METHOD AND SYSTEM FOR REDUCTION OF JET ENGINE NOISE

PROBLEM TO BE SOLVED: To attenuate jet engine noises utilizing fluid control. SOLUTION: Air velocity, in the vicinity of an inlet fan duct outer wall (22), is increased to a greater velocity than a typical velocity of an operational engine ambient inlet airflow (12), adjacent to the inlet fan duct o...

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Bibliographische Detailangaben
Hauptverfasser:	MANI RAMANI, GRAZIOSI PAOLO
Format:	Patent
Sprache:	eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS TRANSPORTING WEAPONS
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