Fuselage Door Assembly With Sliding Panels for Secure Aerial Delivery

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Solution Overview

Problem

Conventional aerial vehicles face issues with poor aerodynamic performance due to non-aerodynamic delivery goods or receptacles, limited range and payload capacity, security concerns from detachable goods, manual handling, and inability to deliver to multiple locations securely.

Innovation Solution

A door assembly with complementary door pieces actuated by a transmission member for automated pick-up, transport, and delivery of goods, ensuring secure containment and conformity with the fuselage, allowing for automated delivery to multiple recipients.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Productivity

If delivery goods are carried externally on conventional aerial vehicles, then pick-up and delivery can be performed, but aerodynamic performance deteriorates due to non-aerodynamic shapes increasing drag and turbulence

Engineering Contradiction:
Improvedelivery capabilityVSAvoidaerodynamic drag
Core Design Contradiction:
ProductivityVSObject-affected harmful factors

Solution Approach 1:

The door assembly is nested within the fuselage structure, with door pieces that slide along the fuselage surface. When closed, the door assembly integrates seamlessly with the fuselage contours, maintaining aerodynamic performance while providing access for delivery operations.

Inventive Principle:
Principle #7Nested doll (Nesting)

Solution Approach 2:

The door assembly features movable door pieces that can dynamically open and close. During flight, the doors remain closed to maintain aerodynamic efficiency, and only open during automated delivery operations at designated locations, thus minimizing the impact on aerodynamic performance.

Inventive Principle:
Principle #15Dynamics

2Adaptability or versatility

If detachable external receptacles are used for delivery goods, then flexibility in delivery operations is improved, but security deteriorates as goods may become detached during transportation or be susceptible to thievery

Engineering Contradiction:
Improvedelivery flexibilityVSAvoidgoods security
Core Design Contradiction:
Adaptability or versatilityVSReliability

Solution Approach 1:

The door assembly provides a nested, integrated access system within the fuselage rather than using external detachable receptacles. Goods are contained within the secured fuselage interior and accessed through the controlled door mechanism, preventing unauthorized access and accidental detachment while maintaining delivery flexibility.

Inventive Principle:
Principle #7Nested doll (Nesting)

Solution Approach 2:

The automated door mechanism acts as an intermediary between the secured cargo hold and the external environment. It controls access to delivery goods through automated opening and closing operations, ensuring security while enabling flexible delivery to multiple locations without requiring manual handling or detachable external containers.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Device complexity

If manual handling is used for loading delivery goods, then device complexity is reduced, but productivity deteriorates due to time-consuming manual operations

Engineering Contradiction:
Improvesystem simplicityVSAvoidloading speed
Core Design Contradiction:
Device complexityVSProductivity

Solution Approach 1:

The door assembly is equipped with an automated actuation system that opens and closes doors without manual intervention. The transmission member mechanism automatically positions and secures door pieces during delivery operations, enabling the system to serve itself and eliminating time-consuming manual handling while maintaining operational simplicity.

Inventive Principle:
Principle #25Self-service

4Ease of manufacture

If conventional door assemblies with large clearance are used, then ease of manufacture is improved, but aerodynamic performance deteriorates due to gaps and poor conformity with fuselage

Engineering Contradiction:
Improvedoor assembly fabricationVSAvoidaerodynamic turbulence
Core Design Contradiction:
Ease of manufactureVSObject-affected harmful factors

Solution Approach 1:

The door pieces are designed with specific local geometric features including curved surfaces and contoured edges that match the fuselage profile at each installation location. This local adaptation ensures aerodynamic conformity where the door assembly interfaces with the fuselage, minimizing turbulence and drag while maintaining manufacturability through standardized components.

Inventive Principle:
Principle #3Local quality

Data Source

PatentUS12479564B2Door assembly for a fuselage of an aerial vehicle
Publication Date: 2025.11.25 CHU WEI KEONG
  • US12479564B2 patent drawing
  • US12479564B2 patent drawing
  • US12479564B2 patent drawing

AI summary

A door assembly for a fuselage of an aerial vehicle is described, including a pair of complementary door pieces, and an actuation mechanism that includes a first transmission member. The first transmission member actuates either one or both door pieces for portions thereof to be in a sliding action with respect to the fuselage while maintaining close conformity thereto as either one or both of them are actuated to either meet or separate. Further disclosed are various embodiments of the door assembly, and a related aerial vehicle and system for delivering goods.