Aerial Refueling Boom Braking Apparatus for Anomalous Extension Control

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Solution Overview

Problem

Aerial refueling boom systems experience anomalous extensions due to hydraulic system malfunctions, leading to loss of control during refueling operations.

Innovation Solution

A braking apparatus with a pulley and lock mechanism that prevents rotation of the second tube relative to the first tube by engaging calipers or a pin when the hydraulic actuation source performance is reduced, ensuring controlled extension and retraction of the refueling boom.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of operation

If a hydraulic system is used to control boom extension and retraction, then the boom can be controllably extended and retracted during refueling operations, but the system may experience anomalous extensions due to hydraulic component malfunctions

Engineering Contradiction:
Improveboom controlVSAvoidboom position control
Core Design Contradiction:
Ease of operationVSReliability

Solution Approach 1:

The braking apparatus applies a counteracting force to the hydraulic actuation system by engaging brake calipers that frictionally contact the pulley, preventing anomalous boom extensions caused by hydraulic component malfunctions such as stuck valves or pressure leaks

Inventive Principle:
Principle #9Preliminary anti-action

Solution Approach 2:

The braking apparatus serves as an intermediary safety mechanism between the hydraulic actuation source and the boom tubes, using a pulley-cable-brake assembly to detect and respond to anomalous hydraulic pressure conditions that could cause uncontrolled boom movement

Inventive Principle:
Principle #24Intermediary (Mediator)

2Reliability

If a braking apparatus is added to prevent anomalous extensions, then boom control reliability is improved during hydraulic system failures, but the device complexity increases

Engineering Contradiction:
Improveboom position controlVSAvoidhydraulic system components
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The braking apparatus is designed to automatically engage and disengage based on hydraulic pressure conditions without requiring external control signals, using the hydraulic system's own pressure fluctuations to trigger the safety mechanism

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The braking apparatus utilizes hydraulic pressure differential detection to control the engagement of brake calipers, employing hydraulic actuators that respond to pressure anomalies in the boom extension/retraction system

Inventive Principle:
Principle #29Pneumatics and hydraulics

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 braking apparatus effectively reduces or eliminates anomalous extensions, maintaining control over the refueling boom even during actuation source performance degradation, thereby ensuring safe and controlled refueling operations.

Implementation Method 1

The lock may also include a spring configured to actuate the pin and to move the pin from the open position to the actuated position

Methodology Applied
Scientific EffectElasticity: Elasticity

Implementation Method 2

The actuation source comprises a hydraulic pressure source, wherein the lock further comprises a housing in which the spring and the pin are disposed

Methodology Applied
Scientific EffectHydraulic pressure: Hydraulic Press

Implementation Method 3

a cable wraps at least partially thereabout, wherein the pulley is operably mounted to the first tube and configured to rotate in response to movement of the second tube relative to the first tube

Methodology Applied
Scientific EffectFriction: Friction

Data Source

PatentEP2603429B1Braking apparatus and method for an aerial refueling boom system
Publication Date: 2017.11.29 THE BOEING CO
  • EP2603429B1 patent drawingFigure 1
  • EP2603429B1 patent drawingFigure 2
  • EP2603429B1 patent drawingFigure 3~4

AI summary

A braking apparatus of an aerial refueling boom system is provided to reduce the likelihood of or to prevent anomalous boom extension. The braking apparatus includes a pulley about which a cable wraps. The pulley is configured to be operably mounted to a first tube of the boom system and to rotate in response to movement of a second tube relative to the first tube as a result of the connection of the cable to the second tube. The braking apparatus also includes a lock, such as a brake or a pin lock, having open and actuated positions. In the actuated position, rotation of the pulley and movement of the second tube relative to the first tube are prevented. The lock is configured to be actuated by a reduction in performance of an actuation source that otherwise controls the relative positions of the first and second tubes.