Rotorcraft Asymmetric Flight Training With Simulated Engine Power

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Existing pilot training methods for rotorcraft engine failures do not effectively simulate asymmetric flight phases, leading to engine stress and potential damage, and lack a means to assess pilot progress during such simulations.

Innovation Solution

A method and system for rotorcraft flight training that simulates asymmetric flight phases by controlling engine power distribution and display, allowing pilots to experience transitions between AEO, asymmetric, and OEI modes, with simulated power displays to enhance training realism and reduce engine stress.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If pilots are trained using actual engine failure simulations with real asymmetric flight phases, then training realism and pilot skill assessment are improved, but engine stress increases and potential damage occurs

Engineering Contradiction:
Improvetraining effectivenessVSAvoidengine stress
Core Design Contradiction:
ReliabilityVSObject-affected harmful factors

Solution Approach 1:

The patent creates a virtual copy of the asymmetric flight phase experience through a simulation system. The training system reproduces the sensory and operational aspects of engine failure without actual engine shutdown, allowing pilots to practice asymmetric flight procedures on a safe virtual replica of the failure scenario.

Inventive Principle:
Principle #26Copying

Solution Approach 2:

The simulation system acts as an intermediary between the pilot and the actual engine system. It mediates the training process by providing virtual feedback and scenarios that mimic real engine failure conditions without directly stressing the physical engines, thus protecting them while maintaining training value.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Adaptability or versatility

If engines are operated in OEI mode during simulation training, then asymmetric flight training is achieved, but engine maintenance costs increase due to high stress on the operating engine

Engineering Contradiction:
Improveasymmetric flight training capabilityVSAvoidmaintenance cost
Core Design Contradiction:
Adaptability or versatilityVSEase of manufacture

Solution Approach 1:

The system creates a virtual replica of the OEI training scenario where pilots experience asymmetric flight conditions without actual engine shutdown. This virtual copy provides the same training value regarding asymmetric flight control and engine management without subjecting the physical engine to the high stress of real OEI operation.

Inventive Principle:
Principle #26Copying

Solution Approach 2:

The patent replaces the mechanical stress of actual engine failure and OEI operation with a virtual simulation system. The physical mechanical system (engines operating in high-stress OEI mode) is substituted with an informational/computational system that models the same scenarios without physical wear and tear.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

3Object-affected harmful factors

If all engines are operated simultaneously during simulated engine failure, then engine stress is reduced, but the ability to assess pilot skills in actual asymmetric flight conditions is diminished

Engineering Contradiction:
Improveengine stressVSAvoidpilot skill assessment accuracy
Core Design Contradiction:
Object-affected harmful factorsVSMeasurement precision

Solution Approach 1:

The simulation system creates a virtual copy of the asymmetric flight phase that accurately replicates the pilot workload, control inputs, and decision-making requirements of real engine failure. This virtual scenario provides precise measurement of pilot skills in asymmetric flight conditions without the compromise of running all engines simultaneously.

Inventive Principle:
Principle #26Copying

Solution Approach 2:

The system implements feedback mechanisms that provide the instructor with detailed information about pilot performance during the simulated asymmetric flight phase. This feedback includes control inputs, response times, and procedural adherence, enabling accurate skill assessment without requiring actual engine failure conditions.

Inventive Principle:
Principle #23Feedback

4Strength

If simulated asymmetric flight phases are not implemented, then engine integrity is maintained, but pilot training in asymmetric flight scenarios becomes ineffective

Engineering Contradiction:
Improveengine integrityVSAvoidtraining effectiveness
Core Design Contradiction:
StrengthVSReliability

Solution Approach 1:

The patent creates a virtual copy of the asymmetric flight training experience that preserves engine integrity while maintaining training effectiveness. The simulation reproduces all critical aspects of engine failure and asymmetric flight operations, allowing pilots to practice procedures and receive assessment without compromising physical engine strength.

Inventive Principle:
Principle #26Copying

Solution Approach 2:

The simulation system serves as an intermediary that decouples the training objective from the harmful physical effects. It mediates between the need for realistic asymmetric flight training and the need to preserve engine integrity, providing a safe intermediate environment for skill development.

Inventive Principle:
Principle #24Intermediary (Mediator)

Data Source

PatentUS12437668B2Rotorcraft flight training method, associated system and rotorcraft
Publication Date: 2025.10.07 EUROCOPTER FRANCE SA
  • US12437668B2 patent drawing
  • US12437668B2 patent drawing
  • US12437668B2 patent drawing

AI summary

A rotorcraft flight training method for a rotorcraft comprising at least two engines and at least one rotor providing lift helping to keep the rotorcraft in the air. The method comprises at least the following steps: flying the rotorcraft in a mode wherein each engine supplies driving power to the rotor; and activating a first command to start a training phase simulating asymmetric flight, the training phase comprising a first flight phase comprising a first control operation, with a controller, controlling the at least two engines and a first display operation for displaying, with a display, information carrying at least two simulated powers.