Burners TRIZ Cases

Adjustable nozzle orientation ensures homogeneous air-liquid fuel mixture across varying operating conditions.

Segmented hydraulic transfer paths with varied openings stabilize coating discharge and prevent air mixing in the chamber.

Dynamic electrostatic control adjusts fuel spray angle and atomization to resolve static injector limitations and improve combustion reliability.

Separate inlet cups prevent premature mixing of reactive coating components, extending pot life and reducing VOC emissions.

Segmented combustor liner fasteners constrain radial and circumferential motion to accommodate thermal expansion, maintaining fuel injector location accuracy.

Integrated evaporator housing inside combustion chamber multiplies fuel surface area to resolve insufficient evaporation efficiency.

Diverging air passages in the swirler reduce swirl velocity, resolving poor mixing issues that compromise flame stability and increase nitrogen oxide formation.

Air supply nozzle directs flow toward liquid fuel nozzle axis, suppressing carbonaceous deposits on surrounding surfaces.

A dual-mode sprinkler head adjusts rotation speed via a viscous rotor motor to produce varied water droplet sizes.

A preformed fiber optic cable with a metal sheath transmits burner radiation through tight bends.

Refractory flare tip structure eliminates metal anchors and uses expansion joints to prevent brick dislodging at 1800°C.

Curvilinear passages impart swirl to fuel-air mixtures, expelling hot spots through pressure gradients to prevent flashback into premixing sections.

Tangential and radial inlets create variable swirl to fix poor atomization at low and high power.

Fluorine-base synthetic resin films on the coating device cover prevent paint deposition and leakage, ensuring stable insulating performance.

A spray nozzle uses a bent flow path to direct mixed fluid, generating turbulence that ensures uniform mixing of the spray medium and fluid.

A burner nozzle uses a conical gas dispersing element to atomize liquid fuel into a monodisperse spray pattern.

Thick, long-chord swirler vanes reduce parasitic pressure losses and emissions by improving airflow uniformity in the gas turbine combustion chamber.

A fuel nozzle spray tip uses a spherical distal end and annular lip to expand the spray cone via the Coanda effect.

High swirl angle distributor slots merge fuel streams early in the annular passage, resolving non-uniform mixing and coking issues.

A bidet nozzle structure uses a fluid mixing unit to generate swirling water currents for precise spray angle control.