Internally-damped airfoil and method therefor
一种阻尼部件、翼型的技术,应用在翼型件领域,达到减小附连应力的效果
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[0013] Figures 1 to 3 schematically depicts an airfoil member 10 according to a first embodiment of the invention, while Figure 4 An airfoil member 50 according to a second embodiment of the invention is schematically depicted. It should be noted that the drawings are drawn for clarity when viewed in conjunction with the following description, and therefore are not necessarily drawn to scale. The particular shape of members 10 and 50 is also not intended to limit the types of airfoil members encompassed by the present invention. In the drawings, like reference numerals designate like elements throughout the various views.
[0014] refer to Figures 1 to 3 In the illustrated embodiment, the member 10 can be seen to have an airfoil portion 12 and a root portion 14, wherein the root portion 14 has a dovetail feature 15 capable of interlocking with complementary features of a rotor disk (not shown) in a manner well known in the art. Consistent with industry terminology, airf...
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