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公开(公告)号:US10774651B1
公开(公告)日:2020-09-15
申请号:US15869124
申请日:2018-01-12
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: Kurt R. Heinemann , Sumin Tao , Christopher B. Jelks , Xuedong Zhou , Mark David Ring , Konstantinos Panagiotis Giannakopolous , Lisa I. Brilliant
Abstract: A turbomachine airfoil element includes an airfoil that has pressure and suction sides spaced apart from one another in a thickness direction and joined to one another at leading and trailing edges. The airfoil extends in a radial direction a span that is in a range of 2.85-3.15 inch (72.4-80.0 mm). A chord length extends in a chordwise direction from the leading edge to the trailing edge at 50% span and is in a range of 1.52-1.82 inch (38.6-46.2 mm). The airfoil element includes at least two of a first mode with a frequency of 506±10% Hz, a second mode with a frequency of 1732±10% Hz, a third mode with a frequency of 2268±10% Hz, a fourth mode with a frequency of 4007±10% Hz, a fifth mode with a frequency of 4851±10% Hz and a sixth mode with a frequency of 6416±10% Hz.