EXHAUST SYSTEMS AND METHODS FOR GAS TURBINE ENGINE

Number of patents in Portfolio can not be more than 2000

United States of America Patent

APP PUB NO 20190107020A1
SERIAL NO

16215914

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Abstract

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A gas turbine engine includes a combustion section that generates combustive gases that form a primary exhaust flow and an exhaust system downstream from the combustion section. The exhaust system includes an eductor system that includes a body that extends along a first axis, and a plurality of ducts spaced apart about a circumference of the body. Each of the plurality of ducts define a plurality of eductor primary flow paths that terminate in a mixing chamber. The exhaust system includes a muffler system downstream from the mixing chamber that includes a plurality of baffles that cooperate to define a tortuous path and attenuate sound generated by the gas turbine engine. The exhaust system includes a housing that surrounds the eductor system and the muffler system such that the eductor system and the muffler system are contained within the housing.

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Patent Owner(s)

Patent OwnerAddress
HONEYWELL INTERNATIONAL INCCHARLOTTE NC 28202

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Brown, Daniel Surprise, US 98 2073
Sheoran, Yogendra Yogi Scottsdale, US 33 269
Shin, Yoonshik Chandler, US 7 15

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