Enhanced New Applications & Use Cases Technical Implementation

Publication ID: 24-11858622_0007_PTD

Published: October 31, 2025

Category:New Applications & Use Cases

Legal Citation

pr1or.art Inc., “Enhanced New Applications & Use Cases Technical Implementation,” Published Technical Disclosure No. 24-11858622_0007_PTD, Published October 31, 2025, available at https://archive.pr1or.art/24-11858622_0007_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. 11,858,622.

Summary of the Inventive Concept

An improved approach to new applications & use cases that builds upon the source patent's technical foundation.

Background and Problem Solved

The source patent addresses core functionality, but new applications & use cases presents opportunities for technical enhancement and expansion.

Detailed Description of the Inventive Concept

A comprehensive technical system that implements new applications & use cases 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 new applications & use cases 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 new applications & use cases enhancements.

Section 103 Obviousness Analysis (PHOSITA)

▼

Field of Art

Aerospace engineering, specifically vertical takeoff and landing (VTOL) aircraft design, focusing on rotor systems, support structures, and aircraft configuration optimization

Person of Ordinary Skill (PHOSITA) Profile

An aerospace engineer with expertise in VTOL aircraft design, familiar with rotor mechanics, structural engineering, and aircraft configuration optimization, typically holding a master's degree or equivalent professional experience in aerospace or mechanical engineering

Obviousness Rationale

A person having ordinary skill in the art would recognize that the PTD's disclosed variations represent predictable extensions of the source patent's core technical concepts. The proposed improvements leverage known design principles and optimization techniques common in VTOL aircraft engineering. The variations demonstrate incremental advancements that would be apparent to a skilled practitioner seeking to enhance aircraft performance and functionality.

Obvious Combinations & Variations

Source Patent Element

Support member with bar-shaped configuration supporting takeoff and landing rotor

PTD Variation

Enhanced support member design with modular attachment points for multiple rotor configurations

Obviousness Reasoning

A PHOSITA would find it obvious to modify support member geometry to accommodate multiple rotor configurations using standard engineering design techniques, representing a predictable variation of known structural approaches

Source Patent Element

Rotor blade support with tapering cross-sectional geometry

PTD Variation

Adaptive tapering support member with dynamic angle adjustment based on operational parameters

Obviousness Reasoning

Implementing variable geometry support structures is a known technique in aerospace engineering, representing a straightforward design optimization that would be obvious to a skilled practitioner seeking improved performance characteristics

Source Patent Element

Vertical takeoff and landing rotor system

PTD Variation

Extended rotor configuration with integrated sensor and control systems for enhanced situational awareness

Obviousness Reasoning

Integrating sensor technologies with existing rotor systems is a predictable evolution in aircraft design, utilizing standard mechatronic integration techniques familiar to VTOL aircraft engineers

Source Patent Element

Aircraft rotor support configuration

PTD Variation

Lightweight composite material implementation for support structures

Obviousness Reasoning

Substituting traditional materials with advanced composites represents a standard engineering optimization approach, driven by well-understood goals of weight reduction and performance enhancement

Source Patent Element

Basic VTOL aircraft rotor arrangement

PTD Variation

Distributed rotor configuration with independent control and stabilization mechanisms

Obviousness Reasoning

Implementing distributed propulsion and control systems is a known technique in aerospace engineering, representing a logical extension of existing VTOL design principles

35 U.S.C. § 103 Summary: Pursuant to 35 U.S.C. § 103, the technical variations disclosed herein would have been obvious to a person having ordinary skill in the art at the time of invention, with a reasonable expectation of success, when considered in light of the teachings of US Patent 11858622. The proposed modifications represent predictable variations employing known techniques within the established technological framework of VTOL aircraft design, thereby rendering potential claims obvious and unpatentable.

Original Patent Information

Patent Number	US 11,858,622
Title	Aircraft
Assignee(s)	Honda Motor Co., Ltd.