Rocket Thrust Ring Adhesive Bonding and Snap Fit Stability

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Solution Overview

Problem

Existing rocket systems, particularly single-use motors, face challenges with thrust rings that can become loose under pressure, leading to safety hazards and motor destruction, due to labor-intensive installation methods and materials that are not always reliable.

Innovation Solution

A thrust ring design that uses an adhesive, such as epoxy, to securely attach to the rocket motor housing and nozzle, with a secondary cyanoacrylate bond for additional retention, preventing ejection under pressure and ensuring a strong, reliable connection.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If traditional mechanical attachment methods are used for thrust rings, then installation is simpler, but the thrust ring becomes loose under pressure leading to safety hazards

Engineering Contradiction:
Improvethrust ring attachment reliabilityVSAvoidattachment mechanism complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent introduces adhesive as an intermediary substance between the thrust ring and motor housing. The adhesive fills the gap between the thrust ring's inner diameter and the motor housing's outer diameter, creating a reliable chemical bond that prevents the thrust ring from becoming loose under pressure while maintaining a simple overall attachment structure.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Reliability

If adhesive is used to attach the thrust ring, then attachment reliability improves, but installation becomes more complex and labor-intensive

Engineering Contradiction:
Improvethrust ring attachment reliabilityVSAvoidinstallation ease
Core Design Contradiction:
ReliabilityVSEase of operation

Solution Approach 1:

The patent incorporates a protrusion feature on the thrust ring that is designed to engage with a corresponding recess in the motor housing before the adhesive fully cures. This preliminary mechanical engagement guides the thrust ring into proper alignment and prevents it from shifting during the adhesive setting process, thereby simplifying the installation procedure while maintaining high reliability.

Inventive Principle:
Principle #10Preliminary action

3Object-affected harmful factors

If the thrust ring is securely attached to prevent ejection, then safety improves, but the motor housing and nozzle require precise dimensional tolerances

Engineering Contradiction:
Improveejection hazard preventionVSAvoidhousing and nozzle dimensional precision
Core Design Contradiction:
Object-affected harmful factorsVSManufacturing precision

Solution Approach 1:

The patent applies adhesive specifically in the gap region between the thrust ring and motor housing, rather than requiring high precision throughout the entire component structure. The adhesive concentrates the sealing and bonding function in a localized area, allowing the rest of the motor housing and nozzle to be manufactured with standard tolerances while still achieving secure attachment and preventing ejection.

Inventive Principle:
Principle #3Local quality

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 provides a secure and reliable attachment of the thrust ring to the rocket motor, preventing ejection and ensuring safe operation by embedding the inner ring in epoxy and using a snap fit for additional stability, thus enhancing safety and reducing the risk of motor failure.

Implementation Method 1

a thrust ring configured for connection to the motor housing using an adhesive

Methodology Applied
Scientific EffectAdhesive bonding: Adhesive

Implementation Method 2

a secondary cyanoacrylate bond for additional retention

Methodology Applied
Scientific EffectCyanoacrylate bonding: Cyanoacrylate

Data Source

PatentUS10746133B2Rocket apparatuses, systems and methods
Publication Date: 2020.08.18 RCS ROCKET MOTOR COMPONENTS
  • US10746133B2 patent drawing
  • US10746133B2 patent drawing
  • US10746133B2 patent drawing

AI summary

A thrust ring for a rocket motor for one or more of limited re-use or single use, including a rocket motor housing, the motor housing adapted to contain propellant; an aft closure with a nozzle, the aft closure connected or connectable to the housing; a forward closure connected or connectable to the housing; wherein one or both of the aft closure and the forward closure are connectable to the housing in manner adapted for one or both of limited re-use or single use.