Adjustable Drogue Canopy for Broad Speed Range Refueling

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Solution Overview

Problem

Current drogue systems for aerial refueling require frequent changes to accommodate different airspeeds, leading to operational delays and increased costs, as they are designed for specific speed ranges and cannot refuel aircraft flying at varying speeds without changing the drogue canopy.

Innovation Solution

A drogue system with a drogue canopy controller that adjusts the surface area of the drogue canopy based on airspeed, using a coupling, vanes, and an air data computer to modify the canopy's surface area, allowing it to operate across a broader speed range without the need for frequent changes.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If a fixed area drogue canopy is used, then the structure is simple and reliable, but the drogue can only operate at a limited speed range and requires frequent changes

Engineering Contradiction:
Improvespeed rangeVSAvoidcanopy structure
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The patent applies the dynamics principle by making the drogue canopy adjustable rather than fixed. The canopy can be configured in different states (e.g., inflated/deflated) to change its surface area, allowing it to adapt to different operating speeds. This resolves the contradiction by enabling a single canopy structure to serve multiple speed ranges, improving versatility without requiring multiple separate canopies.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The patent changes the physical parameter of the canopy's surface area to adapt to different speeds. By controlling the inflation/deflation state of the canopy, the system modifies its effective surface area parameter, allowing optimal performance across a broader speed range. This parameter change enables one canopy to replace multiple fixed-area canopies.

Inventive Principle:
Principle #35Parameter changes

2Reliability

If different drogue canopies are used for different speeds, then each canopy is optimized for its speed range, but the need to change canopies causes time loss and operational delays

Engineering Contradiction:
Improverefueling operationVSAvoidcanopy change time
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The dynamic canopy system allows the drogue to adapt its configuration during operation rather than requiring physical replacement. The canopy can be adjusted between different states to match the required operating speed, eliminating the time-consuming process of changing canopies while maintaining optimal refueling performance.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The system pre-configures the canopy in appropriate states based on anticipated operating conditions. By having the canopy ready in the correct configuration before refueling begins, the system avoids delays that would occur if canopy changes were required during operation.

Inventive Principle:
Principle #10Preliminary action

3Adaptability or versatility

If variable speed and variable drag drogues are used, then the speed range is expanded to 105-230 knots, but the projected frontal area must be manipulated which adds control complexity

Engineering Contradiction:
Improvespeed rangeVSAvoidfrontal area control
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The patent uses a flexible, inflatable canopy structure that can be easily adjusted between inflated and deflated states. This flexible membrane approach is simpler than the rigid frontal area manipulation systems used in variable drag drogues, achieving speed adaptation through a more straightforward mechanical means while maintaining the desired versatility.

Inventive Principle:
Principle #30Flexible shells and thin films

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

Enables efficient and flexible aerial refueling across a wide range of speeds, improving operational readiness and reducing operational and support costs by eliminating the need for frequent drogue changes, thus enhancing compatibility with various receiving aircraft.

Implementation Method 1

The drogue canopy is attached to the drogue structure, wherein the drogue canopy has a surface area

Methodology Applied
Scientific EffectAerodynamic drag: Drag

Data Source

PatentUS8220746B1Broad speed range inflatable drogue canopy
Publication Date: 2012.07.17 THE BOEING CO
  • US8220746B1 patent drawing
  • US8220746B1 patent drawing
  • US8220746B1 patent drawing

AI summary

A refueling system on an aircraft comprises a fuel hose coupled to the aircraft, a drogue coupled to the fuel hose, an air data computer, and a drogue canopy controller coupled to the drogue canopy. The drogue further comprises a coupling, a plurality of vanes, and a drogue canopy. The drogue canopy controller determines a selected surface area of the drogue canopy based on air speed. The drogue canopy controller is configured to modify a surface area of the drogue canopy to conform to the appropriate surface area.