发明名称 EXTENDABLE/RETRACTABLE AIRFOIL ASSEMBLY FOR FIXED WING AIRCRAFT
摘要 A retractable airfoil assembly (20) augments the wing surface area (28) of an aircraft (22) enabling it to fly without stalling at reduced speeds during takeoff and landing. The airfoil assembly includes flexible sails (42, 44) and a furling mast (24) for extending and retracting the sails. The furling mast includes a furling drum mounted for clockwise and counterclockwise rotation on a static tube (50). The flexible sail assembly also includes guide tracks (80) located along a leading edge (101) or trailing edge (40) of the wings. The tracks guide the flexible sails during extension and retraction. A drive cable (26) extends and retracts the sails (42, 44) along the guide tracks and maintains tension in the sails while they are extended.
申请公布号 CA2284979(A1) 申请公布日期 1998.10.15
申请号 CA19982284979 申请日期 1998.04.08
申请人 WAGNER, FRED A., III 发明人 WAGNER, FRED A., III
分类号 B64C3/54;(IPC1-7):B64C3/54 主分类号 B64C3/54
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