Unmanned Rotorcraft With Dual Cargo Doors for Oversized Loads

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Solution Overview

Problem

Manned rotorcraft face limitations in cargo capacity and access due to the need for a human pilot and cockpit, which restricts the ability to carry oversized cargo and requires complex door configurations that hinder flight operations.

Innovation Solution

An unmanned rotorcraft design featuring dual cargo doors that can be opened or lowered to form ramps, allowing for a fully open cargo bay and enabling balanced carrying of oversized cargo without human pilots, combined with various power systems including mechanical, electrical, and hybrid configurations.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Quantity of substance

If a cockpit and human pilot are included in the rotorcraft, then the aircraft can be operated with human control, but the cargo capacity is reduced and access to oversized cargo is limited

Engineering Contradiction:
Improvecargo capacityVSAvoidcockpit configuration
Core Design Contradiction:
Quantity of substanceVSDevice complexity

Solution Approach 1:

The invention extracts and removes the cockpit and human pilot from the rotorcraft system, eliminating the space and structural constraints they impose on cargo capacity. This allows the cargo bay to extend to the forward end of the airframe, enabling oversized cargo transport without the limitations of traditional manned configurations.

Inventive Principle:
Principle #2Taking out (Extraction)

2Ease of operation

If complex door configurations are used to accommodate both cockpit and cargo, then human operation is enabled, but flight operations are hindered and loading/unloading efficiency is reduced

Engineering Contradiction:
Improveloading/unloading efficiencyVSAvoiddoor configuration
Core Design Contradiction:
Ease of operationVSDevice complexity

Solution Approach 1:

The invention segments the rotorcraft into distinct functional zones: a cockpitless forward section optimized for cargo access and a rear cargo bay. The door configuration is simplified to a single rear cargo door that can be opened or lowered to form a ramp, eliminating the need for complex multi-door arrangements required in manned aircraft.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The rear cargo door is designed to be dynamically configurable, capable of being opened horizontally or lowered to form a loading ramp. This dynamic flexibility enables efficient loading and unloading of various cargo types while maintaining structural integrity during flight, without the complexity of multiple fixed door configurations.

Inventive Principle:
Principle #15Dynamics

3Volume of moving object

If the cargo bay is restricted by cockpit space, then human pilots can operate the aircraft, but oversized cargo cannot be carried

Engineering Contradiction:
Improvecargo bay volumeVSAvoidcargo size flexibility
Core Design Contradiction:
Volume of moving objectVSAdaptability or versatility

Solution Approach 1:

By removing the cockpit from the forward end of the airframe, the invention extends the cargo bay volume to occupy the entire interior space from the rear to the forward end. This maximized volume enables the transport of oversized cargo that would not fit in traditional configurations where the cockpit occupies significant forward space.

Inventive Principle:
Principle #2Taking out (Extraction)

Data Source

PatentUS12428148B2Unmanned rotorcraft with dual cargo doors
Publication Date: 2025.09.30 TEXTRON INNOVATIONS INC
  • US12428148B2 patent drawing
  • US12428148B2 patent drawing
  • US12428148B2 patent drawing

AI summary

There is disclosed in one example an unmanned vertical lift aircraft, comprising: an airframe; a drive system configured for vertical takeoff and landing (VTOL); a power plant to power the drive system; and an internal cargo bay comprising a fore aperture and an aft aperture, the fore and aft apertures having dimensions substantially conforming to a cross section of the internal cargo bay, and the internal cargo bay comprising a substantially linear and open volume between the fore and aft apertures.