Vertical Situation Display Profile Segmentation for Fuel Management

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Solution Overview

Problem

Current vertical situation displays (VSDs) in aircraft lack sufficient information for pilots to make informed decisions about intercepting the recommended vertical profile during descent and approach, leading to inefficient fuel consumption and emission management.

Innovation Solution

A system and method that provides a computed vertical profile display with intuitive symbols representing different flight path segments, allowing pilots to select and visualize markers associated with these segments, such as idle path, geometric path, airbrake segment, constant speed segment, and flight path angle, to assist in managing fuel consumption and energy profile.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Loss of information

If the VSD displays only the optimized strategic path, then the display remains simple and clear, but insufficient information is provided for pilots to make informed decisions to intercept the recommended vertical profile

Engineering Contradiction:
Improveinformation provided to pilotVSAvoiddisplay complexity
Core Design Contradiction:
Loss of informationVSDevice complexity

Solution Approach 1:

The patent segments the vertical profile information into multiple discrete elements: the optimized strategic path, intercept paths, and various flight parameters are displayed as separate but integrated components. This allows comprehensive information to be presented in an organized, non-overwhelming manner that maintains clarity while providing full situational awareness

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent adds a lateral dimension to the traditional vertical display by showing both the vertical profile and lateral intercept paths simultaneously. This multi-dimensional approach provides pilots with comprehensive spatial awareness without requiring multiple separate displays, thus increasing information density while maintaining display simplicity

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

2Adaptability or versatility

If the aircraft diverts from the recommended path due to operational situations, then operational flexibility is maintained, but fuel consumption and emissions increase

Engineering Contradiction:
Improveoperational flexibilityVSAvoidfuel consumption
Core Design Contradiction:
Adaptability or versatilityVSLoss of energy

Solution Approach 1:

The system provides continuous feedback to the pilot by displaying the recommended intercept paths and associated fuel savings. This feedback loop enables pilots to make informed decisions about path selection, allowing operational flexibility while minimizing fuel consumption through data-driven decision-making

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The patent calculates and displays multiple intercept paths in advance, along with their associated fuel consumption metrics. This preliminary preparation allows pilots to select the most efficient path before executing the maneuver, reducing overall fuel consumption while maintaining operational flexibility

Inventive Principle:
Principle #10Preliminary action

3Ease of operation

If additional information is provided on the VSD to help pilots intercept the vertical profile, then situational awareness is improved, but the display becomes more complex and difficult to interpret

Engineering Contradiction:
Improvepilot decision-makingVSAvoiddisplay information density
Core Design Contradiction:
Ease of operationVSDevice complexity

Solution Approach 1:

The patent applies local quality by providing different types of information at different locations on the display. Critical intercept paths and fuel savings information are highlighted in specific areas, while other flight parameters are displayed in less prominent locations. This selective emphasis maintains ease of operation by directing pilot attention to the most relevant information

Inventive Principle:
Principle #3Local quality

Data Source

PatentEP2950295B1System and method for economizing flight expenditures during aircraft descent and approach
Publication Date: 2017.04.12 HONEYWELL INTERNATIONAL INC
  • EP2950295B1 patent drawing
  • EP2950295B1 patent drawing
  • EP2950295B1 patent drawing

AI summary

A system and method provides situation awareness for a pilot to appropriately configure the aircraft as well as intercept the flight management system computed vertical profile in order to reduce fuel consumption, emission and better manage aircraft energy for safer operations. Markers are displayed on a vertical situation display suggesting a profile that the pilot may select involving aircraft configuration and actual flown trajectory versus the computed vertical profile, especially when aircraft is off the computed vertical profile.