Pump Components TRIZ Cases

A dust-proof telecommunication chassis integrates a removable filter module within the cooling plate to protect critical components from airborne particles.

Integrating a fluid conduit into the stator retention component eliminates complex drilled channels, reducing packing space and simplifying machining.

A centrifugal fan impeller housing features a convex surrounding section at the air inlet to increase airflow resistance and minimize leakage.

An aircraft environmental control system recycles energy from turbine expansion to drive compressors and condition cabin air.

A rotary gas meter uses internal undercuts to maintain flow efficiency with standard 2-inch flanges.

Merged volute housing reduces structural volume of two-stage supercharging systems while minimizing flow losses.

Airfoil impingement cooling uses dedicated crossover passages to direct coolant airflow into specific cavities for targeted heat removal.

Dynamic blower control reduces parasitic power loss by matching airflow to real-time debris levels.

Segmented autonomous compressor units eliminate fluid leakage risks while magnetic bearings prevent lubricant contamination in compressed air.

A turbine blade airfoil uses a variable sweep angle to optimize fluid flow distribution across the radial height.

Scalloped back faces and asymmetric webbing reduce turbine wheel inertia, resolving the trade-off between transient response speed and structural integrity.

An interference structure in a centrifugal pump directs fluid through dual outlets via rotation, eliminating complex valve systems.