Blower Scroll Casing Recessed Portion Design

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Solution Overview

Problem

Conventional blowers with bellmouth-shaped inflow ports suffer from reduced air blowing efficiency due to the narrowing of the blowout port caused by the overlap of the impeller blades with the recessed portion, leading to increased turbulence and noise.

Innovation Solution

A blower design featuring a scroll casing with a bellmouth-shaped inflow and outflow port, a centrifugal impeller, and a motor, where the recessed portion is formed outside the lateral plate, creating an angle between the inner-circumferential flat portion and the recessed portion to generate small vortices that suppress airflow peeling and turbulence, preventing blade cutting and maintaining equal blowout and suction port heights.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Object-affected harmful factors

If the recessed portion is formed to suppress turbulence and noise, then the airflow stability is improved, but the blowout port is narrowed due to blade cutting, reducing air blowing efficiency

Engineering Contradiction:
Improveturbulence and noiseVSAvoidair blowing efficiency
Core Design Contradiction:
Object-affected harmful factorsVSProductivity

Solution Approach 1:

The recessed portion is repositioned from overlapping with the impeller blades to a location outside the lateral plate's radial extent. This spatial reconfiguration in the radial dimension eliminates blade cutting while preserving the turbulence-suppressing function of the recessed portion, thereby maintaining air blowing efficiency without sacrificing airflow stability.

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

Solution Approach 2:

The harmful effect of blade cutting is extracted and eliminated by separating the recessed portion from the impeller blade path. The recessed portion is extracted from the overlapping region and repositioned outside the lateral plate, removing the conflict between turbulence suppression and blade integrity while maintaining both functions independently.

Inventive Principle:
Principle #2Taking out (Extraction)

2Stability of the object's composition

If the recessed portion is positioned to overlap with the impeller, then turbulence is suppressed, but the blades must be cut away causing blowout port narrowing

Engineering Contradiction:
Improveflow stabilityVSAvoidblowout port geometry
Core Design Contradiction:
Stability of the object's compositionVSShape

Solution Approach 1:

The recessed portion is repositioned in the radial dimension to lie outside the lateral plate's outer circumference, eliminating interference with impeller blades while maintaining its turbulence-suppressing function. This dimensional relocation preserves flow stability without compromising blowout port geometry.

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

Solution Approach 2:

The conflict between flow stability and blade geometry is resolved by extracting the recessed portion from the impeller overlap region. The recessed portion is repositioned outside the lateral plate, removing the harmful interaction while preserving the beneficial flow stabilization effect.

Inventive Principle:
Principle #2Taking out (Extraction)

3Object-affected harmful factors

If the blowout port is narrowed due to blade cutting, then the recessed portion can be formed for turbulence suppression, but air blowing efficiency decreases

Engineering Contradiction:
ImproveturbulenceVSAvoidair blowing efficiency
Core Design Contradiction:
Object-affected harmful factorsVSProductivity

Solution Approach 1:

The recessed portion is repositioned radially outside the lateral plate, eliminating the need to cut impeller blades while maintaining turbulence suppression. This spatial reconfiguration preserves the full blowout port opening, thereby maintaining air blowing efficiency without sacrificing turbulence control.

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

Solution Approach 2:

The harmful effect of blade cutting is extracted and eliminated by relocating the recessed portion outside the impeller blade path. The recessed portion is positioned outside the lateral plate, removing the conflict between turbulence suppression and blade integrity while maintaining both functions independently.

Inventive Principle:
Principle #2Taking out (Extraction)

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

This design effectively reduces turbulence and noise while maintaining air blowing efficiency by preventing airflow peeling and circulation, ensuring the blowout port is not narrowed, thus enhancing the blower's performance.

Implementation Method 1

extremely small vortices are generated from a connection portion between the inner-circumferential flat portion and the recessed portion inner surface

Methodology Applied
Scientific EffectVortex generation: Vortex Ring

Implementation Method 2

peeling of the flow of air which flows into the blower along the bellmouth-shaped inflow port can be suppressed

Methodology Applied
Scientific EffectFlow separation suppression: Flow Separation

Implementation Method 3

centrifugal impeller and a motor disposed in the inside of the scroll casing, the motor being configured to drive the centrifugal impeller

Methodology Applied
Scientific EffectCentrifugal force: Centrifugal Force

Data Source

PatentUS9989067B2Air blower
Publication Date: 2018.06.05 PANASONIC INTELLECTUAL PROPERTY MANAGEMENT CO LTD
  • US9989067B2 patent drawing
  • US9989067B2 patent drawing
  • US9989067B2 patent drawing

AI summary

Blower includes: scroll casing, centrifugal impeller and a motor. Scroll casing includes: recessed portion formed outside lateral plate concentrically with centrifugal impeller; inner-circumferential flat portion disposed more on an inner circumference than recessed portion; and outer-circumferential flat portion disposed more on an outer circumference than recessed portion. Bottommost surface of recessed portion is disposed on a same plane as lateral plate end surface of lateral plate. Angle θa made by inner-circumferential flat portion and recessed portion inner surface of recessed portion on an inner circumference is set to a value which falls within a range of 90° or more to 120° or less.