Pivoting Fitting for Ejection Seat Catapult Retention

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Solution Overview

Problem

Existing aircraft ejection seat systems face challenges in securely retaining a catapult within the smokestack structure, which can lead to instability and increased aircraft height, affecting aerodynamics and envelope space efficiency.

Innovation Solution

A monolithic fitting system comprising a fitting bar, first leg, and second leg that extend across the catapult and pivotally couple to the smokestack structure, featuring angled slots, fastener apertures, retention wires, pivot posts, and retaining rings to securely house and position the catapult, reducing the likelihood of separation and allowing for adjustable pivot angles.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If a traditional retention system is used for the catapult, then the catapult can be retained in place, but the system height increases and aerodynamics deteriorate

Engineering Contradiction:
Improvecatapult retention stabilityVSAvoidejection seat system height
Core Design Contradiction:
ReliabilityVSLength of stationary object

Solution Approach 1:

The fitting incorporates a pivotable connection between the legs and the smokestack structure, allowing the fitting to dynamically adjust its angle during ejection. This dynamic capability enables the fitting to maintain effective retention while adopting a lower profile position during normal operation, thus reducing system height without compromising catapult retention stability

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The retention system is divided into separate functional components: the fitting bar for横向 retention, the legs for vertical support and pivotable connection, and the smokestack structure for housing. This segmentation allows each component to be optimized independently, enabling the legs to pivot at an angle that reduces overall system height while maintaining retention effectiveness

Inventive Principle:
Principle #1Segmentation

2Reliability

If the fitting structure is made more complex to improve retention security, then catapult positioning improves, but device complexity increases

Engineering Contradiction:
Improvecatapult positioning securityVSAvoidfitting structure complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

Multiple retention functions are merged into a single integrated fitting structure. The fitting bar, legs, and pivot connections work as a unified assembly to provide both横向 and vertical retention, eliminating the need for separate retention mechanisms and reducing overall structural complexity while maintaining positioning security

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The fitting structure serves multiple functions simultaneously: it provides横向 retention through the fitting bar, vertical support through the legs, adjustable positioning through the pivot mechanism, and structural integration with the smokestack. This multi-functionality reduces the need for additional separate components, thereby reducing device complexity while improving retention security

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

Data Source

PatentUS11370553B2Space saver fitting for ejection seat catapult
Publication Date: 2022.06.28 AMI IND INC
  • US11370553B2 patent drawing
  • US11370553B2 patent drawing
  • US11370553B2 patent drawing

AI summary

A fitting for use with an ejection seat system of an aircraft includes a fitting bar configured to extend across a top of a catapult of the ejection seat system and defining an angled slot configured to receive a portion of a gas port of the ejection seat system. The fitting further includes a first leg and a second leg coupled to and extending away from the fitting bar and configured to be pivotally coupled to a smokestack structure of the ejection seat system.