Integrated Payload Container Anchors for Parachute Delivery Assembly

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Solution Overview

Problem

Existing aerial delivery systems face challenges with high energy consumption for takeoffs and landings, limiting their range and effectiveness, and often require complex packaging that generates waste and needs skilled assembly.

Innovation Solution

A parachute system with a lightweight, recyclable canopy and attachment features, combined with a deformable payload container, allows for efficient assembly and deployment from aerial vehicles, reducing terminal velocity and minimizing waste.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If aerial vehicles carry payloads directly to delivery location, then delivery accuracy is improved, but energy consumption increases due to frequent takeoffs and landings

Engineering Contradiction:
Improvedelivery accuracyVSAvoidenergy consumption
Core Design Contradiction:
Measurement precisionVSUse of energy by moving object

Solution Approach 1:

The delivery system is divided into two independent phases: aerial transport phase (vehicle carries container) and ground delivery phase (parachute slows descent). This segmentation allows the vehicle to focus on efficient point-to-point transport while the parachute handles the final gentle delivery, reducing the need for frequent takeoffs and landings.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The parachute acts as an intermediary mechanism between the aerial vehicle and the payload. Instead of the vehicle directly placing the payload on the ground (requiring precise positioning and frequent landings), the parachute mediates the transition from aerial to ground phase, enabling safer and more energy-efficient delivery.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Reliability

If complex packaging systems are used for parachute delivery, then delivery safety is improved, but assembly complexity and waste increase

Engineering Contradiction:
Improvedelivery safetyVSAvoidassembly complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The parachute and payload container are merged into a single integrated assembly where the container serves dual purposes: protecting the payload during transport and providing attachment surfaces for the parachute. This eliminates the need for separate complex packaging systems and reduces assembly steps.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The payload container is designed with multi-functionality: it protects the payload, provides structural support, and includes integrated attachment features for the parachute. This universal design replaces multiple specialized components, simplifying the overall system while maintaining safety.

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

3Loss of substance

If reusable packaging is implemented, then waste is reduced, but assembly and disassembly time increases

Engineering Contradiction:
ImprovewasteVSAvoidassembly time
Core Design Contradiction:
Loss of substanceVSLoss of time

Solution Approach 1:

The attachment features for the parachute are pre-integrated into the container structure during manufacturing. This preliminary action eliminates the need for time-consuming on-site assembly of attachment mechanisms, allowing for rapid deployment while maintaining reusability.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The container is designed to be self-sufficient with built-in attachment features that automatically engage with the parachute system. This self-service design reduces the need for complex manual assembly procedures, enabling quick deployment and reuse without significant time loss.

Inventive Principle:
Principle #25Self-service

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

The system enables safe, controlled delivery of payloads with reduced energy consumption and waste, using a parachute that inflates to slow descent and a container that can be easily assembled and recycled.

Implementation Method 1

The parachute inflates to slow descent

Methodology Applied
Scientific EffectAir resistance: Drag

Data Source

PatentUS12479576B2Payload container for parachute delivery systems
Publication Date: 2025.11.25 ZIPLINE INTERNATIONAL INC
  • US12479576B2 patent drawing
  • US12479576B2 patent drawing
  • US12479576B2 patent drawing

AI summary

Containers and parachutes for payloads to be delivered via an aerial delivery system are disclosed. In one example, a system for aerial delivery of a payload includes a parachute having a canopy, a plurality of legs extending from the canopy, one or more attachment features arranged on an end of the legs. The system also includes a payload container with a plurality of anchors and where the plurality of anchors are integral with the payload container and receive the one or more attachment features.