Morphing UAV Wings and Tail for Urban Camouflage

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Solution Overview

Problem

Conventional UAVs are difficult to deploy in urban environments without detection, as their distinct aircraft shape makes them easily identifiable, reducing their effectiveness in surveillance and reconnaissance missions.

Innovation Solution

The development of morphing UAVs that can transform into common objects, such as beverage containers, allowing wings and rotors to extend and retract seamlessly, maintaining a non-aircraft appearance and avoiding detection by blending in with the environment.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Object-affected harmful factors

If conventional UAVs are used with fixed aircraft shape, then flight capability is maintained, but detection risk increases in urban environments

Engineering Contradiction:
Improvedetection riskVSAvoidenvironmental adaptability
Core Design Contradiction:
Object-affected harmful factorsVSAdaptability or versatility

Solution Approach 1:

The UAV employs dynamically transformable components including extendable/retractable wings, tail, and propeller that can change configuration between flight mode and camouflage mode. The fuselage can transform between cylindrical and rectangular shapes, allowing the UAV to adapt its appearance to match different environmental contexts and avoid detection.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The UAV utilizes shape memory alloys and variable geometry mechanisms to change its physical parameters including overall shape, surface area, and structural configuration. These parameter changes enable the UAV to transition between distinct morphological states for flight and for blending into urban environments.

Inventive Principle:
Principle #35Parameter changes

2Speed

If UAV components are extended for flight, then flight performance is improved, but detectability increases

Engineering Contradiction:
Improveflight performanceVSAvoiddetectability
Core Design Contradiction:
SpeedVSDifficulty of detecting and measuring

Solution Approach 1:

The UAV is divided into separable functional components (wings, tail, propeller, fuselage) that can be independently extended or retracted. This segmentation allows the aircraft to expose only the necessary components for flight while keeping other parts concealed, optimizing the balance between flight performance and stealth.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The retractable components are designed to nest within or conform to the fuselage when not in use. The wings, tail, and propeller can be stored within the cylindrical fuselage configuration, creating a compact non-aircraft appearance that reduces detectability when flight capability is not required.

Inventive Principle:
Principle #7Nested doll (Nesting)

3Adaptability or versatility

If morphing mechanisms are added to UAV, then camouflage capability is enhanced, but device complexity increases

Engineering Contradiction:
Improvecamouflage capabilityVSAvoidstructural complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The morphing mechanisms serve multiple functions: they enable shape transformation for camouflage, provide structural support for flight components, and facilitate compact storage. The cylindrical fuselage serves both as the camouflage shape and as the structural backbone that houses all mechanical systems.

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

Solution Approach 2:

The UAV employs flexible or transformable surface structures that can change the external shape of the fuselage between cylindrical and rectangular configurations. These flexible shells allow the UAV to adapt its silhouette to match environmental forms while maintaining structural integrity.

Inventive Principle:
Principle #30Flexible shells and thin films

Data Source

PatentUS8888035B2Morphing aircraft
Publication Date: 2014.11.18 UNIV OF FLORIDA RESEARCH FOUNDATION INC
  • US8888035B2 patent drawing
  • US8888035B2 patent drawing
  • US8888035B2 patent drawing

AI summary

A morphing aircraft that is achieves multi-modality location and camouflage for payload emplacement The morphing aircraft includes a substantially cylindrical fuselage including a shape configured as a packaging container with a first end and a second end A set of wings is coupled to the fuselage The set of wings includes a first position where the set of wings is extended outwards from the fuselage and a second position where the set of wings is retracted inwards towards the fuselage A tail is coupled to the second end of the cylindrical fuselage The tail includes a first position where the tail is extended outward from the fuselage and a second position where the tail is retracted inward towards the fuselage A propeller is mounted to the first end of the fuselage An engine is mechanically coupled to the propeller The engine is enclosed within the fuselage and powers the propeller.