-
公开(公告)号：US20190101002A1
公开(公告)日：2019-04-04
申请号：US16128671
申请日：2018-09-12
Applicant: ROLLS-ROYCE PLC
Inventor： Roger S. DUFFIN , Gabriel GONZALEZ-GUTIERREZ
Abstract: A blade or vane for a gas turbine engine comprising a pressure surface and a suction surface. The pressure surface or the suction surface comprises a roughness zone which is configured to provide greater flow resistance in a direction along the blade or vane than in a direction across the blade or vane.
Search Results
1
records
(took 0.011 seconds)
筛选
AND
AND
过滤
NOT
NOT
Scan to Join
