Compliant tail structure for rotorcraft
A compliant tail structure for a rotorcraft having rotating components and a fuselage. The tail structure includes a tail assembly having first and second oppositely disposed tail members. A tail joint connects the tail assembly to an aft portion of the fuselage. The tail joint includes at least four tail mounts configured to establish a nodding axis for the tail assembly. At least two of the tail mounts are resilient tail mounts that are configured to establish a nodding degree of freedom for the tail assembly relative to the fuselage about the nodding axis, thereby detuning dynamic fuselage responses from excitation frequencies generated by the rotating components.
1. A compliant tail structure for a rotorcraft having rotating components and a fuselage with an aft portion including an upper airframe member, the tail structure comprising:
a tail assembly having a tail assembly airframe including a lower airframe member and first and second oppositely disposed tail members; and
a tail joint connecting the lower airframe member of the tail assembly to the upper airframe member of the aft portion of the fuselage, the tail joint including two forward resilient tail mounts and two aft resilient tail mounts that are configured to establish a virtual nodding axis for the tail assembly between the forward and aft resilient tail mounts;
wherein, the aft resilient tail mounts are stiffer than the forward resilient tail mounts such that the virtual nodding axis is closer to the aft resilient tail mounts than the forward resilient tail mounts;
wherein, the aft resilient tail mounts are tension tail mounts and the forward resilient tail mounts are elastomeric tail mounts; and
wherein, the forward and aft resilient tail mounts are configured to establish a nodding degree of freedom for the tail assembly relative to the fuselage about the virtual nodding axis, thereby detuning dynamic fuselage responses from excitation frequencies generated by the rotating components.
2. The compliant tail structure as recited in claim 1 wherein the tail assembly further comprises an integrated v-tail assembly.
3. The compliant tail structure as recited in claim 1 wherein the tail joint connects the lower airframe member of the tail assembly to the upper airframe member of the fuselage substantially horizontally.
4. The compliant tail structure as recited in claim 1 wherein the resilient tail mounts further comprise substantially vertically oriented tail mounts.
5. A rotorcraft comprising:
a fuselage with an aft portion including an upper airframe member;
at least one rotor assembly rotatably coupled to the fuselage and configured to provide at least vertical thrust;
a tail assembly having a tail assembly airframe including a lower airframe member and first and second oppositely disposed tail members; and
a tail joint connecting the lower airframe member of the tail assembly to the upper airframe member of the aft portion of the fuselage, the tail joint including two forward resilient tail mounts and two aft resilient tail mounts that are configured to establish a virtual nodding axis for the tail assembly between the forward and aft resilient tail mounts;
wherein, the aft resilient tail mounts are stiffer than the forward resilient tail mounts such that the virtual nodding axis is closer to the aft resilient tail mounts than the forward resilient tail
wherein, the aft resilient tail mounts are tension tail mounts and the forward resilient tail mounts are elastomeric tail mounts; and
wherein, the forward and aft resilient tail mounts are configured to establish a nodding degree of freedom for the tail assembly relative to the fuselage about the virtual nodding axis, thereby detuning dynamic fuselage responses from excitation frequencies generated by the at least one rotor assembly.
6. The rotorcraft as recited in claim 5 wherein the rotorcraft further comprises a tiltrotor aircraft.
7. The rotorcraft as recited in claim 5 wherein the tail joint connects the lower airframe member of the tail assembly to the upper airframe member of the fuselage substantially horizontally.
8. The rotorcraft as recited in claim 5 wherein the resilient tail mounts further comprise substantially vertically oriented tail mounts.