Airfoil structure
First Claim
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7. AN AIRFOIL STRUCTURE WITH POSITIVE CAMBER COMPRISING, IN COMBINATON, AN AIRFOIL SHAPOED BASE MEMBER, A COMPRESSION MEMBER ATTACHED AT ITS BASE TO THE BASE MEMBER, AND TENSIONED MEMBERS RUNNING FROM ANCHOR POINTS AT THE APEX OF THE COMPRESSION MEMBER TO ANCHOR POINTS ON THE BASE MEMBER, SAID ANCHOR POINTS ARRANGED IN SUCH MANNER THAT AN AERODYNAMICALLY USEFUL CAMBERED AIRFOIL CONFIGURATION IS CIRCUMSCRIBED AND IMPARTED TO SAID TENSIONED MEMBERS AND RETAINED IN ANY CROSS SECTION.
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7 Claims
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7. AN AIRFOIL STRUCTURE WITH POSITIVE CAMBER COMPRISING, IN COMBINATON, AN AIRFOIL SHAPOED BASE MEMBER, A COMPRESSION MEMBER ATTACHED AT ITS BASE TO THE BASE MEMBER, AND TENSIONED MEMBERS RUNNING FROM ANCHOR POINTS AT THE APEX OF THE COMPRESSION MEMBER TO ANCHOR POINTS ON THE BASE MEMBER, SAID ANCHOR POINTS ARRANGED IN SUCH MANNER THAT AN AERODYNAMICALLY USEFUL CAMBERED AIRFOIL CONFIGURATION IS CIRCUMSCRIBED AND IMPARTED TO SAID TENSIONED MEMBERS AND RETAINED IN ANY CROSS SECTION.
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Current AssigneeRussell W. Smith Jr
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Original AssigneeRussell W. Smith Jr
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InventorsSmith, Russell W. Jr.
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Application NumberUS04/327,204Time in Patent Office883 DaysField of SearchUS Class Current244/123.1CPC Class CodesB64C 3/00 Wings ornithopter wings B64...
