Satellite Antenna Mounting Protrusions Versatile Structure Grip

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Solution Overview

Problem

Existing systems for attaching objects to structures are limited in their applicability due to constraints on the type, construction, and orientation of structures, leaving gaps in application types that need to be addressed.

Innovation Solution

A system comprising a first element, a second element, and a tightening mechanism, where the elements have protrusions that engage with a structure, allowing for secure mounting of satellite antennas or other devices, using a rotatable coupling mechanism to ensure stability across various structural materials.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If existing attachment systems are used, then they can securely attach objects to structures, but they are limited in applicability to specific structure types, constructions, and orientations

Engineering Contradiction:
Improveapplicability to different structure typesVSAvoidsecure attachment
Core Design Contradiction:
Adaptability or versatilityVSReliability

Solution Approach 1:

The mounting system is designed to function across multiple structure types (wood, metal, concrete, masonry, vinyl siding) and orientations (horizontal, vertical, angled surfaces) through a universal attachment mechanism that adapts to different substrates without requiring structure-specific components

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

Solution Approach 2:

The mounting system divides the attachment function into separate modular elements: protrusions for penetration, a mounting body for positioning, and a securing mechanism for fastening. This segmentation allows each component to be optimized for its specific function while maintaining overall versatility across different structure types

Inventive Principle:
Principle #1Segmentation

2Adaptability or versatility

If protrusions are used to penetrate and grip softer structural materials, then adaptability to various structures is improved, but the risk of damaging the structure increases

Engineering Contradiction:
Improvemounting on softer materialsVSAvoidstructure damage
Core Design Contradiction:
Adaptability or versatilityVSObject-affected harmful factors

Solution Approach 1:

The protrusions are designed with localized gripping surfaces and geometry optimized for engaging softer materials like vinyl siding without causing widespread damage. The contact area and penetration depth are controlled to provide secure attachment while minimizing harm to the underlying structure

Inventive Principle:
Principle #3Local quality

3Adaptability or versatility

If a rotatable coupling mechanism is used to provide flexibility in device orientation, then adaptability is improved, but device complexity increases

Engineering Contradiction:
Improvedevice orientation flexibilityVSAvoidmounting system complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The mounting system incorporates a rotatable coupling mechanism that allows the satellite antenna to be dynamically adjusted to various orientations after installation. This dynamic adjustment capability enables the antenna to be positioned optimally for different mounting locations and structural orientations

Inventive Principle:
Principle #15Dynamics

Data Source

PatentUS10648614B2Satellite antenna mounting systems and methods
Publication Date: 2020.05.12 DISH NETWORK LLC
  • US10648614B2 patent drawing
  • US10648614B2 patent drawing
  • US10648614B2 patent drawing

AI summary

Systems for coupling a satellite antenna to a structure is provided. The system may include a first element, a second element, a third element, and a tightening mechanism. The first element may include at least one protrusion. The second element may also include at least one protrusion. The third element may be rotatably coupled with the first element. The third element may also be rotatably coupled with the second element. The third element may further be configured to couple with the satellite antenna. The tightening mechanism may be operable to rotate at least one of the first element or the second element with respect to the third element such that at least one protrusion of the first element and at least one protrusion of the second element engage with the structure located between the first element and the second element.