Thrust Reverser Pivoting Doors Sliding Rear Shell Ring

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Solution Overview

Problem

Conventional thrust reversers with pivoting doors and fixed or movable rear shell rings face constraints such as increased mass, reduced thrust reversal performance, and complex actuation systems, which hinder efficient counter-thrust generation and flight performance.

Innovation Solution

A thrust reverser design featuring a fixed structure with a movable rear shell ring and a simplified actuation system using tie rods to synchronize the movement of doors and the ring, reducing the mass and complexity of the actuation system while enhancing flight performance.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Device complexity

If a fixed rear shell ring is used, then the structure is simple, but the doors must collide with it during opening requiring reduced distance between rotation axis and rear, increasing girder dimension and reducing thrust reversal performance

Engineering Contradiction:
Improvestructure simplicityVSAvoidthrust reversal performance
Core Design Contradiction:
Device complexityVSProductivity

Solution Approach 1:

The rear shell ring is made movable instead of fixed, allowing it to translate in the longitudinal direction during door operation. This dynamic adjustment enables the ring to move away from the door path during opening, eliminating the need for door-girder collisions and allowing optimized door dimensions for better thrust reversal performance.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The actuation system is segmented into two independent tie rods: one connecting the actuator to the door for pivoting, and another connecting the actuator to the rear shell ring for translation. This segmentation allows independent control of door and ring movements while maintaining synchronization through the common actuator.

Inventive Principle:
Principle #1Segmentation

2Device complexity

If a fixed rear shell ring is used, then the structure is simple, but the opening angle of doors is limited requiring increased door and nacelle length, increasing mass

Engineering Contradiction:
Improvestructure simplicityVSAvoidpropulsion unit mass
Core Design Contradiction:
Device complexityVSWeight of moving object

Solution Approach 1:

The movable rear shell ring translates longitudinally to create additional space during door opening, enabling larger door opening angles without increasing door or nacelle length. This maintains compact dimensions and reduces mass while achieving satisfactory counter-thrust flow cross-section.

Inventive Principle:
Principle #15Dynamics

3Adaptability or versatility

If conventional movable rear shell ring reversers are used, then door geometry constraints are resolved, but the actuation system becomes complex and bulky

Engineering Contradiction:
Improvedoor geometry flexibilityVSAvoidactuation system complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

Both the door pivoting and rear shell ring translation are driven by the same actuator through two tie rods. This merging of actuation functions into a single actuator reduces the number of actuators from multiple independent ones to one, significantly simplifying the actuation and control system.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The tie rods serve as intermediary mechanical elements that transmit the actuator's linear motion to both the door (for pivoting) and the rear shell ring (for translation). This intermediary mechanism enables coordinated movement of multiple components through a single actuator, reducing system complexity.

Inventive Principle:
Principle #24Intermediary (Mediator)

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

The solution simplifies the actuation system, reduces the mass of the reverser, and improves thrust reversal performance by synchronizing the movement of doors and the ring, thereby enhancing both direct and reverse thrust configurations.

Implementation Method 1

an actuator configured to move the door between a closed position in which the door forms a trailing edge of the propulsion unit and an open position in which the door is positioned to redirect a fluid flow towards a front of the propulsion unit

Methodology Applied
Scientific EffectMechanical Force: Mechanical Force

Implementation Method 2

a second tie rod having a first end connected to the movable element of the actuator and a second end connected to the ring, the second tie rod being configured to translate the ring in response to movement of the actuator

Methodology Applied
Scientific EffectMechanical Force: Mechanical Force

Implementation Method 3

means for guiding the ring between the forward and retracted positions

Methodology Applied
Scientific EffectMechanical Constraint: Mechanical Force

Data Source

PatentUS20240200507A1Thrust reverser comprising pivoting doors and a sliding rear shell ring
Publication Date: 2024.06.20 SAFRAN NACELLES
  • US20240200507A1 patent drawing
  • US20240200507A1 patent drawing
  • US20240200507A1 patent drawing

AI summary

A thrust reverser including doors, a rear shell ring and an actuation system for synchronising the pivoting of the doors and the translation of the rear shell ring.