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18383362. DAMPED FLUID LINE FOR AIRCRAFT ENGINE (RTX CORPORATION)

From WikiPatents


DAMPED FLUID LINE FOR AIRCRAFT ENGINE

Organization Name

RTX CORPORATION

Inventor(s)

Kerry L. Davis-amendola of Wethersfield CT US

William Bogue of Hebron CT US

Stuart C. Kozan of Bethany CT US

Ryan S. Railton of West Hartford CT US

Seth M. Glaser of Rocky Hill CT US

Matthew T. Grisham of Rocky Hill CT US

Michael A. Krumholz of West Hartford CT US

Eric H. Hoy of East Hartford CT US

Colby S. Dunn of East Hartford CT US

Brian V. Abedon of Silverthorne CO US

Gianna Sabino of Fort Worth TX US

EmmaKate Mortillaro of Glastonbury CT US

Mir S. Haque of Lake Worth Beach FL US

DAMPED FLUID LINE FOR AIRCRAFT ENGINE

This abstract first appeared for US patent application 18383362 titled 'DAMPED FLUID LINE FOR AIRCRAFT ENGINE

Original Abstract Submitted

A method of operation is provided during which a fluid is directed through a fluid line servicing a component of an aircraft engine. Pressure wave oscillations travel through the fluid within the fluid line at a frequency equal to or greater than one thousand five hundred hertz during the directing of the fluid. The pressure wave oscillations traveling through the fluid within the fluid line are damped using an elastomeric foam sleeve in contact with the fluid line. The elastomeric foam sleeve extends longitudinally along and circumscribes the fluid line.

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