Strut assembly for an aircraft engine

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United States of America Patent

PATENT NO 10385868
APP PUB NO 20180010616A1
SERIAL NO

15201934

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Abstract

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A strut assembly for a gas turbine engine includes an outer structural case. The outer structural case includes a first mounting pad for mounting a first strut and a second mounting pad for mounting a second strut. The outer structural case further includes a case ligament extending between the first mounting pad and the second mounting pad in a substantially straight direction to reduce an amount of bending stress on the outer structural case.

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Patent Owner(s)

Patent OwnerAddress
GENERAL ELECTRIC COMPANY1 NEUMANN WAY MAIL DROP F16 EVENDALE OH 45215-6301

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
King, Daniel Elmer Norwood, US 4 11
Roll, Christopher Timothy West Chester, US 2 4
Seitzer, Kenneth E Cincinnati, US 9 202

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