Single-gauge monitoring of multiple components

• US 9,630,724 B2
• Filed: 07/01/2013
• Issued: 04/25/2017
• Est. Priority Date: 03/04/2013
• Status: Active Grant

• Current Assignee: Bell Helicopter Textron Incorporated (Textron Inc)
• Original Assignee: Bell Helicopter Textron Incorporated (Textron Inc)
• Inventors: Oltheten, Erik, Halverson, Aaron
• Primary Examiner(s): Bonzell, Philip J
• Application Number:
  US13/932,456
• Publication Number:
  US 20140246537A1
• Time in Patent Office: 1,394 Days
• CPC Class Codes: B64C 27/008 Rotors tracking or balancing devices
• CPC Class Codes: B64D 43/00 Arrangements or adaptations of instruments arrangements of cameras B64D47/08; aeronautical measuring instruments per se G01C
• CPC Class Codes: G01D 7/08 using a common indicating element for two or more variables

Abstract

According to one embodiment, a gauge display prioritization system comprises a priority engine and an output engine. The priority engine is operable to receive a measurement from a first sensor associated with a first aircraft component and a measurement from a second sensor associated with a second aircraft component, select a prioritization criterion based on the received measurements, and select one priority measurement from the received measurements based on the prioritization criterion. The output engine is operable to instruct a gauge disposed within a cockpit to display information representative of the one priority measurement to a pilot.

Claims

1. A rotorcraft, comprising:

a body;

a power train coupled to the body and comprising a power source and a drive shaft coupled to the power source;

a hub;

a rotor blade coupled to the hub;

a first sensor configured to measure a first performance aspect of a gearbox in mechanical or fluid communication with the power source;

a second sensor configured to measure a second performance aspect of a gearbox in mechanical or fluid communication with the power source, the first and second performance aspects both being either temperature aspects or pressure aspects;

a gauge disposed within a cockpit of the body and operable to display information to a pilot; and

a display prioritization system configured to;

receive a first measurement from the first sensor and a second measurement from the second sensor;

select a prioritization criterion based on at least the received first and second measurements;

select, without user input, one priority measurement for display from the received measurements based on the prioritization criterion selected by the display prioritization system; and

instruct the gauge to display information representative of the one priority measurement selected by the display prioritization system without user input such that the gauge displays only the information representative of the one priority measurement and does not display information representative of any other received measurements.

2. The rotorcraft of claim 1, wherein the display prioritization system is operable to select a prioritization criterion by selecting whether to display the highest value of the received measurements or the lowest value of the received measurements.

3. The rotorcraft of claim 1, wherein the first performance aspect is a temperature or pressure of a first gearbox in mechanical or fluid communication with the power source, and the second performance aspect is a temperature or pressure of a second gearbox in mechanical or fluid communication with the power source.

4. The rotorcraft of claim 1, wherein:

the display prioritization system is operable to normalize the first measurement and the second measurement to a common scale; and

the display prioritization system is operable to select a prioritization criterion by selecting the prioritization criterion based on at least the normalized first and second measurements.

5. The rotorcraft of claim 4, wherein the display prioritization system is operable to instruct the gauge to display information representative of the normalized value of the one priority measurement.

6. The rotorcraft of claim 1, wherein the first performance aspect and the second performance aspect are both pressure aspects, and the first measurement and the second measurement are both pressure measurements.

7. The rotorcraft of claim 6, wherein the display prioritization system is configured to select as the one priority measurement the lowest value of the received pressure measurements.

8. The rotorcraft of claim 6, wherein the display prioritization system is configured to select as the one priority measurement either:

the highest value of the received pressure measurements, if all of the received pressure measurements are above thresholds approaching their respective lower limits and the highest value of the received pressure measurements is above a threshold approaching its upper limit, or

the lowest value of the received pressure measurements.

9. The rotorcraft of claim 6, wherein the display prioritization system is configured to:

normalize the received pressure measurements to a common scale;

select as the one priority measurement either;

the highest value of the normalized pressure measurements, if all of the normalized pressure measurements are above a threshold approaching a lower limit on the common scale and the highest value of the normalized pressure measurements is above a threshold approaching an upper limit on the common scale, or

the lowest value of the normalized pressure measurements; and

instruct the gauge to display information representative of the normalized value of the one priority measurement.

10. The rotorcraft of claim 1, wherein the first performance aspect and the second performance aspect are both temperature aspects, and the first measurement and the second measurement are both temperature measurements.

11. The rotorcraft of claim 10, wherein the display prioritization system is configured to select as the one priority measurement the highest value of the received temperature measurements.

12. The rotorcraft of claim 10, wherein the display prioritization system is configured to select as the one priority measurement either:

the lowest value of the received temperature measurements, if all of the received temperature measurements are below thresholds approaching their respective upper limits and the rotorcraft is operating in an engine startup condition, or

the highest value of the received temperature measurements.

13. The rotorcraft of claim 10, wherein the display prioritization system is configured to:

normalize the received temperature measurements to a common scale;

select as the one priority measurement either;

the lowest value of the normalized temperature measurements, if all of the normalized temperature measurements are below a threshold approaching an upper limit on the common scale and the rotorcraft is operating in an engine startup condition, or

the highest value of the normalized temperature measurements; and

instruct the gauge to display information representative of the normalized value of the one priority measurement.

14. A gauge display prioritization system comprising:

a priority engine operable to;

receive a first measurement from a first sensor associated with a rotorcraft gearbox and a second measurement from a second sensor associated with a rotorcraft gearbox, the first and second measurements both being either temperature measurements or pressure measurements,

select a prioritization criterion based on at least the received first and second measurements, and

select, without user input, one priority measurement for display from the received measurements based on the prioritization criterion selected by the display prioritization system; and

an output engine operable to instruct a gauge disposed within a cockpit to display information representative of the one priority measurement selected by the display prioritization system without user input to a pilot such that the gauge displays only the information representative of the one priority measurement and does not display information representative of any other received measurements.

15. The gauge display prioritization system of claim 14, wherein the display prioritization system is operable to select a prioritization criterion by selecting whether to display the highest value of the received measurements or the lowest value of the received measurements.

16. The gauge display prioritization system of claim 14, further comprising a normalization engine operable to normalize the first and second measurements to a common scale, wherein the display prioritization system is operable to select a prioritization criterion by selecting the prioritization criterion based on at least the normalized first and second measurements.

17. The gauge display prioritization system of claim 16, wherein the display prioritization system is operable to instruct the gauge to display information representative of the normalized value of the one priority measurement.

18. A method of prioritizing measurements for display on a single gauge in a rotorcraft, comprising:

receiving a first measurement from a first sensor associated with a gearbox and a second measurement from a second sensor associated with a gearbox, the first and second measurements both being either temperature measurements or pressure measurements;

selecting a prioritization criterion based on at least the received first and second measurements;

selecting, without user input, one priority measurement for display from the received measurements based on the prioritization criterion selected by the display prioritization system; and

instructing a gauge disposed within a cockpit to display information representative of the one priority measurement selected by the display prioritization system without user input to a pilot such that the gauge displays only the information representative of the one priority measurement and does not display information representative of any other received measurements.

19. The method of claim 18, wherein selecting a prioritization criterion comprises selecting whether to display the highest value of the received measurements or the lowest value of the received measurements.

20. The method of claim 18, further comprising normalizing the first and second measurements to a common scale, wherein selecting a prioritization criterion comprises selecting the prioritization criterion based on at least the normalized first and second measurements.

21. The method of claim 20, wherein instructing the gauge comprises instructing the gauge to display information representative of the normalized value of the one priority measurement.