Protective shroud for aircraft tail rotor
One embodiment is an apparatus for inhibiting accidental contact by a human with a tail rotor connected to an empennage of an aircraft. The apparatus includes an inverted V-tail connected to an empennage of the aircraft forward of the tail rotor, the inverted V-tail stabilizer comprising a first V-tail stabilizer on a side of the empennage to which the tail rotor is connected and a second V-tail stabilizer on a side of the empennage opposite the side of the empennage to which the tail rotor is connected; and a shroud bar having a first end connected to an outboard end of the first V-tail stabilizer and a second end opposite the first end connected to the empennage aft of the tail rotor, wherein a horizontal distance from the shroud bar to the tail rotor is greater than a length of an arm of the human.
1 . Apparatus for inhibiting accidental contact by a human with a tail rotor connected to an empennage of an aircraft, the apparatus comprising:
an inverted V-tail stabilizer connected to an empennage of the aircraft forward of the tail rotor, the inverted V-tail stabilizer comprising a first V-tail stabilizer portion on a side of the empennage to which the tail rotor is connected and a second V-tail stabilizer portion on a side of the empennage opposite the side of the empennage to which the tail rotor is connected, and
a shroud bar having a first end connected to an outboard end of the first V-tail stabilizer portion and a second end opposite the first end connected directly to the empennage aft of the tail rotor.
2 . The apparatus of claim 1 , wherein the inverted V-tail stabilizer is movable.
3 . The apparatus of claim 1 , wherein the inverted V-tail stabilizer includes at least one control surface.
4 . The apparatus of claim 1 , wherein the inverted V-tail stabilizer comprises a forward inverted V-tail stabilizer, the apparatus further comprising an aft inverted V-tail stabilizer connected to the empennage aft of the tail rotor, the aft inverted V-tail stabilizer including a first V-tail stabilizer portion on side of the empennage to which the tail rotor is connected and a second V-tail stabilizer portion on the side of the empennage opposite the side of the empennage to which the tail rotor is connected.
5 . The apparatus of claim 4 , wherein the shroud bar is connected to the empennage via the first V-tail stabilizer portion of the aft inverted V-tail stabilizer.
6 . The apparatus of claim 5 , wherein the second end of the shroud bar is connected to the outboard end of the first V-tail stabilizer portion of the aft inverted V-tail stabilizer.
7 . The apparatus of claim 4 , wherein at least one of the forward and aft inverted V-tail stabilizers is movable.
8 . The apparatus of claim 4 , wherein at least one of the forward and aft inverted V-tail stabilizers includes at least one control surface.
9 . The apparatus of claim 1 , wherein the shroud bar comprises a substantially horizontal portion including the first end of the shroud bar and a substantially vertical portion including the second end of the shroud bar.
10 . The apparatus of claim 1 , wherein the inverted V-tail stabilizer is symmetrical.
11 . The apparatus of claim 1 , wherein the inverted V-tail stabilizer is asymmetrical.
12 . The apparatus of claim 1 , wherein the inverted V-tail stabilizer provides horizontal and vertical stabilization for the aircraft while the aircraft is in motion.
13 . A rotorcraft comprising:
a fuselage;
an empennage aft of the fuselage;
a tail rotor connected to a first side of the empennage; and
a tail rotor shroud comprising:
an inverted V-tail stabilizer connected to the empennage forward of the tail rotor, wherein a portion of the inverted V-tail stabilizer is on the first side of the empennage; and
a shroud bar having a first end connected to an outboard end of the portion of the inverted V-tail stabilizer and a second end opposite the first end connected directly to the empennage aft of the tail rotor;
wherein the tail rotor shroud provides ground strike protection for the tail rotor.
14 . The rotorcraft of claim 13 , wherein the inverted V-tail stabilizer comprises a forward inverted V-tail stabilizer, the rotorcraft further comprising an aft inverted V-tail stabilizer, wherein a portion of the aft inverted V-tail stabilizer is on the first side of the empennage aft of the tail rotor.
15 . The rotorcraft of claim 14 , wherein the second end of the shroud bar is connected to an outboard end of the portion of the aft inverted V-tail stabilizer.
16 . The rotorcraft of claim 14 , wherein at least one of the forward and aft inverted V-tail stabilizers is movable.
17 . The rotorcraft of claim 14 , wherein at least one of the forward and aft inverted V-tail stabilizers includes a control surface.
18 . The rotorcraft of claim 13 , further comprising a vertical stabilizer proximate an aft end of the empennage.
19 . A protective shroud for a tail rotor on a first side of an empennage of a helicopter comprising a forward inverted V-tail stabilizer and an aft inverted V-tail stabilizer, the protective shroud comprising:
a portion of the forward inverted V-tail stabilizer connected to the first side of the empennage forward of the tail rotor;
a portion of the aft inverted V-tail stabilizer connected to the first side of the empennage aft of the tail rotor; and
a shroud bar having a first end connected to an outboard end of the portion of the forward inverted V-tail stabilizer and a second end opposite the first end connected an outboard end of the portion of the aft inverted V-tail stabilizer;
wherein the forward and aft V-tail stabilizers are configured to provide horizontal stabilization and vertical stabilization for the helicopter.
20 . The protective shroud of claim 19 , wherein at least one of the forward and aft inverted V-tail stabilizers is movable, includes a control surface, or both.