Method and system of automatic warnings and guidance for avoiding loss of tail rotor effectiveness on a rotorcraft
A method for responding to loss of tail rotor effectiveness (LTE) on a rotorcraft having a tail rotor includes detecting an actual or predicted LTE, and determining a lateral LTE area relative to a position of the rotorcraft that is associated with the LTE. In response to the determination of the lateral LTE area, the method automatically displays an LTE alert on a horizontal display that indicates a location of the lateral LTE area relative to the position of the rotorcraft, and automatically indicates on the horizontal display a direction from the position of the rotorcraft that the rotorcraft should move to avoid the lateral LTE area.
1 . A method for responding to loss of tail rotor effectiveness (LTE) on a rotorcraft having a tail rotor, the method comprising:
detecting an actual or predicted LTE;
determining a lateral LTE area in the air and offset to a lateral side of a position of the rotorcraft that indicates which side of the rotorcraft will maintain the LTE; and
in response to the determination of the lateral LTE area, automatically displaying an LTE alert on a horizontal display that indicates an offset side location of the lateral LTE area relative to the position of the rotorcraft, and automatically displaying on the horizontal display, a graphical indicator of a direction from the position of the rotorcraft that the rotorcraft should move to avoid the lateral LTE area and that is distinct from display of the LTE alert.
2 . The method of claim 1 , wherein the horizontal display has a circular portion with a symbol of the rotorcraft at a center of the circular portion, and the LTE alert is a highlighting or a symbol on a sector of the circular portion.
3 . The method of claim 2 , wherein the sector is a quadrant of the circular portion.
4 . The method of claim 2 , wherein the horizontal display is a horizontal situation indicator (HSI), and the circular portion is an image of a compass.
5 . The method of claim 1 , wherein the direction is indicated by an intersection of lateral and longitudinal deviation lines on the horizontal display, wherein a position of the intersection relative to the symbol of the rotorcraft indicates which direction the rotorcraft should move from its current position to avoid the lateral LTE area.
6 . The method of claim 1 , comprising determining whether a pilot is implementing flight controls to adequately compensate for LTE effects on the aircraft; and displaying the location of the lateral LTE area when it is determined that the flight controls are not adequate.
7 . The method of claim 1 , comprising displaying an exit LTE flight plan on the horizontal display that avoids the lateral LTE area.
8 . The method of claim 7 , comprising automatically controlling the rotorcraft to move along the heading of the exit LTE flight plan without a pilot steering the rotorcraft.
9 . The method of claim 1 , comprising broadcasting data indicating a location of the lateral LTE area to other aircraft.
10 . The method of claim 1 , wherein the LTE is a predicted LTE downpath from a position of the rotorcraft, and wherein the method comprises displaying an initial flight path on the horizontal display and with an indication of the lateral LTE area on the horizontal display and an automatically generated alternative flight path that avoids the lateral LTE area.
11 . A rotorcraft, comprising:
a body having a cockpit with a horizontal situation indicator display;
at least one main rotor and a tail rotor interconnected to the body, wherein the tail rotor rotates in a direction transverse to the rotation of the main rotor; and
processor circuitry forming at least one processor communicatively coupled to the display and being arranged to operate by:
detecting an actual or predicted loss of tail rotor effectiveness (LTE),
determining a lateral LTE area in the air and offset to a lateral side of the rotorcraft that indicates which side of the rotorcraft will maintain the LTE, and
in response to the determination of the lateral LTE area, automatically displaying an LTE alert on a horizontal display that indicates an offset side location of the lateral LTE area relative to a position of the rotorcraft, and automatically displaying on the horizontal display, a graphical indicator of a direction from the position of the rotorcraft that the rotorcraft should move to avoid the lateral LTE area and that is distinct from the display of the LTE alert.
12 . The rotorcraft of claim 11 , wherein the horizontal display has a circular portion with a symbol of the rotorcraft at a center of the circular portion, and the LTE alert is a highlighting along an outer edge of a sector of the circular portion.
13 . The rotorcraft of claim 11 , wherein the direction is indicated by a sector of a circular portion of the display that is highlighted in a different color than a color of highlighting of the LTE alert.
14 . The rotorcraft of claim 11 , wherein the at least one processor comprises multiple processors comprising at least one processor disposed remote from the rotorcraft to perform at least one part of the detecting, determining, displaying, or indicating.
15 . The rotorcraft of claim 11 , comprising determining whether a pilot is implementing flight controls to adequately compensate for LTE effects on the aircraft; and
displaying the location of the lateral LTE area and the direction when it is determined that the flight controls are not adequate.
16 . A system, comprising:
a horizontal display on a rotorcraft; and
processor circuitry forming at least one processor communicatively coupled to the display and arranged to operate by:
detecting an actual or predicted LTE,
determining a lateral LTE area in the air and offset to a lateral side of a position of the rotorcraft that indicates which side of the rotorcraft will maintain the LTE; and
in response to the determination of the lateral LTE area, automatically displaying an LTE alert on a horizontal display that indicates an offset side location of the lateral LTE area relative to the position of the rotorcraft, and automatically displaying on the horizontal display, a graphical indicator of a direction from the position of the rotorcraft that the rotorcraft should move to avoid the lateral LTE area and that is distinct from the display of the LTE alert.
17 . The system of claim 16 , wherein the at least one processor is arranged to operate by automatically controlling the rotorcraft to move along the heading of the direction to an exit location without a pilot steering the rotorcraft.
18 . The system of claim 16 , wherein the at least one processor is arranged to operate by displaying an exit LTE flight plan on the horizontal display that avoids the lateral LTE area.
19 . The system of claim 16 , wherein the at least one processor is arranged to operate by broadcasting data indicating the direction away from the lateral LTE area to other aircraft.
20 . The system of claim 16 , wherein the at least one processor is arranged to operate by receiving data of the movement of other rotorcraft, and predicting a lateral LTE area depending on the data.