UAV Payload Attachment Using Vacuum Suction for Versatile Surface Deployment

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Solution Overview

Problem

Existing UAV payload attachment systems are limited in their ability to attach to a wide range of surfaces, including those at various angles, and require complex control systems to maintain payload support, which is beyond the capability of typical commercial off-the-shelf UAVs, and often rely on magnetic properties, restricting surface types and increasing risk in environments like high winds.

Innovation Solution

A UAV system with a payload deployment system comprising a payload attachment system that uses suction, adhesion, and Van der Waals forces, along with motors and a vacuum system to attach payloads to surfaces, allowing for orientation and secure attachment at various angles, and a decoupling system that enables the UAV to move freely while the payload remains attached, and a detachment system that safely releases the payload from the surface.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of manufacture

If magnetic attachment systems are used, then payload attachment is simplified, but surface type restrictions increase and reliability decreases in high winds

Engineering Contradiction:
Improveattachment system simplicityVSAvoidsurface type compatibility
Core Design Contradiction:
Ease of manufactureVSAdaptability or versatility

Solution Approach 1:

The patent replaces magnetic attachment mechanisms with a vacuum-based mechanical attachment system. The vacuum system uses a vacuum cup that creates suction to adhere to surfaces, eliminating the need for magnetic properties in either the attachment system or the surface. This substitution enables attachment to non-magnetic surfaces while maintaining simplicity in the attachment mechanism.

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

Solution Approach 2:

The patent changes the attachment mechanism from magnetic force to vacuum suction. By controlling the vacuum level within the vacuum cup, the system can adjust the attachment force to accommodate different surface types and environmental conditions. This parameter change allows the same attachment system to work on diverse surfaces without relying on magnetic properties.

Inventive Principle:
Principle #35Parameter changes

2Reliability

If complex control systems are used to maintain payload support, then payload attachment reliability improves, but device complexity increases

Engineering Contradiction:
Improvepayload support stabilityVSAvoidcontrol system complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The vacuum-based attachment system is inherently self-regulating. The vacuum cup automatically maintains attachment through continuous vacuum maintenance, and the system can self-adjust to minor disturbances without requiring complex active control mechanisms. The physical design of the vacuum cup and its mounting allows it to self-correct positioning and maintain attachment force.

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The patent uses a vacuum (negative pressure) system to provide attachment force, which is simpler and more reliable than active mechanical or magnetic control systems. The vacuum maintenance system provides passive, stable attachment without requiring complex sensors or actuators to regulate payload support, thereby reducing overall system complexity while maintaining reliability.

Inventive Principle:
Principle #29Pneumatics and hydraulics

3Manufacturing precision

If payload is fully supported by UAV during attachment, then attachment precision improves, but UAV maneuverability decreases

Engineering Contradiction:
Improvepayload positioning accuracyVSAvoidUAV maneuverability
Core Design Contradiction:
Manufacturing precisionVSEase of operation

Solution Approach 1:

The patent segments the payload support function into two parts: the UAV provides positioning and orientation, while the vacuum attachment system provides mechanical support and stabilization. This segmentation allows the UAV to maneuver freely during approach and positioning, then transfers support to the vacuum cup at the landing site, improving both positioning accuracy and maneuverability.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The UAV performs preliminary positioning and orientation maneuvers to align the payload with the landing site before actual attachment occurs. Once the vacuum cup is positioned and sealed to the surface, the payload is fully supported by the attachment system, allowing the UAV to be released or repositioned independently. This preliminary action sequence enables precise positioning without compromising UAV maneuverability during the attachment process.

Inventive Principle:
Principle #10Preliminary action

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

Enables secure and versatile attachment of payloads to diverse surfaces, including non-magnetic surfaces at various angles, while allowing the UAV to move freely, improving safety and reducing complexity in control systems, making it suitable for commercial off-the-shelf UAVs.

Implementation Method 1

generating a vacuum by the vacuum system to cause the payload to attach to the landing site

Methodology Applied
Scientific EffectVacuum: Vacuum

Implementation Method 2

uses suction, adhesion, and Van der Waals forces

Methodology Applied
Scientific EffectSuction: Suction

Implementation Method 3

uses suction, adhesion, and Van der Waals forces

Methodology Applied
Scientific EffectAdhesion: Adhesive

Implementation Method 4

uses suction, adhesion, and Van der Waals forces

Methodology Applied
Scientific EffectVan der Waals force: Van der Waals Force

Data Source

PatentUS20240409212A1Payload deployment using a UAV and related systems, devices, and methods
Publication Date: 2024.12.12 NIRICSON SOFTWARE INC
  • US20240409212A1 patent drawing
  • US20240409212A1 patent drawing
  • US20240409212A1 patent drawing

AI summary

An embodiment of an unmanned-aerial-vehicle (UAV) system includes a UAV, a payload deployment system, and a payload. The payload deployment system includes a payload attachment system, a payload decoupling system, and, optionally, a payload detachment system. The payload attachment system is configured to attach the payload at a landing site such that the payload is at least partially supported at the landing site. The payload decoupling system is configured to decouple the payload from the UAV such that the UAV can move within a range of motions while the payload remains attached at the landing site. The payload attachment system can be configured to generate a vacuum to cause the payload to attach to the landing site. And the payload decoupling system can include an umbilical that can include a vacuum hose.