Wide chord fan blade

申请号 JP3130892 申请日 1992-01-23 公开(公告)号 JPH04330301A 公开(公告)日 1992-11-18
申请人 General Electric Co ; 发明人 GAI KURIFU MAAFUI; BARETSUTO JIYOSEFU FUUAMAN;
摘要 PURPOSE: To provide a large-size laminated airfoil which is excellent in weight adequate to a high bypass engine and can endure normal impact and motion conditions in relation to a fan blade in an aircraft turbo fan engine.
CONSTITUTION: An airfoil with a wide chip chord is comprised of alternating layers of thin metallic foil 28 and elastomeric layers 30. The exterior surfaces of the airfoil are comprised of the thin, metallic foil 28. The airfoil has a metal sheath 20 secured to the leasing edge. High strength metal members extend through the dovetail root sections 14.
COPYRIGHT: (C)1992,JPO
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