Articulating Solar Array Leaves for Compact Transport and Deployment

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Solution Overview

Problem

Design challenges for articulating and transportable solar power systems include durability during transport and deployment, protection from damage during high wind events, and achieving a compact configuration compatible with transport modes.

Innovation Solution

A solar array design featuring an elongate support, slew drive, and pivotally coupled solar panel leaves, with a base and optional energy storage, allowing for deployment and articulation without failure, and a transport fixture for secure transport.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If solar panels are made rigid and fixed for durability, then structural strength is improved, but transportability and space efficiency deteriorate

Engineering Contradiction:
Improvestructural strengthVSAvoidtransportability
Core Design Contradiction:
StrengthVSAdaptability or versatility

Solution Approach 1:

The solar array is divided into multiple leaves that can be pivotally coupled together. Each leaf can be independently positioned and secured, allowing the structure to be disassembled into compact segments for transport while maintaining full structural strength when deployed. The leaves are connected through pivotal couplings that enable both rigid deployment and flexible packaging.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The solar array employs dynamic articulation mechanisms including pivotal couplings and slew drives that allow the structure to transition between deployed and transported configurations. During deployment, the leaves articulate to form a rigid sun-tracking structure; during transport, they fold into compact arrangements. This dynamic adaptability resolves the contradiction between structural strength and transportability.

Inventive Principle:
Principle #15Dynamics

2Adaptability or versatility

If solar panels are made articulating with multiple moving parts, then adaptability and sun-tracking capability are improved, but reliability and resistance to failure deteriorate

Engineering Contradiction:
Improvesun-tracking capabilityVSAvoiddeployment reliability
Core Design Contradiction:
Adaptability or versatilityVSReliability

Solution Approach 1:

The pivotal couplings are pre-configured with inherent mechanical constraints and alignment features that guide the leaves into correct positions during deployment. This pre-engineered guidance system reduces the risk of misalignment or failure during articulation operations, thereby maintaining reliability while enabling sun-tracking capability.

Inventive Principle:
Principle #11Beforehand cushioning (Prior cushioning)

Solution Approach 2:

The articulation mechanism employs self-aligning pivotal couplings that automatically guide the leaves into their correct deployed configuration without requiring external intervention or complex control systems. The mechanical design itself provides the alignment and positioning functions, reducing points of failure while maintaining adaptability.

Inventive Principle:
Principle #25Self-service

3Volume of moving object

If solar arrays are designed for compact transport configuration, then space efficiency is improved, but structural stability and durability during deployment deteriorate

Engineering Contradiction:
Improvetransport volumeVSAvoiddeployment stability
Core Design Contradiction:
Volume of moving objectVSStability of the object's composition

Solution Approach 1:

The solar array is segmented into multiple leaves that can be compactly folded during transport while maintaining structural integrity when deployed. Each leaf is designed to fold into a compact arrangement that minimizes transport volume, yet the same segmented structure assembles into a stable, rigid configuration when deployed with full structural strength.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The structure transitions dynamically between compact transport configuration and stable deployed configuration. During transport, the leaves are folded into a compact arrangement minimized volume. When deployed, the same articulation mechanisms enable the leaves to form a rigid, stable structure capable of withstanding operational loads and maintaining compositional stability.

Inventive Principle:
Principle #15Dynamics

Data Source

PatentUS20250279746A1Articulating solar arrays and methods
Publication Date: 2025.09.04 HELICAL SOLAR SOLUTIONS LLC
  • US20250279746A1 patent drawing
  • US20250279746A1 patent drawing
  • US20250279746A1 patent drawing

AI summary

A solar array includes an elongate support having a proximal end and a distal end, a slew drive coupled to the distal end of the elongate support, and first and second pivotally coupled leaves of solar panels, where the first leaf is coupled to the slew drive. In some examples, the solar array further includes a base coupled to the proximal end of the elongate support, and optionally, at least one energy storage system.