Autonomous Helicopter Payload Rail for CG-Aligned Modular Missions

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Solution Overview

Problem

Conventional unmanned aerial vehicles (UAVs) face issues such as reliance on remote piloting, limited range, slower speeds, and reduced reliability, which hinder their performance in various tasks.

Innovation Solution

An unmanned helicopter platform with a fuselage housing flight control electronics, a tail section, a main rotor assembly, and a payload rail, equipped with a processor to autonomously determine and execute routes based on tasks, geography, and terrain, allowing for autonomous operation and modular payload management.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If conventional drones are remotely piloted, then human control is maintained, but reliability and performance are reduced

Engineering Contradiction:
Improvesystem reliabilityVSAvoidautonomous operation capability
Core Design Contradiction:
ReliabilityVSExtent of automation

Solution Approach 1:

The drone system performs self-navigation, self-monitoring, and self-control functions through integrated sensors, processors, and autonomous flight control algorithms, eliminating the need for remote human piloting and thereby improving reliability

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The patent replaces manual remote control operations with automated electronic control systems including flight control computers, GPS receivers, and sensor arrays that autonomously manage navigation and mission execution

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

2Adaptability or versatility

If conventional drones have fixed configurations, then manufacturing is simplified, but adaptability and versatility are limited

Engineering Contradiction:
Improvemission adaptabilityVSAvoidsystem configuration complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The drone system is divided into modular components including interchangeable payloads, adjustable landing gear configurations, and separable sensor modules that can be tailored to specific mission requirements without redesigning the entire platform

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent incorporates dynamically adjustable features such as variable geometry landing gear, reconfigurable payload mounts, and adaptive flight control parameters that allow the system to optimize its configuration based on real-time mission needs

Inventive Principle:
Principle #15Dynamics

Data Source

PatentUS11721222B2Ruggedized autonomous helicopter platform
Publication Date: 2023.08.08 ANDURIL IND INC
  • US11721222B2 patent drawing
  • US11721222B2 patent drawing
  • US11721222B2 patent drawing

AI summary

An unmanned helicopter platform includes a fuselage, a tail coupled with the fuselage, a payload rail coupled with and extending along the fuselage and a main rotor assembly coupled with the fuselage. The tail includes a tail rotor and a tail rotor motor. The main rotor assembly includes a main rotor having an axis of rotation and a main rotor motor. The payload rail allows mechanical connection of payloads to the fuselage and positioning of the payloads such that a center of gravity of the payloads is alignable with the axis of rotation.