Aircraft Cowl Misalignment Latch With Spherical Bearing Surfaces

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Solution Overview

Problem

Existing latch assemblies for aircraft cowls do not effectively accommodate misalignment between components, leading to potential bending moments and difficulty in maintenance.

Innovation Solution

A latch assembly featuring semi-spherical geometry in keepers and hooks, coupled through ball joints, allowing for slight misalignment adjustment and secure engagement, with a handle mechanism for easy opening and closing.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If traditional latch assemblies are used to secure aircraft cowls, then the latch can maintain the cowl in a closed position, but the latch cannot accommodate misalignment between components, leading to bending moments and maintenance difficulties

Engineering Contradiction:
Improvealignment accommodationVSAvoidmaintenance difficulty
Core Design Contradiction:
Adaptability or versatilityVSEase of operation

Solution Approach 1:

The patent employs spherical bearing surfaces on both the keeper and hook components, allowing them to form a ball joint connection. This spherical geometry enables the latch assembly to accommodate misalignment between cowl and nacelle components by rotating and adjusting to the correct alignment position, eliminating bending moments while maintaining secure engagement.

Inventive Principle:
Principle #14Spheroidality (Curvature)

Solution Approach 2:

The latch assembly transitions from a rigid fixed-position connection to a dynamic adjustable connection through the ball joint mechanism. The spherical bearings allow the hook and keeper to rotate and self-align during operation, enabling the system to adapt to misalignment conditions and making maintenance easier by allowing simple disengagement and repositioning.

Inventive Principle:
Principle #15Dynamics

2Strength

If a rigid latch connection is used to securely hold the cowl, then the latch provides strong holding force, but it cannot adjust to misalignment, creating bending moments that stress the structure

Engineering Contradiction:
Improveholding forceVSAvoidbending moments
Core Design Contradiction:
StrengthVSObject-affected harmful factors

Solution Approach 1:

The spherical bearing surfaces enable the latch to maintain strong holding force through proper surface contact while simultaneously accommodating misalignment. The ball joint configuration allows the components to rotate and align correctly, eliminating bending moments that would otherwise stress the structure, thus achieving both strength and alignment tolerance.

Inventive Principle:
Principle #14Spheroidality (Curvature)

3Ease of manufacture

If the latch components have fixed geometric interfaces, then manufacturing is simplified, but the latch cannot accommodate misalignment between installed components

Engineering Contradiction:
Improvecomponent fabricationVSAvoidmisalignment accommodation
Core Design Contradiction:
Ease of manufactureVSAdaptability or versatility

Solution Approach 1:

The patent uses spherical bearing surfaces on both the keeper and hook, which can be manufactured using standard spherical bearing or ball joint techniques. This curved surface geometry provides misalignment accommodation through rotational adjustment while maintaining relative manufacturing simplicity compared to complex adjustable mechanisms.

Inventive Principle:
Principle #14Spheroidality (Curvature)

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 assembly securely maintains cowls in closed positions while accommodating misalignment, reducing bending moments and simplifying maintenance by allowing easy disengagement when intended.

Implementation Method 1

The keeper includes a keeper bearing surface with a semi-spherical geometry. The latch includes a handle and a hook structure operatively coupled to the handle. The hook structure includes a hook bearing surface with a semi-spherical geometry. The hook bearing surface is engaged with the keeper bearing surface when the handle is in the closed position.

Methodology Applied
Scientific EffectSpherical geometry contact: Ball

Data Source

PatentUS12420938B2Misalignment latch for an aircraft system
Publication Date: 2025.09.23 ROHR INC
  • US12420938B2 patent drawing
  • US12420938B2 patent drawing
  • US12420938B2 patent drawing

AI summary

An assembly is provided for an aircraft. This aircraft assembly includes a keeper and a latch. The keeper includes a keeper bearing surface with a semi-spherical geometry. The latch includes a handle and a hook structure operatively coupled to the handle. The handle is configured to move between a closed position and an open position. The hook structure includes a hook bearing surface with a semi-spherical geometry. The hook bearing surface is engaged with the keeper bearing surface when the handle is in the closed position. The hook structure is disengaged from the keeper when the handle is in the open position.