Nose Landing Gear Yoke and Breaker Bar for Precise Tire Alignment

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Solution Overview

Problem

The existing methods for aligning the nose landing gear of the F-35 aircraft are cumbersome due to the large size and weight of the tow bar, requiring multiple personnel and prone to errors, which can lead to misalignment and safety issues.

Innovation Solution

A tire alignment tool comprising an elongate breaker bar, a yoke with trunnions fitting into the landing gear gudgeons, and an index to align the collar notch, allowing for precise azimuth adjustment with a single person.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If a two leg tow bar is used to align the nose landing gear, then the alignment function is achieved, but the device becomes heavy and difficult to operate

Engineering Contradiction:
Improvealignment accuracyVSAvoidtow bar weight
Core Design Contradiction:
ReliabilityVSWeight of moving object

Solution Approach 1:

The alignment tool is divided into separate components: a yoke assembly with trunnions that interfaces with the landing gear gudgeons, and a breaker bar that applies force. This segmentation allows each component to be optimized independently, reducing overall weight while maintaining alignment functionality.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The yoke assembly acts as an intermediary between the breaker bar and the landing gear. Instead of directly applying force to the landing gear, the breaker bar applies force to the yoke, which then translates this force through the trunnions to rotate the landing gear azimuthally. This intermediary mechanism provides mechanical advantage and reduces the weight required in the breaker bar.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Ease of operation

If a two person crew is used for alignment, then the heavy tow bar can be manipulated, but the process becomes complex and prone to errors

Engineering Contradiction:
Improvealignment operationVSAvoidalignment process complexity
Core Design Contradiction:
Ease of operationVSDevice complexity

Solution Approach 1:

The alignment tool incorporates a visual index that automatically indicates when the landing gear is properly aligned. The index aligns with a reference mark on the aircraft fuselage when the landing gear azimuth is correct, providing self-verifying alignment without requiring multiple personnel to coordinate and communicate.

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The visual indexing system replaces the mechanical coordination required between multiple personnel. Instead of one person verbally directing another person's manual manipulation of a heavy tow bar, the system uses visual alignment indicators that provide immediate feedback on alignment status, reducing human error and simplifying the operational process.

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

3Measurement precision

If visual determination of azimuthal angle is used, then alignment can be performed, but parallax error and other errors occur

Engineering Contradiction:
Improveazimuthal angle measurementVSAvoidvisual alignment accuracy
Core Design Contradiction:
Measurement precisionVSDifficulty of detecting and measuring

Solution Approach 1:

The visual index provides a clear, high-contrast visual indication of proper alignment. When the index aligns with the reference mark on the aircraft fuselage, it creates an unambiguous visual signal that eliminates parallax errors and subjective judgment calls associated with traditional visual alignment methods.

Inventive Principle:
Principle #32Color changes

Data Source

PatentUS20250368353A1Tire alignment breaker bar and yoke
Publication Date: 2025.12.04 THE GOVERNMENT OF THE UNITED STATES AS REPRESENTED BY THE SECRETARY OF THE AIR FORCE
  • US20250368353A1 patent drawing
  • US20250368353A1 patent drawing
  • US20250368353A1 patent drawing

AI summary

A yoke and breaker bar for aligning the nose landing gear tire of an F-35 aircraft. The F-35 landing gear has a fixed forward notch which is used to align the landing gear and tire with the centerline of the airframe. The yoke is removably attached to the landing gear through a pair of matched trunnion and gudgeons. Torque may then be applied to the yoke through the breaker bar to adjust the azimuthal angle of the landing gear. An index is joined to the yoke or breaker bar for aligning the landing gear with the fixed notch. The index may be a laser beam, an elongate pointer or combination thereof.