Ejection Jack Release Mechanism for Ram Air Turbine Deployment

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Solution Overview

Problem

Existing ram air turbine deployment mechanisms lack an efficient and reliable release mechanism for transitioning from a stowed to a deployed position, particularly in aircraft emergency power scenarios, where precise and controlled deployment is critical.

Innovation Solution

A release mechanism incorporating a locking mechanism with pivotable legs, a blocking pin, and solenoids that exert force to pivot the legs away from the solenoid, allowing the blocking pin to clear the locking mechanism, enabling the ram air turbine to deploy effectively.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If a locking mechanism with blocking pin is used to secure the ram air turbine in stowed position, then the reliability of secure storage is improved, but the complexity of the release mechanism increases

Engineering Contradiction:
Improvereliability of secure storageVSAvoidcomplexity of release mechanism
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The release mechanism is divided into separate functional components: pivotable legs for movement, a blocking pin for locking, and solenoids for actuation. This segmentation allows each component to perform its specific function efficiently while maintaining overall system reliability and controlled complexity.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent replaces manual or complex mechanical release operations with solenoid actuation. The solenoids provide reliable, controlled electromagnetic actuation that simplifies the release operation while maintaining the mechanical locking mechanism's reliability during storage.

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

2Ease of operation

If solenoids are used to pivot the legs and clear the blocking pin, then the ease of operation is improved, but the use of energy increases

Engineering Contradiction:
Improveease of deployment operationVSAvoidenergy consumption of solenoids
Core Design Contradiction:
Ease of operationVSUse of energy by moving object

Solution Approach 1:

The solenoids are activated in a controlled sequence during deployment: first to pivot the legs, then to clear the blocking pin. This periodic, staged actuation ensures reliable operation while minimizing total energy consumption by activating solenoids only when and where needed, rather than continuously.

Inventive Principle:
Principle #19Periodic action

3Reliability

If the blocking pin must clear the locking mechanism for deployment, then the reliability of deployment is improved, but the precision required for positioning increases

Engineering Contradiction:
Improvereliability of deploymentVSAvoidpositioning precision of blocking pin
Core Design Contradiction:
ReliabilityVSManufacturing precision

Solution Approach 1:

The blocking pin is made rotatable and is rotated into position by the solenoid actuation of the pivotable legs. This dynamic positioning allows the blocking pin to move from a locked position to a cleared position through controlled rotation, reducing the need for extremely tight manufacturing tolerances while ensuring reliable deployment.

Inventive Principle:
Principle #15Dynamics

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

Ensures reliable and controlled deployment of the ram air turbine by overcoming spring bias and frictional forces, allowing the ram air turbine to transition from a stowed to a deployed position, providing emergency auxiliary power when needed.

Implementation Method 1

The first rod extends a first distance perpendicular to the axis and is configured to exert a first force to push the first leg and second leg away from the solenoid

Methodology Applied
Scientific EffectElectromagnetic force: Lorentz Force

Data Source

PatentUS8920062B2Ejection jack release mechanism
Publication Date: 2014.12.30 HAMILTON SUNDSTRAND CORP
  • US8920062B2 patent drawing
  • US8920062B2 patent drawing
  • US8920062B2 patent drawing

AI summary

An example release mechanism for an ejection jack includes a locking mechanism disposed about an axis. A pivotable first leg is connected to a pivotable second leg by a crossbar. A blocking pin is rotatably connected to the first leg and the second leg such that the locking mechanism abuts the blocking pin. A first solenoid includes a first rod abutting one of the first leg or the second leg. The first rod extends a first distance perpendicular to the axis and is configured to exert a first force to push the first leg and second leg away from the solenoid. The first leg and second leg are configured to pivot away from the first solenoid such that the blocking pin no longer abuts the locking mechanism.