Payload Extension Rack With Locking Mechanism

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Solution Overview

Problem

Current aircraft systems lack an efficient mechanism for safely extending and retracting payloads stored in a payload bay while maintaining aerodynamic performance and ensuring consistent load reaction without rotation.

Innovation Solution

A system comprising tracks attached to the upper interior surface of a payload bay and extending along the bottom surface of the aircraft wing, with a rack moveably connected via a carrier assembly and a payload actuator system for selective extension and retraction, utilizing locking mechanisms to manage load and position.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of operation

If payload is extended from payload bay along track, then payload deployment capability is improved, but aerodynamic drag increases

Engineering Contradiction:
Improvepayload deployment capabilityVSAvoidaerodynamic drag
Core Design Contradiction:
Ease of operationVSObject-generated harmful factors

Solution Approach 1:

The payload extension system is divided into segmented components: payload bay, track segments along the wing, carrier assembly, and rack. This segmentation allows the payload to be extended only when needed while maintaining aerodynamic efficiency during retraction, resolving the contradiction between deployment capability and drag reduction.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The system transitions between static (retracted) and dynamic (extended) states based on operational requirements. The payload is retracted to minimize drag during flight and extended only when deployment is required, dynamically adapting to balance aerodynamic performance with operational capability.

Inventive Principle:
Principle #15Dynamics

2Adaptability or versatility

If rack is moved along track using carrier assembly, then payload extension flexibility is improved, but system complexity increases

Engineering Contradiction:
Improvepayload extension flexibilityVSAvoidsystem complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The carrier assembly serves as an intermediary component between the track and the rack, enabling smooth movement and positioning of the payload along the track. This intermediary mechanism provides flexibility while managing system complexity by using a standardized interface that simplifies the interaction between moving parts.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Reliability

If locking mechanisms are engaged at extended and retracted positions, then load reaction stability is improved, but device complexity increases

Engineering Contradiction:
Improveload reaction stabilityVSAvoiddevice complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

Locking mechanisms are pre-positioned at specific locations along the track corresponding to extended and retracted positions. These mechanisms are engaged automatically or manually at predetermined moments during payload movement, ensuring load reaction stability without requiring continuous active control, thus balancing reliability with manageable complexity.

Inventive Principle:
Principle #10Preliminary action

Data Source

PatentUS20210309365A1System for internal payload extension and retraction with locking mechanism
Publication Date: 2021.10.07 TEXTRON INNOVATIONS INC
  • US20210309365A1 patent drawing
  • US20210309365A1 patent drawing
  • US20210309365A1 patent drawing

AI summary

A system is described and includes at least one track attached to an upper interior surface of a payload bay and extending along a bottom surface of a vehicle structure external to the payload bay, wherein the track comprises a horizontal flange; a rack moveably connected to the at least one track via at least one carrier assembly; and a payload actuator system for selectively extending the rack from the payload bay along the at least one track to a position from which payload carried by the rack may be safely deployed and retracting the rack into the payload bay along the at least one track.