Sean P Mcgee

US Patent:

20190249605, Aug 15, 2019

Filed:

Feb 12, 2018

Appl. No.:

15/893833

Inventors:

- Farmington CT, US
David Barger - East Hartford CT, US
Sean P. McGee - Vernon CT, US

International Classification:

F02C 7/28
F02C 3/04
F16J 15/3288

Abstract:

A seal configuration for an aircraft engine includes a ring shaped sealing component defining an axis, a carrier disposed radially outward of the ring shaped sealing component and supporting the ring shaped sealing component, and a housing disposed at least partially about the carrier. The housing is maintained in a static position relative to the carrier via a bellows spring. At least one of the carrier and the housing include a plurality of rotation inhibiting features disposed in a balanced configuration about the at least one of the carrier and the housing. Each of the rotation inhibiting features including a finger extending from the housing and at least one interface feature corresponding to each finger, and being disposed on the carrier. The at least one interface feature comprises one of a notch protruding radially into the carrier and a tab protruding radially outward from the carrier.

US Patent:

20190003389, Jan 3, 2019

Filed:

Jan 13, 2017

Appl. No.:

15/405688

Inventors:

- Farmington CT, US
David Barger - East Hartford CT, US
Sean P. McGee - Vernon CT, US

International Classification:

F02C 7/06
F01D 25/18
F16N 7/28

Abstract:

Aspects of the disclosure are directed to a system comprising: a lubrication applicator device that includes: a base having a cavity that is configured to store a lubricant, and a plunger that is configured to seat a head of a bolt in a counterbore of the base, where the plunger is axially movable in the cavity and is configured to be at least partially recessed in the cavity to cause a side of the bolt to be immersed in the lubricant.