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filingDate 2016-09-27-04:00^^<http://www.w3.org/2001/XMLSchema#date>
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publicationDate 2017-04-05-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber EP-3150801-A1
titleOfInvention Cmc film cooled gas turbine engine component
abstract An engine component (80) for a gas turbine engine (10) generating hot combustion gas flow (H) is provided. The engine component (80) can include a substrate (82) constructed from a CMC material and having a hot surface (84) facing the hot combustion gas flow (H) and a cooling surface (86) facing a cooling fluid flow (C). The hot combustion gas flow (H) defines an upstream direction (108) and a downstream direction (110) relative to the hot surface (84). The substrate (82) also defines a film hole (90) extending through the substrate (82) and having an inlet (92) provided on the cooling surface (86), an outlet (94) provided on the hot surface (84), and a passage (96) connecting the inlet (92) and the outlet (94). The passage (96) comprises a metering section (98); and a diffusing section (100), with the diffusing section (100) including a shelf (101), a first outer lobe (120a) and a second outer lobe (120b).
priorityDate 2015-09-30-04:00^^<http://www.w3.org/2001/XMLSchema#date>
type http://data.epo.org/linked-data/def/patent/Publication

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