Aircraft Apparatus with Dynamic Docking for Payload Redistribution

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Solution Overview

Problem

Existing automated transport systems, including those using scalable aircraft apparatuses and self-propelled modules, are unable to redistribute payloads during transportation, limiting their flexibility and efficiency.

Innovation Solution

The system incorporates aircraft apparatuses with air propulsion units, docking modules, and guides that allow for detachable connection and reconfiguration, enabling the formation of cluster guides for payload movement and redistribution by allowing aircraft and self-propelled modules to dock and undock dynamically, with control modules managing these operations.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If aircraft apparatuses use fixed-position payload mounting, then structural simplicity is maintained, but payload redistribution capability is lost

Engineering Contradiction:
Improvepayload redistribution capabilityVSAvoidguide system complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The payload transport system is segmented into multiple independent aircraft apparatuses, each with its own guide system. This allows the payload to be divided into segments that can be independently transported and redistributed. Each aircraft apparatus carries a portion of the payload along its guide, enabling flexible reconfiguration without requiring a monolithic complex structure.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The guide system is designed with universal docking modules that can connect different aircraft apparatuses in various configurations. The same guide structure serves multiple functions: transporting payload segments, enabling redistribution between aircraft, and providing detachable connections for flexible reconfiguration. This multi-functionality reduces overall system complexity while maintaining adaptability.

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

2Adaptability or versatility

If aircraft apparatuses dock permanently, then structural stability is improved, but reconfiguration flexibility is reduced

Engineering Contradiction:
Improvereconfiguration flexibilityVSAvoiddocking stability
Core Design Contradiction:
Adaptability or versatilityVSReliability

Solution Approach 1:

The docking modules incorporate dynamic connection mechanisms that can transition between locked and unlocked states. This allows the system to switch between stable docked configurations for transport and flexible undocked configurations for reconfiguration. The dynamic nature of the docking system enables both permanent-looking stability during transport and easy reconfiguration when needed.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The control systems of the aircraft apparatuses communicate docking status and configuration information in real-time. This feedback mechanism ensures that docking operations are coordinated properly, maintaining stability when docked while enabling safe undocking and reconfiguration when required. The feedback loop allows the system to adapt its docking stability based on operational requirements.

Inventive Principle:
Principle #23Feedback

3Adaptability or versatility

If payload position is fixed relative to aircraft housing, then mounting simplicity is maintained, but transport path flexibility is lost

Engineering Contradiction:
Improvetransport path flexibilityVSAvoidguide mounting complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The guide system is nested within the aircraft apparatus structure, with guides integrated into the housing and payload segments nested along the guide paths. This nesting arrangement allows the guide system to be compact yet flexible, enabling transport path reconfiguration without requiring external complex mounting structures. The payload segments can be positioned at different locations along the nested guide system.

Inventive Principle:
Principle #7Nested doll (Nesting)

Solution Approach 2:

The guide system incorporates multi-dimensional movement capabilities, allowing payload segments to move not only along the primary transport axis but also in lateral and vertical dimensions. This dimensional flexibility enables the payload to be redistributed to different aircraft apparatuses and repositioned along various transport paths without requiring overly complex mounting mechanisms.

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

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

This solution enhances the flexibility and efficiency of payload movement by enabling redistribution and reconfiguration of transport paths, expanding the range of means for moving payloads and improving the overall efficiency of the transport process.

Implementation Method 1

one or more air propulsion units enabling movement of the aircraft apparatus through the air

Methodology Applied
Scientific EffectAir propulsion: Jet

Data Source

PatentUS20240217678A1Aircraft apparatus (variants), self-propelled module, payload, system and method for moving payload (variants)
Publication Date: 2024.07.04 ANDREEV PAVEL RUSLANOVICH
  • US20240217678A1 patent drawing
  • US20240217678A1 patent drawing
  • US20240217678A1 patent drawing

AI summary

Transport equipment for moving a payload, and more specifically to systems and methods for moving a payload which are based on the use of aircraft apparatuses, self-propelled modules and payloads and also to an aircraft apparatus, self-propelled module and payload, each of which may be used in such systems and methods individually or in combination with one another. Also provided are embodiments of an aircraft apparatus, a self-propelled module and a payload which may be used in the systems and methods.