Compactable Solar Power Arrays for Space Launch

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Solution Overview

Problem

Space-based solar structures face challenges in achieving commercially viable energy generation due to the high cost of launching large-scale structures into space, necessitating compact and lightweight designs, whereas ground-based systems can be bulky and inefficient without these constraints.

Innovation Solution

A compactable solar power generation array is developed, featuring solar concentrators with a curved body and resilient connectors that deploy to redirect solar radiation onto photovoltaic cells, utilizing carbon fiber matrices and reflective materials to optimize energy collection and reduce mass, and incorporating flexible structural support layers for self-deployment.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Productivity

If large arrays are used to generate commercially viable energy, then power generation capacity is improved, but launch cost increases significantly

Engineering Contradiction:
Improvepower generation capacityVSAvoidlaunch cost
Core Design Contradiction:
ProductivityVSWeight of stationary object

Solution Approach 1:

The solar power generation system is divided into multiple modular units (tiles) that can be independently deployed. Each tile contains integrated photovoltaic cells and concentrator optics, allowing the system to scale in discrete units rather than requiring a single large structure, thereby reducing launch cost while maintaining power generation capacity.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The design integrates multiple functional components within nested structures - photovoltaic cells are positioned at the focal points of concentrator optics, which are themselves integrated into the tile structure. This nesting allows maximum power generation density within minimum mass constraints.

Inventive Principle:
Principle #7Nested doll (Nesting)

2Productivity

If solar concentrators are deployed to redirect solar radiation onto photovoltaic cells, then energy collection efficiency is improved, but structural complexity increases

Engineering Contradiction:
Improveenergy collection efficiencyVSAvoidstructural complexity
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

Parabolic concentrator optics with curved surfaces are used to redirect solar radiation onto photovoltaic cells. The curved geometry naturally focuses parallel sunlight rays to a focal point, achieving high energy collection efficiency without requiring complex mechanical adjustment mechanisms.

Inventive Principle:
Principle #14Spheroidality (Curvature)

Solution Approach 2:

The concentrator optics are designed to automatically track and focus sunlight based on their geometric configuration, eliminating the need for active control systems or complex mechanical tracking mechanisms. The structure serves its own optical function through its inherent geometry.

Inventive Principle:
Principle #25Self-service

3Weight of stationary object

If compactable design is used to reduce mass and volume, then launch cost is reduced, but deployment mechanism complexity increases

Engineering Contradiction:
Improvemass and volumeVSAvoiddeployment mechanism complexity
Core Design Contradiction:
Weight of stationary objectVSDevice complexity

Solution Approach 1:

The solar tiles incorporate deployable mechanisms that transition from a compact stowed configuration during launch to a deployed operational configuration in space. The concentrator optics and photovoltaic cells are arranged to fold or collapse along with the tile structure, reducing mass and volume for launch while maintaining full functionality when deployed.

Inventive Principle:
Principle #15Dynamics

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 compactable design reduces the mass and volume of solar power generation arrays, enabling more efficient energy collection per unit mass, lowering launch costs, and improving the practicality of space-based solar power systems by allowing for greater power generation while minimizing weight and complexity.

Implementation Method 1

each of the at least two solar concentrators comprising a curved body having a front reflector surface

Methodology Applied
Scientific EffectReflection: Reflection

Implementation Method 2

at least one photovoltaic cell disposed on at least a portion of the back surface of each of the solar concentrators

Methodology Applied
Scientific EffectPhotovoltaic effect: Photovoltaic Effect

Data Source

PatentUS10992253B2Compactable power generation arrays
Publication Date: 2021.04.27 CALIFORNIA INST OF TECH
  • US10992253B2 patent drawing
  • US10992253B2 patent drawing
  • US10992253B2 patent drawing

AI summary

Compactable power generation arrays are provided. The compactable power generation arrays may include a structural substrate body having an array of solar concentrators configured to receive and re-direct solar radiation onto a plurality of photovoltaic (PV) cells. In many other embodiments the PV cells may be disposed upon a back surface of each of the solar concentrators such that an adjacent solar concentrator is configured to re-direct solar radiation onto the PV cell disposed on the back surface of the adjacent solar concentrator.