Reduced-Engine Taxi Route Annotation System

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

The complexity of factors such as weather conditions, airport procedures, and engine warm-up/cool-down durations limits the effectiveness of reduced-engine taxi operations in aircraft, reducing potential fuel savings during landing and takeoff cycles.

Innovation Solution

A system that determines a recommendation for reduced-engine taxi operations by analyzing taxi operation information and plotting a route on an airport diagram, dividing the operation into steps with and without engine use, and generating a graphical user interface to indicate fuel savings.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Loss of energy

If reduced-engine taxi operation is implemented, then fuel savings are achieved, but the complexity of multiple factors (weather, airport procedures, engine warm-up/cool-down durations) limits effectiveness and may reduce or eliminate fuel savings

Engineering Contradiction:
Improvefuel consumptionVSAvoidoperational complexity
Core Design Contradiction:
Loss of energyVSDevice complexity

Solution Approach 1:

The taxi operation is divided into multiple segments or phases, with engine operations optimized for each segment. The system identifies specific taxi routes and determines appropriate engine configurations for different portions of the journey, allowing reduced-engine operation during suitable segments while maintaining full engine operation when necessary

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The system performs preliminary analysis of taxi routes, weather conditions, airport procedures, and engine performance requirements before executing the taxi operation. By pre-determining the optimal engine configuration strategy based on advance information, the system eliminates the need for complex real-time decision-making while ensuring fuel savings are achieved

Inventive Principle:
Principle #10Preliminary action

2Loss of energy

If reduced-engine taxi operation is used, then fuel burn is reduced, but technical and operational challenges (routing constraints, SOP limitations, traffic conditions) limit the ability to implement this operation

Engineering Contradiction:
Improvefuel burnVSAvoidoperational ease
Core Design Contradiction:
Loss of energyVSEase of operation

Solution Approach 1:

The system automatically evaluates taxi routes, weather conditions, airport procedures, and traffic conditions to determine optimal engine configuration without requiring manual pilot input. The system serves itself by making the complex operational decisions, presenting pilots with pre-analyzed recommendations that simplify their workload while achieving fuel savings

Inventive Principle:
Principle #25Self-service

3Reliability

If engine warm-up and cool-down durations are extended to ensure proper operation, then engine reliability is maintained, but potential fuel savings from reduced-engine taxi operation are reduced or eliminated

Engineering Contradiction:
Improveengine reliabilityVSAvoidfuel savings
Core Design Contradiction:
ReliabilityVSLoss of energy

Solution Approach 1:

The system dynamically adjusts engine operation based on real-time and historical data about engine performance, ambient conditions, and taxi route characteristics. By optimizing the timing and duration of engine warm-up and cool-down periods based on actual conditions rather than fixed procedures, the system maintains engine reliability while minimizing the time engines must run, thereby preserving fuel savings

Inventive Principle:
Principle #15Dynamics

Data Source

PatentUS12073730B2Supporting an aircraft in a reduced-engine taxi operation
Publication Date: 2024.08.27 JEPPESEN FOREFLIGHT INC
  • US12073730B2 patent drawing
  • US12073730B2 patent drawing
  • US12073730B2 patent drawing

AI summary

A method is provided for supporting taxi operation of an aircraft. The method includes accessing information that describes a taxi operation of the aircraft at an airport, for a flight of the aircraft. The method includes determining a recommendation for reduced-engine taxi operation of the aircraft based on the information. The recommendation divides the reduced-engine taxi operation into steps including reduced-engine and all-engines steps. A route for the taxi operation is plotted on a diagram of the airport, the route is annotated with an indication of the recommendation for the taxi operation, and a graphical user interface (GUI) is generated that includes the diagram with the route and the indication of the recommendation. The indication of the recommendation includes indications of the steps into which the reduced-engine taxi operation is divided, and the route is annotated to indicate segments of the route over which the steps are performed.