A resonator system transmits pressure oscillations from the exhaust stream to amplify pulses at the turbine inlet.
A turbo air cooler system circulates natural gas through cooling tubes to reduce engine intake air temperature.
Triiron tetraoxide oxide film prevents red rust and resin deformation to maintain fastening force.
A heat exchanger uses a corridor to improve coolant liquid flow distribution across the core.
A variable compression ratio engine uses a secondary piston mechanism to adjust combustion chamber volume.
An oxyhydrogen burner system mixes HHO gas with natural gas to create a controlled flame inside exhaust pipes.
Targeted perforations enable a fixed exhaust pipe to absorb thermal expansion forces elastically, eliminating sliding seats and reducing noise.
A utility pedestal mounts a turbocharger while routing internal oil and coolant passages directly through the structure.
A crankless miniature engine uses a multi-helix spring to oscillate an alternator coil within a magnetic core for power generation.
A dual pump fluid conditioning system recirculates fuel through a primary filter at high flow rates to enhance particulate removal.
Segmented turbine diffuser attached to inner housing via struts enables single-unit rotor removal.
Magnesium-graphite alloys prevent blocking hydroxide layers during hydrolysis, sustaining continuous hydrogen production rates.
Fluidically isolated resonators suppress pressure pulses via tuning passages to modify engine sound emissions.
A speed sensor detects rotational speed via electric field perturbation and current modulation.
Balancing channel compensates hydraulic thrust on shutting head, reducing elastic force requirements and mechanical inertia for precise fuel injection.