US Patent 10385777 Bifurcated inlet scoop for gas turbine engine
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Patent abstract
A bifurcated inlet scoop frame for a gas turbine engine and method of using such frame for a gas turbine engine are disclosed. The bifurcated inlet scoop frame having a nose, a first side panel, and a second side panel. The first side panel and the nose defining a first inlet port. The second side panel and the nose defining a second inlet port. The method including the steps of providing a bifurcated inlet scoop frame, splitting the fan air flow, and receiving fan air through the bifurcated inlet scoop frame.
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Patent Jurisdiction
Patent Number
103857770
Date of Patent
August 20, 2019
0Patent Application Number
139266320
Date Filed
June 25, 2013
0Official Website
Patent Primary Examiner
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Infobox
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Patent Jurisdiction
Patent Number
103857770
Date of Patent
August 20, 2019
0Patent Application Number
139266320
Date Filed
June 25, 2013
0Official Website
Patent Primary Examiner
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US Patent 10385777 Bifurcated inlet scoop for gas turbine engine
Infobox
Is a
Patent jurisdiction
Patent number
10385777
Date of patent
August 20, 2019
Patent application number
13926632
Date Filed
June 25, 2013
Patent primary examiner
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