Aerial Refueling Coupling With Pilot Poppet for Low Engagement Force

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Solution Overview

Problem

Aerial refueling systems require high engagement loads and high drag drogues, leading to safety concerns and potential hose damage due to high tension forces, especially during disengagement, as receiving aircraft must approach at high speeds to open the refueling coupling.

Innovation Solution

A low drag drogue and an aerial refueling coupling with a main poppet valve and pilot poppet valve configuration, where the nozzle tip opens both valves at lower speeds, reducing the force required for engagement and stabilizing the hose with a parachute-like effect, allowing for safer and lower-speed approaches.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Stability of the object's composition

If a high drag drogue is used to stabilize the hose, then the hose stability is improved, but the tension forces on the hose increase making it prone to breaking

Engineering Contradiction:
Improvehose stabilityVSAvoidtension force on hose
Core Design Contradiction:
Stability of the object's compositionVSForce

Solution Approach 1:

The patent changes the drag parameter of the drogue from high drag to low drag configuration. This parameter change reduces the tension forces on the hose while maintaining adequate stabilization through the modified drogue design, resolving the contradiction between hose stability and tension force reduction

Inventive Principle:
Principle #35Parameter changes

2Force

If the receiving aircraft approaches at high speeds to open the coupling, then the engagement force is sufficient to open the valves, but the safety risks increase

Engineering Contradiction:
Improveengagement forceVSAvoidsafety
Core Design Contradiction:
ForceVSReliability

Solution Approach 1:

The patent segments the valve opening function into two separate stages: a pilot valve that opens first at lower speeds, and a main valve that opens subsequently. This segmentation allows the receiving aircraft to approach at lower speeds while still achieving complete valve opening through the two-stage process, resolving the contradiction between sufficient engagement force and safety

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The pilot valve performs a preliminary action by opening first at lower engagement speeds, preparing the system for subsequent main valve opening. This preliminary action enables the main valve to open more easily after the initial low-speed engagement, reducing safety risks while maintaining effective fuel transfer

Inventive Principle:
Principle #10Preliminary action

3Speed

If a high drag drogue is used, then the coupling can be opened at higher speeds, but the hose becomes prone to breaking during disengagement

Engineering Contradiction:
Improveapproach speedVSAvoidhose strength
Core Design Contradiction:
SpeedVSStrength

Solution Approach 1:

The patent changes the drogue drag parameter from high to low, which modifies the tension characteristics on the hose during both engagement and disengagement phases. This parameter change reduces the risk of hose breaking while still enabling effective coupling operation at appropriate speeds

Inventive Principle:
Principle #35Parameter changes

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 reduces engagement loads and tension forces on the refueling hose, enabling safer and more stable refueling operations by allowing aircraft to approach at lower speeds, minimizing the risk of hose damage and improving safety.

Implementation Method 1

a low drag drogue disposed at a fueling end of the hose, the coupling being disposed within the drogue

Methodology Applied
Scientific EffectAerodynamic drag: Drag

Data Source

PatentUS10974842B2Low engagement force aerial refueling coupling
Publication Date: 2021.04.13 EATON INTELLIGENT POWER LTD
  • US10974842B2 patent drawing
  • US10974842B2 patent drawing
  • US10974842B2 patent drawing

AI summary

A system including a coupling (100) configured to couple a hose associated with a tanker aircraft to a nozzle associated with a receiving aircraft. The coupling may include a housing that houses a main poppet and a pilot poppet. The main poppet and the pilot poppet may control fuel flow from the tanker aircraft to the receiving aircraft. The coupling may also include an opening disposed at a first side of the housing. The opening may receive the fuel nozzle. An orifice may be disposed on a second side of the housing, the orifice may permit fuel to flow into the housing. The system may also include a low drag drogue configured to house the coupling. The system may also include a nozzle tip configured to open the pilot poppet and the main poppet, wherein fuel flows to the receiving aircraft in response to the main poppet being open.