U-Shaped Leaf Spring for Aircraft Thrust Reverser Shutter

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Solution Overview

Problem

Existing springs for thrust reverser shutters in aircraft turbojet engines are heavy and do not optimize elastic behavior for a given mass, failing to adequately compensate for tolerance deviations and structural deformations.

Innovation Solution

A U-shaped leaf spring with tapered sections and fork-shaped ends, made from titanium alloy or composite materials, which reduces mass and weight while maintaining effective elastic behavior and structural support by eliminating the need for additional bearing pieces.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Weight of moving object

If traditional helical or blade springs are used for thrust reverser shutters, then the spring can provide necessary elastic behavior and compensate for tolerance deviations, but the spring mass is excessive

Engineering Contradiction:
Improvespring massVSAvoidelastic behavior
Core Design Contradiction:
Weight of moving objectVSReliability

Solution Approach 1:

The spring is divided into two distinct branches (first and second branches) that are interconnected, allowing each branch to be optimized independently for weight reduction while maintaining overall elastic functionality

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The spring adopts a U-shaped configuration with curved branches instead of traditional helical or blade forms, reducing mass while maintaining elastic behavior through the curved geometry that distributes bending moments more efficiently

Inventive Principle:
Principle #14Spheroidality (Curvature)

2Weight of moving object

If the spring branches have uniform section throughout their length, then the structure is simple to manufacture, but the mass cannot be reduced

Engineering Contradiction:
Improvespring massVSAvoidmanufacturing complexity
Core Design Contradiction:
Weight of moving objectVSEase of manufacture

Solution Approach 1:

The spring branches feature varying cross-sections along their length, with different sections optimized for their specific functional requirements, allowing mass reduction in less critical areas while maintaining strength where needed

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The cross-sectional parameters of the spring branches are varied along their length to optimize the strength-to-weight ratio, with sections designed to have different thicknesses or widths based on local stress requirements

Inventive Principle:
Principle #35Parameter changes

3Weight of moving object

If additional bearing pieces are added to support the connecting rod, then the structural support is improved, but the overall mass increases

Engineering Contradiction:
Improveoverall massVSAvoidbearing support
Core Design Contradiction:
Weight of moving objectVSStrength

Solution Approach 1:

The bearing function is integrated directly into the spring structure through returns formed in the mass of the spring, eliminating the need for separate bearing pieces and reducing overall mass while maintaining structural support

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The spring structure serves multiple functions simultaneously: providing elastic behavior for tolerance compensation, structural support for the connecting rod, and bearing support through integrated returns, eliminating the need for separate components

Inventive Principle:
Principle #6Universality (Multi-functionality)

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 U-shaped leaf spring achieves a significant weight reduction of up to 1800 grams per thrust reverser, improving elastic performance and reducing material costs, while maintaining sufficient pressure on flaps to ensure proper operation.

Implementation Method 1

the ends of this spring are subjected to weak or zero bending moments, which allows to have a spring which, for a given mass, has a better elastic behavior

Methodology Applied
Scientific EffectElasticity: Elasticity

Data Source

PatentEP2179194B8Spring for a cascade-type thrust reverser shutter for an aircraft jet engine
Publication Date: 2014.01.08 AIRCELLE SA

AI summary

This leaf spring (17) for a thrust reverser shutter (13) is noteworthy in that it has two branches (19, 21) defining a U shape, the ends (19a, 19b, 21a, 21b) of these branches being able to cooperate respectively with a shutter (13) of said reverser and with a link (15) for actuating this shutter.