Rotary Latch System with Adjustable Plunger for Aerospace

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Solution Overview

Problem

Existing rotary latch systems for aerospace applications lack efficient mechanisms for secure closure and easy opening of removable and moveable elements on exterior surfaces of vehicles, such as hatches and doors, often requiring complex mechanisms and limited adjustability.

Innovation Solution

A rotary latch system comprising a base with a planar portion and projection, an elongated plunger, drive shaft, bracket, and closure element, which allows for rotational movement between positions to secure or release structures, utilizing a dog leg and compression springs for adjustable engagement and easy operation.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If a rotary latch system is used for securing aerospace vehicle elements, then secure closure is achieved, but the mechanism becomes complex and difficult to operate

Engineering Contradiction:
Improvesecure closureVSAvoidoperation simplicity
Core Design Contradiction:
ReliabilityVSEase of operation

Solution Approach 1:

The latch mechanism is divided into distinct functional segments: a rotatable plunger with dog legs for engagement, a drive shaft for actuation, and a closure element for securing. This segmentation allows each component to perform its specific function efficiently, reducing overall operational complexity while maintaining secure closure

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The latch system inverts the traditional locking mechanism by using a rotatable plunger that engages with grooves in the closure element. Instead of the closure element actively locking, the plunger rotates to engage and disengage, simplifying the operation to a simple rotational motion while ensuring secure closure

Inventive Principle:
Principle #13The other way round (Inversion)

2Ease of manufacture

If a rotary latch system with fixed geometry is used, then manufacturing is simplified, but adaptability to various door thicknesses is reduced

Engineering Contradiction:
Improvemanufacturing simplicityVSAvoidcompatibility with various door thicknesses
Core Design Contradiction:
Ease of manufactureVSAdaptability or versatility

Solution Approach 1:

The plunger is designed with adjustable positioning along its longitudinal axis, allowing the dog legs to be positioned at different heights. This dynamic adjustability enables the latch to adapt to various door thicknesses while maintaining a standardized manufacturing process for the base components

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The system allows modification of the plunger's operational parameters, specifically the position of the dog legs along the longitudinal axis. This parameter change enables the same base structure to work with different door thicknesses, providing versatility without requiring multiple manufacturing variants

Inventive Principle:
Principle #35Parameter changes

3Volume of moving object

If a compact latch design is used, then space is saved, but the mechanism for engagement and release becomes more difficult to access

Engineering Contradiction:
Improvelatch compactnessVSAvoidaccessibility for operation
Core Design Contradiction:
Volume of moving objectVSEase of operation

Solution Approach 1:

The plunger is positioned within a bore in the base, nesting the actuating mechanism within the fixed structure. The drive shaft extends from the base to provide external access for rotation, allowing the compact nested design to maintain ease of operation through the externally accessible drive shaft

Inventive Principle:
Principle #7Nested doll (Nesting)

Data Source

PatentEP3469171B1Rotary latch system
Publication Date: 2023.05.10 HOWMET AEROSPACE INC
  • EP3469171B1 patent drawingFigure 1
  • EP3469171B1 patent drawingFigure 2~3
  • EP3469171B1 patent drawingFigure 4~5

AI summary

A latch (10) includes a base (12) having a bore (22) extending therethrough defining an axis (36), a plunger (150) positioned within the bore (22) and rotatable about the axis (36), a drive shaft (120) positioned adjacent the base (12) and engaged with the plunger (150) such that rotation of the plunger (150) about the axis (36) causes corresponding rotation of the drive shaft (120) about the axis (36), a bracket (70) positioned adjacent the base (12) and the drive shaft (120) and engaged with the drive shaft (120) such that rotation of the drive shaft (120) about the axis (36) causes movement of the bracket (70), and a closure element coupled to the bracket (70) such that movement of the bracket (70) causes the closure element (320) to move between a position wherein the closure element (320) allows a structure to move with respect to an adjacent structure and a position in which the closure element (320) prevents the structure from moving with respect to the adjacent structure.