Raytheon Technologies Corporation

Mark T McAuliffe

Christopher Waitkus

Randall Lee Greenberg

Colby S Dunn

Daniel H Godfrey

Curtis J Ruckey

Philip DiMuzio

A cable conduit for a bypass flow duct may comprise a head end, a sleeve, a foot end, a boot, and a split grommet wherein the head end is coupled to the sleeve opposite the foot end, wherein the foot end comprises a flared portion, wherein the boot comprises a first flange and a neck, wherein the boot is configured to couple at the neck to the flared portion of the foot end, wherein the head end comprises a second flange and a cutout penetrating into an interior volume of the sleeve, and wherein the split grommet is coupled within the interior volume of the sleeve.

Cable conduit for turbine engine bypass

A cable conduit may comprise a head end, a sleeve having a foot end, a boot, and a split grommet having a first upper surface, wherein the head end is coupled to the sleeve opposite the foot end, wherein the boot comprises a first flange and is coupled to the foot end, wherein the head end comprises a second flange having a second upper surface and a cutout penetrating into an interior volume of the sleeve, and wherein the split grommet is coupled about the inner diameter of the cutout.

Igniter cable conduit for gas turbine engine

Growing community of inventors

Colchester, CT, United States of America

Mark T McAuliffe