Light Deflection Unit Rotor Frame Mass Optimization

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Solution Overview

Problem

Existing light deflection units in optical scanning apparatuses generate excessive fluid dynamic noise due to multiple balance weights, leading to increased noise frequencies and fatigue risks in rotary members, particularly when initial imbalances are high and require multiple balance corrections.

Innovation Solution

A light deflection unit design featuring a rotor frame made of a metal plate with a mass less than 3 grams and optimized thickness to minimize stress amplitude below the fatigue limit, allowing for a single balance correction to effectively reduce dynamic imbalance and noise.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If balance weights are provided to multiple portions to correct dynamic imbalance, then the imbalance correction effectiveness is improved, but the fluid dynamic noise increases due to multiple noise sources

Engineering Contradiction:
Improveimbalance correction effectivenessVSAvoidfluid dynamic noise
Core Design Contradiction:
ReliabilityVSObject-generated harmful factors

Solution Approach 1:

The balance correction function is segmented into two independent corrections: first correction using a balance weight on the rotor frame, and second correction using a balance weight on the rotary polygon mirror. This segmentation allows each correction to target specific imbalance components, improving overall correction effectiveness while limiting the number of balance weights that generate noise simultaneously.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The balance correction is implemented in periodic stages: first correction applied to the rotor frame, then second correction applied to the rotary polygon mirror at 180° opposite phase. This periodic approach distributes the correction process over time and different rotational phases, preventing cumulative noise from multiple concurrently operating balance weights.

Inventive Principle:
Principle #19Periodic action

2Object-generated harmful factors

If the rotor frame mass is reduced to minimize balance weight requirements, then the fluid dynamic noise is reduced, but the structural strength may be compromised

Engineering Contradiction:
Improvefluid dynamic noiseVSAvoidrotor frame structural strength
Core Design Contradiction:
Object-generated harmful factorsVSStrength

Solution Approach 1:

The rotor frame mass is optimized to a specific parameter range (0.5g to 3g) that simultaneously satisfies noise reduction requirements and structural strength requirements. This parameter optimization allows the thin plate structure to be sufficiently light to minimize balance weight mass and associated fluid dynamic noise, while remaining strong enough to withstand operational stresses.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The rotor frame is constructed from a thin metal plate (0.01mm to 0.5mm thickness) that provides sufficient structural strength despite minimal mass. The use of metal material with high strength-to-weight ratio enables the rotor frame to maintain structural integrity while keeping mass below 3g, thereby reducing the mass of balance weights and associated fluid dynamic noise.

Inventive Principle:
Principle #40Composite materials

3Reliability

If multiple balance corrections are performed to reduce initial imbalance, then the dynamic imbalance is reduced, but the frequency of balance weight applications increases leading to more noise

Engineering Contradiction:
Improvedynamic imbalance reductionVSAvoidfrequency of balance weight applications
Core Design Contradiction:
ReliabilityVSProductivity

Solution Approach 1:

The balance correction process is segmented into two distinct correction stages targeting different components: first correction on the rotor frame addresses imbalances in the support structure, while second correction on the rotary polygon mirror addresses imbalances in the rotating element. This segmentation achieves comprehensive imbalance reduction in fewer steps compared to multiple corrections on a single component.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The first balance correction is applied preliminarily to the rotor frame before the second correction on the rotary polygon mirror. This preliminary action stabilizes the support structure first, creating a stable baseline that enables the second correction to more effectively address remaining imbalances, thereby reducing the total number of correction iterations needed.

Inventive Principle:
Principle #10Preliminary action

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 reduces the frequency of balance weight applications, minimizes fluid dynamic noise, and prevents fatigue fracture, ensuring accurate and precise balance corrections while shortening the rise time of the optical scanning apparatus.

Implementation Method 1

When the rotary member provided with the balance weight as described above rotates, air strikes on the balance weight to generate fluid dynamic noise.

Methodology Applied
Scientific EffectFluid dynamic noise: Turbulence

Implementation Method 2

a rotary polygon mirror configured to rotate together with the rotor frame and deflect a light beam emitted from a light source

Methodology Applied
Scientific EffectLight deflection: Reflection

Data Source

PatentUS9523851B2Light deflection unit, optical scanning apparatus, and image forming apparatus
Publication Date: 2016.12.20 CANON KK
  • US9523851B2 patent drawing
  • US9523851B2 patent drawing
  • US9523851B2 patent drawing

AI summary

The light deflection unit including a rotary member having a rotor frame formed of a plate of a metal, and a rotary polygon mirror configured to rotate together with the rotor frame and deflect a light beam emitted from a light source, in which a mass of the rotor frame is largest among masses of a plurality of members forming the rotary member, the mass of the rotor frame is smaller than 3 g, and a thickness of the plate of metal is set within a range in which a stress amplitude of a portion of the rotor frame on which a largest stress is exerted during rotation of the rotor member becomes smaller than a fatigue limit of the metal.