Optical Microdrone Antenna Layout for Nanoparticle Trapping and Transport

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Existing methods for trapping and transporting nanoparticles face limitations due to the diffraction limit and lack of precise control over nanoparticle orientation, requiring high spatial control over light fields and specialized environments.

Innovation Solution

A microdrone system with antenna structures that scatter circularly polarized light to provide propulsion and trapping forces, allowing for precise control over nanoparticle transport and orientation using a single light source or multiple sources at different wavelengths.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If optical tweezers are used for nanoparticle transport, then trapping capability is achieved, but spatial control precision deteriorates due to diffraction limit

Engineering Contradiction:
Improvespatial control precisionVSAvoidlight field control complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The patent divides the optical control function into separate antenna structures: motion-promoting antenna structures for propulsion and trapping-field-promoting antenna structures for particle trapping. This segmentation allows each component to be optimized independently, achieving sub-micrometer spatial precision without requiring complex overall light field control.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

Different regions of the microdrone are assigned different functions through localized antenna structures. The motion-promoting antenna structures are positioned to generate propulsion forces, while trapping-field-promoting antenna structures are positioned to create trapping potentials. This local functional differentiation enables precise control of nanoparticle position and orientation.

Inventive Principle:
Principle #3Local quality

2Measurement precision

If techniques to induce particle rotation using circularly polarized light are used, then nanoparticle orientation control is achieved, but spatial control requirements worsen

Engineering Contradiction:
Improvenanoparticle orientation controlVSAvoidspatial control over light field
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The microdrone system performs self-propulsion and self-orientation using antenna structures that interact with circularly polarized light. The motion-promoting antenna structures generate forces that automatically orient the microdrone and transport the nanoparticle without requiring external complex light field manipulation, thus reducing spatial control requirements.

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The patent replaces complex mechanical or multi-component optical systems with a simplified antenna-based optical-mechanical coupling system. The antenna structures convert optical momentum directly into mechanical propulsion and orientation forces, eliminating the need for complex light field spatial control while achieving precise nanoparticle orientation.

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

3Measurement precision

If plasmonic holograms are used for subwavelength positioning, then positioning precision is improved, but spatial range deteriorates

Engineering Contradiction:
Improvesubwavelength positioning precisionVSAvoidspatial range
Core Design Contradiction:
Measurement precisionVSArea of stationary object

Solution Approach 1:

The patent employs dynamic control of the microdrone's antenna structures in response to incident light. The motion-promoting antenna structures can be configured to generate propulsion forces in different directions, and the trapping-field-promoting structures can adjust their trapping potential dynamically. This dynamic adaptability enables the system to achieve subwavelength positioning precision while maintaining a large operational spatial range.

Inventive Principle:
Principle #15Dynamics

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 precise, non-destructive transport and trapping of nanoparticles with sub-micrometer accuracy, independent of light polarization, using moderate illumination intensity and enabling predefined nanoparticle orientation.

Implementation Method 1

Each of the first and the second motion-promoting antenna structures is adapted to scatter incoming, circularly polarized light at the respective first resonance wavelength such that at least a fraction of a momentum of the incoming, circularly polarized light is transferred to the microdrone

Methodology Applied
Scientific EffectLight scattering: Scattering

Implementation Method 2

at least a fraction of a momentum of the incoming, circularly polarized light is transferred to the microdrone

Methodology Applied
Scientific EffectMomentum transfer: Conservation of Momentum

Implementation Method 3

The trapping-field-promoting antenna structure is adapted to provide, under illumination with incoming light at the second wavelength, a gradient force directed at the trapping-field promoting antenna structure

Methodology Applied
Scientific EffectOptical gradient force: Optical Tweezers

Data Source

PatentEP4685533A1Microdrone, microdrone system, use of the microdrone or of the microdrone system for trapping and transporting a particle, and method of fabricating a microdrone
Publication Date: 2026.01.28 JULIUS MAXIMILIANS UNIV WURZBURG
  • EP4685533A1 patent drawingFigure 1~3b
  • EP4685533A1 patent drawingFigure 4a~6d
  • EP4685533A1 patent drawingFigure 7~9

AI summary

A microdrone is adapted to, selectively under illumination, trap and transport a particle. The microdrone comprises a plurality of motion-promoting antenna structures and a trapping-field-promoting antenna structure. The plurality of motion-promoting antenna structures comprises a first motion-promoting antenna structure and a second motion-promoting antenna structure. Each of the first and the second motion-promoting antenna structures exhibits a respective optically addressable resonance at a respective first resonance wavelength. Each of the first and the second motion-promoting antenna structures is adapted to scatter incoming, circularly polarized light at the respective first resonance wavelength such that at least a fraction of a momentum of the incoming, circularly polarized light is transferred to the microdrone. The trapping-field-promoting antenna structure exhibits an optically addressable resonance at a second resonance wavelength. The trapping-field-promoting antenna structure is adapted to provide, under illumination with incoming light at the second wavelength, a gradient force directed at the trapping-field promoting antenna structure both for left-handed circularly polarized incoming light at the second wavelength and for right-handed circularly polarized incoming light at the second wavelength.