Separating Device Axial Discharge Port Design
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Solution Overview
Problem
Existing separating devices face challenges in effectively separating solid substances from gas based on particle size, leading to degraded separative performance.
Innovation Solution
A separating device comprising a casing, a rotatable rotor, and blades, with a discharge port configuration that includes a space between the rotor blades and the discharge port, enhancing the separation efficiency by utilizing centrifugal force and airflow swirling to discharge solid substances effectively.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Volume of moving object
If the discharge port is positioned close to the rotor blades, then the device structure is compact, but the separative performance degrades due to insufficient space for effective particle discharge
Solution Approach 1:
The discharge port is positioned at the axial end of the rotor rather than radially adjacent to the blades. This spatial reconfiguration in the axial dimension allows sufficient distance between the rotor blades and discharge port while maintaining overall device compactness, resolving the contradiction between compact structure and effective separation performance.
2Productivity
If the blade length is increased to improve separation efficiency, then more particles can be discharged, but the pressure loss increases and the device becomes more complex
Solution Approach 1:
The rotor is designed with multiple discrete blades spaced at specific intervals rather than a continuous structure. This segmentation allows the gas flow to pass through multiple channels created by the spaced blades, improving separation efficiency through repeated centrifugal action while maintaining lower pressure loss compared to a single long blade structure.
Solution Approach 2:
The blade length is optimized to extend partially through the casing rather than spanning the entire axial length. This partial action provides sufficient centrifugal force for effective particle discharge while reducing the blade surface area that would otherwise create excessive pressure loss and structural complexity.
3Reliability
If the rotor rotation speed is increased to enhance centrifugal separation, then separation performance improves, but energy consumption increases and fine particles may be damaged
Solution Approach 1:
The multiple spaced blades create continuous centrifugal separation zones throughout the rotor length, allowing sustained particle discharge action as gas flows through. This continuous separation mechanism achieves high separation performance for fine particles at moderate rotation speeds, reducing the need for excessive energy input that would be required with fewer or shorter blades.
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 device improves separation efficiency for fine particles, particularly those with sizes from 1 μm to 7 μm, by effectively discharging solid substances through the discharge port, while minimizing pressure loss and extending the life of downstream air filters.
Implementation Method 1
enhancing the separation efficiency by utilizing centrifugal force and airflow swirling to discharge solid substances effectively
Implementation Method 2
enhancing the separation efficiency by utilizing centrifugal force and airflow swirling to discharge solid substances effectively
Data Source
AI summary
A separating device includes a casing, a rotor, and a blade. The casing has a gas inlet, a gas outlet, and a discharge port for solid substances. The rotor is disposed on an inner side of the casing and is configured to be rotatable around a central axis of rotation of the rotor, the central axis of rotation extending along an axial direction of the casing. The blade is disposed between the casing and the rotor and is configured to rotate together with the rotor. The blade has a first end adjacent to the gas inlet and a second end adjacent to the gas outlet. The casing has a space between the second end of the blade and the discharge port in the axial direction.


