Electric Thrust Reverser Actuation via Dynamic Pressure Analysis

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Solution Overview

Problem

Existing thrust reverser systems rely on hydraulic or pneumatic actuators, which are maintenance-intensive, heavy, and prone to premature fatigue due to constant high power operation, especially during heavily loaded scenarios, leading to increased risk of jamming and component deformation.

Innovation Solution

A control method using electric motors that analyzes turbojet stream pressure parameters to adapt operating sequences, delivering only necessary power for opening or closing the thrust reverser, reducing the likelihood of high-power shocks and allowing for lighter, more reliable components by limiting torque and speed according to turbojet speed conditions.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If hydraulic or pneumatic actuators are used to actuate moving covers, then the thrust reverser can be opened or closed, but the system requires a pressurized-fluid transport network that is maintenance-intensive and prone to leaks

Engineering Contradiction:
Improvereverser operation reliabilityVSAvoidpressurized-fluid transport network complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent replaces hydraulic or pneumatic actuators with electric motors to actuate the moving covers. This substitution eliminates the need for pressurized-fluid transport networks, reducing maintenance requirements and leakage risks while maintaining the ability to open or close the thrust reverser effectively.

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

Solution Approach 2:

The patent eliminates the use of hydraulic or pneumatic systems by adopting electromechanical actuators. This removes the pressurized-fluid transport network entirely, addressing the maintenance and reliability issues associated with fluid leakage in such systems.

Inventive Principle:
Principle #29Pneumatics and hydraulics

2Reliability

If actuators deliver maximum power designed for heavily loaded scenarios, then the reverser can be opened or closed under high turbojet speed conditions, but the loads exerted on structures and equipments are always the highest loads leading to premature fatigue wear

Engineering Contradiction:
Improvereverser operation under heavily loaded conditionsVSAvoidcomponent service life
Core Design Contradiction:
ReliabilityVSDuration of action of stationary object

Solution Approach 1:

The patent implements dynamic power delivery through electric motors that adjust torque and speed based on real-time turbojet stream pressure conditions. The control method analyzes pressure parameters and adapts operating sequences, delivering only the necessary power for current conditions rather than constant maximum power, thereby reducing fatigue wear while ensuring adequate performance in heavily loaded scenarios.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The patent changes the operating parameters (torque, speed, power) of the electric motors based on analyzed turbojet stream pressure parameters. By adapting power delivery to actual operational conditions rather than maintaining fixed maximum settings, the system reduces unnecessary high loads on components while ensuring sufficient power availability when needed.

Inventive Principle:
Principle #35Parameter changes

3Weight of moving object

If electric motors are used to actuate moving covers, then the system is lighter and more reliable, but the motors must still be capable of operating under heavily laden scenarios requiring great motive power

Engineering Contradiction:
Improveactuator massVSAvoidmotive power requirement
Core Design Contradiction:
Weight of moving objectVSPower

Solution Approach 1:

The patent uses electric motors with dynamic control capabilities that can deliver high power when needed (during heavily laden scenarios) but operate at lower power levels during normal conditions. This dynamic power adjustment allows the use of lighter motors compared to those that would be required to continuously deliver maximum power, while still meeting the peak power requirements for safety-critical operations.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The patent enables the electric motors to change their operating parameters (torque, speed, power output) based on real-time analysis of turbojet stream pressure. This allows the motors to be sized for peak requirements while operating at fraction of maximum capacity during normal conditions, achieving weight reduction without compromising the ability to handle heavily laden scenarios.

Inventive Principle:
Principle #35Parameter changes

4Force

If full power is delivered each time the reverser is used, then the reverser can overcome strong depression and opposing aerodynamic forces, but the probability of component jamming increases due to high dynamic and static loads

Engineering Contradiction:
Improveforce to overcome jet depression and aerodynamic oppositionVSAvoidreverser jamming probability
Core Design Contradiction:
ForceVSReliability

Solution Approach 1:

The patent changes the power delivery parameters of the electric motors based on analyzed turbojet stream pressure conditions. By delivering appropriate power levels matched to actual operational needs rather than constant full power, the system overcomes necessary forces while reducing the probability of component jamming caused by excessive dynamic and static loads.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The patent implements a feedback control system that analyzes turbojet stream pressure parameters and adjusts motor power delivery accordingly. This feedback mechanism ensures sufficient force is applied to overcome jet depression and aerodynamic opposition while avoiding excessive power delivery that could cause component jamming, thereby improving overall system reliability.

Inventive Principle:
Principle #23Feedback

Data Source

PatentUS8151550B2Control method for actuating a thrust reverser
Publication Date: 2012.04.10 SAFRAN NACELLES
  • US8151550B2 patent drawing
  • US8151550B2 patent drawing
  • US8151550B2 patent drawing

AI summary

The invention relates to a control method for opening or closing a turbojet engine thrust reverser (1) by using at least one mobile cowl (2) displaceable by means of at least one electric motor (7) consisting in analyzing at least one parameter representative for a pressure in the turbojet engine jet and in carrying out an operating sequence in which the operating parameters of the electric motor (7) are adjusted to a situation.