Auto Rotating Canister Descent Control via Dynamic Rotor Pitch

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Solution Overview

Problem

Existing air drop canister systems are highly visible, slow, and difficult to control, leading to damage of supplies due to uncontrolled descent and centrifugal forces, making them impractical for military and emergency applications.

Innovation Solution

An auto-rotating canister (ARC) with a controllable rotor system, including electric motors and servomechanisms, is designed to slow descent and control direction via auto-rotation, using GPS and autopilot systems for precise landing, and can be scaled for various mission requirements.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of operation

If a bladed rotor is used to control descent, then descent control capability is improved, but centrifugal force causes damage to supplies and equipment

Engineering Contradiction:
Improvedescent control capabilityVSAvoidcentrifugal force damage
Core Design Contradiction:
Ease of operationVSObject-affected harmful factors

Solution Approach 1:

The rotor system dynamically adjusts blade pitch angles during descent to control rotation speed and direction, transforming from a static structure to an actively controlled dynamic system that adapts to changing descent conditions while maintaining cargo safety

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The system changes operational parameters by varying blade pitch angles and rotation speeds to optimize descent control, allowing precise control of descent rate and horizontal movement while preventing excessive centrifugal forces that could damage supplies

Inventive Principle:
Principle #35Parameter changes

2Measurement precision

If mechanical and electrical control systems are added to the rotor, then descent control precision is improved, but system cost increases making it unsuitable for single use applications

Engineering Contradiction:
Improvedescent control precisionVSAvoidsystem cost
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The rotor system uses automatic control algorithms that process sensor data and adjust blade pitches without requiring complex external control systems, enabling the system to self-regulate its descent trajectory and reduce dependency on expensive mechanical control mechanisms

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The invention replaces complex mechanical control systems with electronic sensors and computer-based control algorithms that can achieve superior precision with fewer moving parts, reducing overall system complexity and cost while improving control accuracy

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

3Device complexity

If parachute drop is used for supply delivery, then simplicity is maintained, but visibility to enemy forces increases and landing control is lost

Engineering Contradiction:
Improvesystem simplicityVSAvoidlanding control
Core Design Contradiction:
Device complexityVSEase of operation

Solution Approach 1:

The system transitions from the static, passive parachute configuration to a dynamic rotor-controlled descent system that can actively adjust its trajectory, providing landing control while maintaining relative simplicity through automated control

Inventive Principle:
Principle #15Dynamics

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 ARC enables precise and controlled delivery of supplies by reducing descent velocity and preventing container rotation, thus protecting contents and allowing for reusable and environmentally friendly deployment.

Implementation Method 1

a bladed rotor operably coupled to the container through a rotor arm

Methodology Applied
Scientific EffectAerofoil: Aerofoil

Implementation Method 2

The ARC includes a top-plate assembly configured to support electronic systems or portions thereof

Methodology Applied
Scientific EffectDrag: Drag

Implementation Method 3

The rotor arm is hingedly connected to the container and configured to pivot to deploy the bladed rotor from a stowed position during free fall

Methodology Applied
Scientific EffectFree Fall: Free Fall

Data Source

PatentUS11518515B1Auto rotating canister
Publication Date: 2022.12.06 THE GOVERNMENT OF THE UNITED STATES AS REPRESENTED BY THE SECRETARY OF THE AIR FORCE
  • US11518515B1 patent drawing
  • US11518515B1 patent drawing
  • US11518515B1 patent drawing

AI summary

An apparatus for air dropping equipment and supplies from an aircraft is disclosed herein. The apparatus includes a canister having a rotor system configured to slow the descent at a predetermined altitude to a desired landing speed via auto-rotation and/or with motor assist. The rotor system is configured to prevent the container from spinning about its longitudinal axis during the descent.