Anti-rotation tabs for the platforms in the fan section of a gas turbine engine are provided. The anti-rotation tabs interface with the trailing edge of the spinner, thereby preventing the platform from rotating and twisting.
申请公布号
EP2971524(A4)
申请公布日期
2016.11.02
申请号
EP20130877503
申请日期
2013.12.16
申请人
UNITED TECHNOLOGIES CORPORATION
发明人
ALARCON, ANDREW, G.;QUINN, CHRISTOPHER, M.;GLASPEY, JAMES;TURNER, MATTHEW, A.
