Aircraft Fuel Switching for Contrail Suppression Control

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Solution Overview

Problem

Existing contrail suppression methods, such as using contrail suppressing fuel, are costly and undesirable due to increased aircraft weight, necessitating a more efficient and weight-efficient method to reduce contrail production.

Innovation Solution

A method involving alternating between two fuel compositions in an aircraft's propulsion system, using a less contrail-prone fuel for a predetermined time, monitoring for contrails, and switching back to a more contrail-prone fuel when necessary, with real-time feedback to optimize fuel use and minimize contrail formation.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Object-affected harmful factors

If contrail suppressing fuel is used to reduce contrail production, then contrail formation is suppressed, but the fuel cost increases and aircraft weight increases

Engineering Contradiction:
Improvecontrail formationVSAvoidfuel cost and weight
Core Design Contradiction:
Object-affected harmful factorsVSQuantity of substance

Solution Approach 1:

The system dynamically switches between first fuel composition (contrail-suppressing) and second fuel composition (conventional) based on real-time atmospheric conditions detected by sensors. The fuel composition is not static but adapts to changing environmental factors such as temperature, humidity, and pressure that influence contrail formation, allowing optimal contrail suppression only when atmospheric conditions are favorable.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The system changes the chemical composition parameter of the fuel being burned by switching between different fuel types. The first fuel composition has properties that suppress contrail formation (such as lower soot content or different hydrocarbon composition), while the second fuel composition is conventional aviation fuel. The control system monitors atmospheric parameters and adjusts the fuel composition parameter accordingly.

Inventive Principle:
Principle #35Parameter changes

2Object-affected harmful factors

If both conventional fuel and contrail suppressing fuel are carried on the aircraft, then contrail suppression is enabled, but the overall weight of the aircraft increases

Engineering Contradiction:
Improvecontrail suppression capabilityVSAvoidaircraft weight
Core Design Contradiction:
Object-affected harmful factorsVSWeight of moving object

Solution Approach 1:

Instead of continuously using contrail-suppressing fuel, the system applies partial action by using it only during specific time intervals when atmospheric conditions indicate contrail formation risk. The system alternates between first and second fuel compositions, using the contrail-suppressing fuel in controlled portions rather than continuously, thereby reducing the total amount needed onboard while maintaining suppression effectiveness when required.

Inventive Principle:
Principle #16Partial or excessive action

Solution Approach 2:

The system implements periodic switching between fuel compositions based on monitored atmospheric conditions. Rather than continuous use of heavy contrail-suppressing fuel, the system periodically alternates between first and second fuel types, creating a rhythmic fuel switching pattern that maintains contrail suppression capability while minimizing the weight penalty of carrying large quantities of suppressant fuel.

Inventive Principle:
Principle #19Periodic action

3Object-affected harmful factors

If contrail suppressing fuel is used continuously, then contrail production is minimized, but operational costs increase

Engineering Contradiction:
Improvecontrail productionVSAvoidfuel cost
Core Design Contradiction:
Object-affected harmful factorsVSUse of energy by moving object

Solution Approach 1:

The system employs feedback control by continuously monitoring atmospheric conditions (temperature, humidity, pressure, altitude) and using this information to adjust fuel composition selection. Sensors detect environmental parameters and feed this data back to the control system, which then determines whether to use first or second fuel composition, creating a closed-loop system that optimizes contrail suppression based on real-time conditions rather than continuous suppressant fuel use.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The system uses naturally occurring atmospheric conditions to determine when contrail suppression is necessary, rather than relying solely on predetermined flight plans or continuous suppressant application. The atmospheric sensors detect environmental factors that naturally indicate contrail formation risk, and the system responds autonomously by selecting appropriate fuel composition, allowing the environment itself to guide the suppression strategy.

Inventive Principle:
Principle #25Self-service

Data Source

PatentUS12612877B2Contrail suppression
Publication Date: 2026.04.28 AIRBUS OPERATIONS LTD
  • US12612877B2 patent drawing
  • US12612877B2 patent drawing
  • US12612877B2 patent drawing

AI summary

A method of suppressing contrails emitted by a propulsion system of an aircraft. A first fuel composition is fed into the propulsion system for a predetermined period. The expiry of the predetermined period is detected with a timer. Upon expiry of the predetermined period, a second fuel composition is fed into the propulsion system. The second fuel composition is more prone to cause contrails than the first fuel composition. Contrails generated by the propulsion system are detected as the second fuel composition is fed into the propulsion system. If a contrail is detected, the steps of the method are repeated.