the thermal stabilization-compensation chamber (10) comprises a two-phase reservoir (5) and a liquid accumulator reservoir (6) separated by a heat exchange surface (15), such that the remote compensation chamber (20) is hydraulically connected with the two-phase reservoir (5) and the liquid accumulator reservoir (6).