Furlable Antenna Blade Restraint and Release Mechanism

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Solution Overview

Problem

Existing deployable antenna systems face challenges in compact stowage and efficient deployment, lacking effective mechanisms to prevent slippage and ensure reliable deployment mechanisms.

Innovation Solution

The development of furlable antenna blade devices and systems that include conductive elements with laminate layers, antenna support components, restraint bands, and release mechanisms, such as rotational hinges and torsion springs, to control the deployment of antenna blades from a storage compartment, preventing slippage and ensuring efficient unfurling.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Volume of moving object

If antenna blades are stored in a compact configuration, then stowage space is reduced, but deployment reliability may be compromised due to potential slippage

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

Solution Approach 1:

The restraint band is pre-configured to engage with the antenna blade at a specific location before deployment. The release mechanism is pre-positioned to automatically disengage the restraint band at the optimal moment during deployment, ensuring reliable unfurling without slippage while maintaining compact stowage

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The restraint band acts as an intermediary component between the antenna blade and the release mechanism. It provides a controlled interface that prevents slippage during stowage while allowing reliable deployment when released, solving the contradiction between compact storage and deployment reliability

Inventive Principle:
Principle #24Intermediary (Mediator)

2Reliability

If restraint mechanisms are added to prevent slippage, then deployment reliability improves, but device complexity increases

Engineering Contradiction:
Improvedeployment reliabilityVSAvoidmechanism complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The release mechanism is designed to automatically disengage the restraint band from the antenna blade without requiring external intervention. The mechanism uses the deployment motion itself to trigger the release, reducing complexity by eliminating the need for separate actuation systems while maintaining high deployment reliability

Inventive Principle:
Principle #25Self-service

3Strength

If antenna blades are designed with conductive elements and laminate layers, then structural integrity is improved, but manufacturing complexity increases

Engineering Contradiction:
Improvestructural integrityVSAvoidmanufacturing complexity
Core Design Contradiction:
StrengthVSEase of manufacture

Solution Approach 1:

The antenna blade uses a composite structure with conductive elements embedded within laminate layers. This design provides the necessary structural integrity and electrical conductivity while using standardized composite manufacturing processes that balance performance requirements with manufacturing feasibility

Inventive Principle:
Principle #40Composite materials

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

These systems enable compact stowage and efficient deployment of antenna blades, preventing slippage and ensuring reliable operation by using conductive elements with laminate layers and advanced restraint mechanisms, enhancing deployment precision and stability.

Implementation Method 1

one or more torsion springs configured for the rotational deployment of the one or more furlable antenna blade components from a storage compartment

Methodology Applied
Scientific EffectTorsion spring: Torsion Spring

Implementation Method 2

the one or more stops include at least a crushable energy absorber or an elastic element

Methodology Applied
Scientific EffectElasticity: Elasticity

Data Source

PatentUS11069951B2Furlable antenna blade devices, systems, and methods
Publication Date: 2021.07.20 REDWIRE SPACE SOLUTIONS LLC
  • US11069951B2 patent drawing
  • US11069951B2 patent drawing
  • US11069951B2 patent drawing

AI summary

Methods, systems, and devices for furlable antenna blade components are provided in accordance with various embodiments. For example, some embodiments include a device that may include one or more furlable antenna blade components; each of the one or more furlable antenna blade components may include one or more conductive elements. In some embodiments, each of the one or more furlable antenna blade components include one or more laminate layers. Some embodiments include a method that may include: furling one or more furlable antenna blade components around a central axis; and/or securing the one or more furlable antennae blade components when in a furled state.