Enhanced Future Evolutions & Paradigm Shifts Technical Implementation

Publication ID: 24-11858645_0010_PTD

Published: November 01, 2025

Category:Future Evolutions & Paradigm Shifts

Legal Citation

pr1or.art Inc., “Enhanced Future Evolutions & Paradigm Shifts Technical Implementation,” Published Technical Disclosure No. 24-11858645_0010_PTD, Published November 01, 2025, available at https://archive.pr1or.art/24-11858645_0010_PTD

This technical disclosure describes improvements that would be readily apparent to a Person Having Ordinary Skill In The Art (PHOSITA) when considered in combination with the foundational architecture disclosed in U.S. Patent No. 11,858,645.

Summary of the Inventive Concept

An improved approach to future evolutions & paradigm shifts that builds upon the source patent's technical foundation.

Background and Problem Solved

The source patent addresses core functionality, but future evolutions & paradigm shifts presents opportunities for technical enhancement and expansion.

Detailed Description of the Inventive Concept

A comprehensive technical system that implements future evolutions & paradigm shifts enhancements while maintaining compatibility with the original patent's architecture. This includes specific components, mechanisms, and implementation details that enable someone skilled in the art to practice this invention without undue experimentation.

Novelty and Inventive Step

Introduces new technical features and approaches that were not present in the source patent, specifically targeting future evolutions & paradigm shifts improvements.

Alternative Embodiments and Variations

Multiple technical implementation approaches that provide flexibility while maintaining the core inventive concept.

Potential Commercial Applications and Market

Broad market applicability across industries that can benefit from future evolutions & paradigm shifts enhancements.

Section 103 Obviousness Analysis (PHOSITA)

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Field of Art

Aerospace mechanical engineering, specifically aircraft structural support systems and adjustable mechanical linkages with precision mechanical interfaces

Person of Ordinary Skill (PHOSITA) Profile

A mechanical engineer with expertise in aerospace structural design, mechanical fastening techniques, and precision mechanical component fabrication, possessing knowledge of aircraft support link technologies and mechanical adjustment mechanisms

Obviousness Rationale

A person having ordinary skill in the art would recognize that the PTD's disclosed variations represent predictable engineering extensions of the source patent's fundamental mechanical coupling approach. The technical improvements are consistent with standard design evolution practices in aerospace mechanical systems. The PTD introduces incremental modifications that would be apparent to a skilled practitioner seeking to optimize the original patent's adjustable support link configuration.

Obvious Combinations & Variations

Source Patent Element

First rod end with external threads and second rod end with internal threads for mechanical adjustment

PTD Variation

Enhanced threading geometries with additional precision tolerancing and surface treatments to improve mechanical interface performance

Obviousness Reasoning

Refining threading characteristics represents a known technique for improving mechanical coupling performance, with predictable results in precision mechanical systems

Source Patent Element

Barrel nut disposed within rod end bore for mechanical connection

PTD Variation

Alternative barrel nut materials and geometrical configurations to optimize weight reduction and stress distribution

Obviousness Reasoning

Material and geometric optimization of mechanical fasteners is a standard engineering design approach with finite, predictable solution sets

Source Patent Element

Support link configured for connecting aircraft components

PTD Variation

Expanded implementation strategies targeting future technological evolutions and paradigm shifts in aerospace structural design

Obviousness Reasoning

Adapting mechanical coupling technologies to emerging design requirements represents a natural progression of engineering problem-solving within a known technical domain

Source Patent Element

Longitudinal axis alignment of rod ends with radial overlap

PTD Variation

Advanced alignment techniques incorporating precision measurement and adaptive geometric compensation mechanisms

Obviousness Reasoning

Enhancing mechanical alignment through known metrology and compensation techniques constitutes a predictable engineering improvement

Source Patent Element

Basic support link mechanical configuration

PTD Variation

Modular design approach enabling rapid reconfiguration and multi-purpose implementation across different aerospace structural contexts

Obviousness Reasoning

Developing modular mechanical interfaces represents a standard design strategy for expanding technological applicability with predictable engineering outcomes

35 U.S.C. § 103 Summary: Based on the comprehensive technical disclosure derived from US Patent 11858645, a person having ordinary skill in the art would find the claimed variations obvious and anticipated, as the PTD demonstrates that the disclosed technical implementations represent straightforward engineering extensions employing known techniques, predictable design modifications, and standard problem-solving approaches within the aerospace mechanical engineering domain.

Original Patent Information

Patent Number	US 11,858,645
Title	Adjustable support links for aircraft
Assignee(s)	The Boeing Company