Reverse tactile cue for rotorcraft rotor overspeed protection

Patent metadata

Field	Value
Publication number	US-11599111-B2
Application number	US-202016830463-A
Country	US
Kind code	B2
Filing date	Mar 26, 2020
Priority date	Feb 27, 2017
Publication date	Mar 7, 2023
Grant date	Mar 7, 2023

Abstract

A flight control computer (FCC) for a rotorcraft includes a processor and a non-transitory computer-readable storage medium storing a program to be executed by the processor, with the program including instructions for providing main rotor overspeed protection. The instructions for providing the main rotor overspeed protection include instructions for monitoring sensor signals indicating a main rotor RPM, determining a target operating parameter, determining one or more flight parameters in response to a relationship between the main rotor RPM and the target operating parameter indicating a main rotor overspeed condition. Determining the one or more flight parameters includes determining a setting for a flight control device of the rotorcraft that changes the main rotor RPM, controlling positioning of a pilot control according to the flight parameters, and controlling the flight control device of the rotorcraft according to positioning of the pilot control.

First claim

What is claimed is:

1. A method for operating a rotorcraft, comprising:
monitoring, by a flight control computer (FCC), a plurality of first sensor signals indicating a main rotor revolutions per minute (RPM) of the rotorcraft;
determining a predicted main rotor RPM according to the plurality of first sensor signals;
determining one or more target operating parameters according to a second signal indicating one or more operating parameters of the rotorcraft;
determining that a main rotor is in an overspeed condition in response to one of the main rotor RPM or the predicted main rotor RPM falling outside of a threshold associated with the one or more target operating parameters within a predetermined time period;
determining a flight parameter according to the one or more target operating parameters and in response to determining that the main rotor is in the overspeed condition;
sending a set signal to a trim motor indicating a first position of one or more pilot controls according to the flight parameter, the set signal causing the trim motor to attempt to move a pilot collective control stick to the first position, wherein the trim motor attempting to move the pilot collective control stick provides a tactile response to a pilot indicating the overspeed condition, and wherein the attempt to move the collective control to the position is overridable through manual control by the pilot; and
controlling one or more flight control devices of the rotorcraft according to positioning of the one or more pilot controls.

2. The method of claim 1 , wherein the controlling the one or more flight control devices of the rotorcraft according to positioning of the one or more pilot controls comprises receiving a position signal indicating a second position of the one or more pilot controls different from the first position and indicating a manual pilot control of the one or more flight control devices.

3. The method of claim 1 , wherein the determining the flight parameter comprises determining a collective control setting associated with raising a collective setting of the one or more flight control devices and further associated with decreasing the main rotor RPM.

4. The method of claim 3 , wherein the sending the set signal to the trim motor comprises sending the set signal and causing the trim motor to drive the one or more pilot controls to the first position while the overspeed condition is maintained.

5. The method of claim 3 , further comprising determining a limit range within a range of movement for the one or more pilot controls and adjusting the flight parameter to maintain the first position of the one or more pilot controls within the limit range.

6. The method of claim 1 , wherein the determining the predicted main rotor RPM comprises:
determining a rate of change of the main rotor RPM; and
determining the predicted main rotor RPM according the main rotor RPM, and the rate of change of the main rotor RPM over a predetermined period of time.

7. The method of claim 1 , wherein the one or more target operating parameters includes a target main rotor RPM, and wherein the threshold is a 1% variation from the target main rotor RPM.

8. A method, comprising:
determining a rotor revolutions per minute (RPM) for a rotor of an aircraft by a flight control computer (FCC) that is of an aircraft and that is in signal communication with a collective trim assembly and that is further in signal communication with one or more flight control devices that are of the aircraft and that are operable to control flight of the aircraft according to a received flight control device control signal;
determining, by the FCC, in response to a relationship between the RPM and an RPM threshold indicating a rotor overspeed condition, a flight parameter associated with reducing the rotor RPM according to the RPM threshold;
determining, by the FCC, a pilot control setting according to the flight parameter;
generating, by the FCC, a rotor pitch set command according to the pilot control setting and sending the rotor pitch set command to a trim assembly connected to a pilot control of the aircraft, the rotor pitch set command causing the trim assembly to attempt to move a pilot collective control stick according to the rotor pitch set command and to generate a rotor pitch position signal indicating a position of the pilot control, wherein the trim assembly attempting to move the pilot collective control stick provides a tactile response to a pilot indicating the overspeed condition, and wherein the attempt to move the collective control is overridable through manual control by the pilot;
generating, by the FCC, a flight control device control signal according to the rotor pitch position signal; and
sending, by the FCC, the flight control device control signal to the one or more flight control devices.

9. The method of claim 8 , wherein the determining, in response to the relationship between the RPM and the RPM threshold indicating the rotor overspeed condition, the flight parameter associated with reducing the rotor RPM according to the RPM threshold comprises determining, by the FCC, according to at least one of the rotor RPM exceeding the RPM threshold or the rotor RPM being predicted to exceed the RPM threshold, the flight parameter associated with reducing the rotor RPM according to the RPM threshold.

10. The method of claim 9 , determining, by the FCC, according to at least one of the rotor RPM exceeding the RPM threshold or the rotor RPM being predicted to exceed the RPM threshold, the flight parameter associated with reducing the rotor RPM according to the RPM threshold comprises determining, by the FCC, according to the rotor RPM and a rate of change of the rotor RPM, the flight parameter associated with reducing the rotor RPM according to the RPM threshold.

11. The method of claim 9 , further comprising determining a target rotor RPM, and wherein the RPM threshold is associated with the target rotor RPM.

12. The method of claim 11 , wherein the determining the target rotor RPM comprises determining the target rotor RPM according to at least one of an altitude of the aircraft and an airspeed of the aircraft.

13. The method of claim 11 , wherein the RPM threshold is a 1% variation of the target rotor RPM.

14. The method of claim 8 , wherein the aircraft is a rotorcraft, wherein the rotor is a main rotor of the rotorcraft, and wherein the flight parameter associated with reducing the rotor RPM includes a collective angle for main rotor blades of the main rotor of the rotorcraft.

15. The method of claim 14 , further comprising determining the flight parameter by determining a value for the collective angle that prevents the main rotor from exceeding a maximum RPM threshold.

16. A method, comprising:
monitoring, by a flight control computer (FCC) that is of a rotorcraft and that is configured to provide main rotor overspeed protection, sensor signals indicating a main rotor revolutions per minute (RPM) for a main rotor of the rotorcraft;
determining a target operating parameter;
determining one or more flight parameters in response to a relationship between the main rotor RPM and the target operating parameter indicating a main rotor overspeed condition, wherein the determining the one or more flight parameters includes determining a setting for one or more flight control devices of the rotorcraft that changes the main rotor RPM;
controlling positioning of one or more pilot controls according to the flight parameters, wherein the controlling the position of the one or more pilot controls comprises causing a trim motor o

Assignees

• Textron Innovations Inc

Inventors

• Bothwell Christopher Mike
• Gillett Luke Dafydd
• Alfred Jillian Samantha

Classifications

• G05D1/0055 Primary

  with safety arrangements · CPC title

• B64C27/57

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

• B64D31/06 Primary

  actuated automatically · CPC title

• F02C9/28

  Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed (F02C9/30 - F02C9/38, F02C9/44 take precedence) · CPC title

• B64C13/343

  overriding of personal controls; with automatic return to inoperative position · CPC title