System and method for protection against vortex ring state

Patent metadata

Field	Value
Publication number	US-12054244-B2
Application number	US-202318152924-A
Country	US
Kind code	B2
Filing date	Jan 11, 2023
Priority date	Dec 31, 2019
Publication date	Aug 6, 2024
Grant date	Aug 6, 2024

Abstract

A system and method for protecting a rotorcraft from entering a vortex ring state, the method including monitoring a vertical speed of a rotorcraft, comparing the vertical speed to a vertical speed safety threshold, and performing vortex ring state (VRS) avoidance in response to the vertical speed exceeding the vertical speed safety threshold. The performing the VRS avoidance includes determining a power margin available from one or more engines of the rotorcraft, limiting the vertical speed of the rotorcraft in response to the power margin exceeding a threshold, and increasing a forward airspeed of the rotorcraft in response to the power margin not exceeding the threshold.

First claim

What is claimed is:

1. A method, comprising:
monitoring a vertical speed of a rotorcraft and a forward airspeed of the rotorcraft; and
performing vortex ring state (VRS) avoidance according to at least one of the vertical speed or the forward airspeed, wherein the performing VRS avoidance comprises:
causing the rotorcraft to avoid operating near a restricted region of a rotorcraft flight envelope by controlling flight parameters of the rotorcraft, wherein the controlling the flight parameters of the rotorcraft comprises performing at least one of:
controlling the vertical speed of the rotorcraft; or
controlling the forward airspeed.

2. The method of claim 1 , wherein the causing the rotorcraft to avoid operating at least near the restricted region comprises causing the rotorcraft to operate outside a vertical speed safety threshold, wherein the vertical speed safety threshold is separated from a portion of the restricted region by a vertical speed margin.

3. The method of claim 2 , wherein the vertical speed margin from the restricted region is substantially constant, and wherein the vertical speed safety threshold varies with the forward airspeed, and wherein the vertical speed safety threshold is outside all portions of the restricted region.

4. The method of claim 2 , wherein the vertical speed safety threshold is substantially constant, wherein the vertical speed safety threshold is outside all portions of the restricted region, and wherein the vertical speed margin is associated with at least the forward airspeed and a boundary of the restricted region.

5. The method of claim 1 , wherein the performing the VRS avoidance further comprises determining an accelerated flight VRS boundary of the restricted region of the flight envelope according to operational parameters of the rotorcraft; and
wherein the performing the VRS avoidance comprises controlling the vertical speed of the rotorcraft according to an accelerated flight vertical speed safety threshold associated with the accelerated flight VRS boundary.

6. The method of claim 1 , wherein the performing the VRS avoidance further comprises determining an accelerated flight VRS boundary of the restricted region of the rotorcraft flight envelope according to operational parameters of the rotorcraft; and
wherein the performing the VRS avoidance comprises controlling the forward airspeed of the rotorcraft and wherein the performing the VRS avoidance further comprises controlling a shift in the accelerated flight VRS boundary by initiating at least one VRS suppression technique.

7. The method of claim 6 , wherein the at least one VRS suppression technique comprises one or more of a banked turn, increasing a lateral speed, increasing a yaw and the lateral speed, or a roll-reversal.

8. A device, comprising:
at least one processor;
a non-transitory computer readable medium storing a program for execution by the at least one processor, the program comprising instructions for:
monitoring a vertical speed of a rotorcraft and a forward airspeed of the rotorcraft; and
performing vortex ring state (VRS) avoidance according to at least one of the vertical speed or the forward airspeed, wherein the performing VRS avoidance comprises:
causing the rotorcraft to avoid operating at least near a restricted flight region of a flight envelope for the rotorcraft by controlling flight parameters of the rotorcraft, wherein the controlling the flight parameters of the rotorcraft comprises performing at least one of:
controlling the vertical speed of the rotorcraft; or
controlling the forward airspeed.

9. The device of claim 8 , wherein the instructions for causing the rotorcraft to avoid operating at least near the restricted flight region include instructions for causing the rotorcraft to operate outside a vertical speed safety threshold, wherein the vertical speed safety threshold is separated by a vertical speed margin from a portion of the restricted flight region.

10. The device of claim 9 , wherein the vertical speed margin is substantially constant, and wherein the vertical speed safety threshold is a variable vertical speed safety threshold that varies with the forward airspeed, wherein the vertical speed safety threshold is outside all portions of the restricted flight region.

11. The device of claim 9 , wherein the vertical speed safety threshold is substantially constant, wherein the vertical speed safety threshold is outside all portions of the restricted flight region, and wherein the vertical speed margin is associated with at least the forward airspeed and a boundary of the restricted flight region.

12. The device of claim 8 , wherein the instructions for performing the VRS avoidance include instructions for determining an accelerated flight VRS boundary of the restricted flight region of the flight envelope according to operational parameters of the rotorcraft; and
wherein the instructions for performing the VRS avoidance include instructions for controlling the vertical speed of the rotorcraft according to an accelerated flight vertical speed safety threshold associated with the accelerated flight VRS boundary.

13. The device of claim 8 , wherein the instructions for performing the VRS avoidance include instructions for determining an accelerated flight VRS boundary of the restricted flight region of the flight envelope according to operational parameters of the rotorcraft; and
wherein the instructions for performing the VRS avoidance include instructions for controlling the forward airspeed of the rotorcraft and wherein the performing the VRS avoidance further comprises controlling a shift in the accelerated flight VRS boundary by initiating at least one VRS suppression technique.

14. The device of claim 13 , wherein the at least one VRS suppression technique comprises one or more of a banked turn, increasing a lateral speed, increasing a yaw and the lateral speed, or a roll-reversal.

15. A rotorcraft, comprising:
one or more flight controls;
a flight control computer (FCC) configured to:
monitor a vertical speed of the rotorcraft and a forward airspeed of the rotorcraft; and
perform vortex ring state (VRS) avoidance according to at least one of the vertical speed or the forward airspeed, wherein performing the VRS avoidance comprises:
causing the rotorcraft to avoid operating near a restricted flight region of a flight envelope for the rotorcraft by controlling flight parameters of the rotorcraft, wherein the controlling the flight parameters of the rotorcraft comprises performing at least one of:
controlling the vertical speed of the rotorcraft; or
controlling the forward airspeed.

16. The rotorcraft of claim 15 , wherein causing the rotorcraft to avoid operating at least near the restricted flight region comprises causing the rotorcraft to operate outside a vertical speed safety threshold, wherein the vertical speed safety threshold is separated from a portion of the restricted flight region by a vertical speed margin.

17. The rotorcraft of claim 16 , wherein the vertical speed margin is substantially constant, and wherein the vertical speed safety threshold varies with the forward airspeed, wherein the vertical speed safety threshold is outside all portions of the restricted flight region.

18. The rotorcraft of claim 16 , wherein the vertical speed safety threshold is substantially constant, wherein the vertical speed safety threshold is outside all portions of the restricted flight region, and wherein the vertical speed margin is associated with at least the forward airspeed and a b

Assignees

• Textron Innovations Inc

Inventors

• Brand Albert Gerard
• Kisor Ronald Lorenz

Classifications

• B64D31/06

  actuated automatically · CPC title

• B64C27/57

  automatic or condition responsive, e.g. responsive to rotor speed, torque or thrust · CPC title

• B64D43/02

  for indicating aircraft speed or stalling conditions · CPC title

• B64D2045/0085

  Devices for aircraft health monitoring, e.g. monitoring flutter or vibration · CPC title

• G05D1/815

  to recover from unusual attitude conditions · CPC title