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U.S. Patent: 5102067 - Integrated helicopter empennage structure - April 7, 1992 |
 | | The integrated empennage structure comprises a shroud integral with the tail boom, a shroud-fin integration shelf, an aft shroud closure, a vertical stabilizer, and a horizontal stabilizer intersecting the vertical stabilizer. |
 | | The empennage structure 20 includes a shroud 22 integral with the tail boom 16, a shroud-fin integration shelf 24, an aft shroud closure 26, a vertical fin or stabilizer 28, and a horizontal fin or stabilizer 30 intersecting the vertical stabilizer 28. |
 | | The integrated empennage structure 20 further comprises an aerodynamically configured and orientated horizontal stabilizer 30 that is optimized, in relation to a predetermined configuration and orientation of the vertical stabilizer 28, to provide negative vertical forces for dynamic pitch stability of the helicopter 10 in the forward flight regimes. |
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