Furlable Sail with Shear Take-Up and Structural Sheet

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Solution Overview

Problem

Deployable sail systems face challenges in sail support, stowage, and deployment, particularly in maintaining structural integrity and preventing issues like telescoping and ballooning during deployment and stowage.

Innovation Solution

The implementation of a furlable sail system that includes a furlable boom and a shear take-up mechanism with springs, coupled with a structural sheet made of fiber-reinforced polymer composite, and a hold-down and release mechanism with a restraint strap to manage tension and prevent telescoping, along with a slit-tube boom with high-strain composite material for tailored deployment energy.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If traditional lateral supports are used to maintain structural integrity, then strength is improved, but device complexity increases

Engineering Contradiction:
Improvestructural integrityVSAvoiddevice complexity
Core Design Contradiction:
StrengthVSDevice complexity

Solution Approach 1:

The patent removes traditional lateral supports (battens) from the sail structure. Instead, the sail membrane itself is engineered with varying bending stiffness to provide structural support, eliminating unnecessary components and reducing device complexity while maintaining strength.

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The sail membrane incorporates non-uniform bending stiffness distribution, with stiffer regions at critical locations (leading edge, trailing edge, and radial ribs) and more flexible regions elsewhere. This local quality variation provides structural integrity where needed without requiring lateral supports throughout the entire sail.

Inventive Principle:
Principle #3Local quality

2Area of moving object

If the sail is fully deployed, then area is improved, but stability deteriorates due to telescoping and ballooning

Engineering Contradiction:
Improvesail areaVSAvoidsail stability
Core Design Contradiction:
Area of moving objectVSStability of the object's composition

Solution Approach 1:

The sail membrane features spatially varying bending stiffness with rigid radial ribs and flexible inter-rib regions. This local quality differentiation prevents telescoping by maintaining shape at critical locations while allowing controlled deformation in other areas, and prevents ballooning through the stiffened leading and trailing edges.

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The sail design allows dynamic adaptation of its structural properties through the varying bending stiffness distribution. The flexible inter-rib regions enable the sail to adjust its shape dynamically during deployment and operation, maintaining stability while achieving full area deployment.

Inventive Principle:
Principle #15Dynamics

3Volume of moving object

If the sail is compactly stowed, then volume is improved, but reliability deteriorates due to crep and telescoping

Engineering Contradiction:
Improvestowage volumeVSAvoidsail reliability
Core Design Contradiction:
Volume of moving objectVSReliability

Solution Approach 1:

The sail is stowed in a compact rolled configuration within a cylindrical dispenser, with the furlable boom nested alongside. This nesting arrangement achieves compact stowage volume while the varying bending stiffness structure prevents crep and telescoping during the stowed phase, maintaining reliability.

Inventive Principle:
Principle #7Nested doll (Nesting)

4Ease of operation

If self-deployment is implemented, then ease of operation is improved, but control precision worsens

Engineering Contradiction:
Improveease of deploymentVSAvoiddeployment precision
Core Design Contradiction:
Ease of operationVSManufacturing precision

Solution Approach 1:

The sail and boom are pre-assembled with the varying bending stiffness structure and radial ribs in the desired final configuration before stowage. This preliminary action ensures that when self-deployment occurs, the structure naturally assumes the correct shape with high precision, combining ease of operation with deployment precision.

Inventive Principle:
Principle #10Preliminary action

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 allows for self-supporting, efficient deployment and stowage of the sail without traditional lateral supports, preventing creep and telescoping, while maintaining structural integrity and adaptability for various applications such as deorbit sails and solar sails.

Implementation Method 1

The shear take-up mechanism may include one or more springs coupled with the root end of the furlable sail

Methodology Applied
Scientific EffectElasticity: Elasticity

Implementation Method 2

The shear take-up mechanism may include one or more springs coupled with the root end of the furlable sail

Methodology Applied
Scientific EffectSpring: Spring

Implementation Method 3

The high-strain composite laminate geometry and/or material may be tailored along the slit-tube axial length to vary the deployment energy, authority and/or behavior

Methodology Applied
Scientific EffectElastic energy storage: Elasticity

Data Source

PatentUS11292619B2Furlable sail devices, systems, and methods
Publication Date: 2022.04.05 REDWIRE SPACE SOLUTIONS LLC
  • US11292619B2 patent drawing
  • US11292619B2 patent drawing
  • US11292619B2 patent drawing

AI summary

Furlable sail devices, systems, and methods are provided in accordance with various embodiments. For example, some embodiments include a system and/or device that may include: a furlable boom; a furlable sail coupled with a distal end of the furlable boom; and/or a shear take-up mechanism coupled with a root end of the furlable sail. In some embodiments, the shear take-up mechanism applies tension to the furlable sail. The shear-take up mechanism may include one or more springs coupled with the root end of the furlable sail. In some embodiments, the furlable sheet includes a structural sheet. The structural sheet may include one or more areas with bending stiffness. The structural sheet may be fabricated to be self-supporting. In some embodiments, the furlable boom includes a slit-tube boom. Some embodiments may be configured as deorbit sails.