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公开(公告)号：US20200080428A1
公开(公告)日：2020-03-12
申请号：US16129457
申请日：2018-09-12
Applicant: United Technologies Corporation
Inventor： TIMOTHY J. JENNINGS , Mark F. Zelesky
Abstract: A component for use in a gas turbine engine includes a channel configured to port a gas from an inlet along a flow path. The component further includes a wall defining an outlet configured to receive the gas, the wall forming an angle with the flow path that is between 60 degrees and 120 degrees, the outlet having a first portion with a first diameter and a second portion with a second diameter, the first portion configured to receive the gas before the second portion, and the first diameter being greater than the second diameter.
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