http://rdf.ncbi.nlm.nih.gov/pubchem/patent/EP-2903894-A2

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filingDate 2013-07-19-04:00^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_767a3e3b873728414d46270f07c5dc4c
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publicationDate 2015-08-12-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber EP-2903894-A2
titleOfInvention Bifurcated inlet scoop for gas turbine engine
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 may include a nose, a first side panel, and a second side panel. The first side panel and the nose may define a first inlet port. The second side panel and the nose may define a second inlet port. The method may comprise providing a bifurcated inlet scoop frame, splitting the fan air flow, and receiving fan air through the bifurcated inlet scoop frame.
priorityDate 2012-10-01-04:00^^<http://www.w3.org/2001/XMLSchema#date>
type http://data.epo.org/linked-data/def/patent/Publication

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