AERIAL VEHICLE WITH MISSION DURATION CAPABILITY DETERMINATION

• US 20130325212A1
• Filed: 05/29/2012
• Published: 12/05/2013
• Est. Priority Date: 05/29/2012
• Status: Abandoned Application

• Current Assignee: Rtx Corporation
• Original Assignee: United Technologies Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Wickman, David L.
• Application Number:
  US13/482,477
• Publication Number:
  US 20130325212A1
• Time in Patent Office: Days
• US Class Current: 701/3
• CPC Class Codes: B64U 2101/00 UAVs specially adapted for particular uses or applications
• CPC Class Codes: B64U 2101/15 for conventional or electronic warfare
• CPC Class Codes: F01D 25/18 Lubricating arrangements of machines or engines in general F01M
• CPC Class Codes: F05D 2270/80 Devices generating input signals, e.g. transducers, sensors, cameras or strain gauges

Abstract

An aerial vehicle can include oil sensors connected to a lubrication system and a computer connected to the oil sensors. The computer can be programmed to determine mission duration for the unmanned aerial vehicle, determine a maximum oil system duration for the unmanned aerial vehicle based upon data from the oil sensors, perform a comparison of the mission duration to the maximum oil system duration, and output a signal based upon the comparison.

Claims

1. An unmanned aerial vehicle comprising:

a gas turbine engine;

a lubrication system connected to the gas turbine engine;

oil sensors connected to the lubrication system; and

a computer connected to the oil sensors and programmed to determine mission duration for the unmanned aerial vehicle, determine a maximum oil system duration for the unmanned aerial vehicle based upon data from the oil sensors, perform a comparison of the mission duration to the maximum oil system duration, and output a signal based upon the comparison.

2. The unmanned aerial vehicle of claim 1, wherein the oil sensors comprise an oil level sensor and an oil temperature sensor, the unmanned aerial vehicle further comprising:

an aircraft attitude sensor connected to the computer for determining attitude data of the unmanned aerial vehicle, wherein the computer is programmed to determine the maximum oil system duration for the unmanned aerial vehicle only when the attitude data is in a predetermined range.

3. The unmanned aerial vehicle of claim 1, wherein the computer is a data computer, the unmanned aerial vehicle further comprising:

a vehicle management computer connected to the gas turbine engine for controlling the gas turbine engine based upon information received wirelessly from a ground control station.

4. Computer readable media for storing instruction for operating an aerial vehicle, comprising:

instructions to determine a mission duration for the aerial vehicle;

instructions to determine a maximum oil system duration for the aerial vehicle based upon data from oil sensors;

instructions to perform a comparison of the mission duration to the maximum oil system duration; and

instructions to output a signal based upon the comparison.

5. The computer readable media of claim 4, and further comprising:

instructions for revising a mission plan to have a shorter revised mission duration in response to the mission duration exceeding the maximum oil system duration.

6. The computer readable media of claim 4, and further comprising:

instructions for aborting a mission plan in response to the mission duration exceeding the maximum oil system duration.

7. The computer readable media of claim 4, wherein the instructions to determine a maximum oil system duration for the aerial vehicle comprise:

instructions for sensing oil level in an oil system of a gas turbine engine of the aerial vehicle via an oil level sensor;

instructions for sensing oil temperature in the oil system via an oil temperature sensor;

instructions for sensing attitude of the aerial vehicle via an aircraft attitude sensor;

instructions for calculating a current oil quantity based upon sensed oil level, oil temperature, and attitude over a plurality of cycles;

instructions for estimating oil consumption rate based upon the current oil quantity calculated over the plurality of cycles; and

instructions for estimating an amount of time until the current oil quantity drops below a threshold based upon the oil consumption rate and the current oil quantity.

8. The computer readable media of claim 4, wherein the instructions to determine a maximum oil system duration for the aerial vehicle further comprise:

instructions for continuously updating the amount of time until the current oil quantity drops below the threshold at each of the plurality of cycles during flight.

9. The computer readable media of claim 8, wherein the plurality of cycles are spaced by between 0.1 second and 1.0 second.

10. A method for operating an aerial vehicle, the method comprising:

determining a mission duration for the aerial vehicle;

determining a maximum oil system duration for the aerial vehicle based upon data from oil sensors;

performing a comparison of the mission duration to the maximum oil system duration via a computer; and

outputting a signal from the computer based upon the comparison.

11. The method of claim 10, and further comprising:

revising a mission plan to have a shorter revised mission duration in response to the mission duration exceeding the maximum oil system duration.

12. The method of claim 10, and further comprising:

aborting a mission plan in response to the mission duration exceeding the maximum oil system duration.

13. The method of claim 10, wherein the aerial vehicle is an unmanned aerial vehicle and wherein the mission duration exceeds 100 hours.

14. The method of claim 10, wherein the signal comprises an alarm in the form of a text warning that the mission duration exceeds the maximum oil system duration.

15. The method of claim 10, wherein determining a maximum oil system duration for the aerial vehicle comprises:

sensing oil level in an oil system of a gas turbine engine of the aerial vehicle via an oil level sensor;

sensing oil temperature in the oil system via an oil temperature sensor;

sensing attitude of the aerial vehicle via an aircraft attitude sensor;

calculating a current oil quantity based upon sensed oil level, oil temperature, and attitude over a plurality of cycles;

estimating oil consumption rate based upon the current oil quantity calculated over the plurality of cycles; and

estimating an amount of time until the current oil quantity drops below a threshold based upon the oil consumption rate and the current oil quantity.

16. The method of claim 15, wherein determining a maximum oil system duration for the aerial vehicle further comprises:

continuously updating the amount of time until the current oil quantity drops below the threshold at each of the plurality of cycles during flight.

17. The method of claim 16, wherein the plurality of cycles are spaced by between 0.1 second and 1.0 second.

18. The method of claim 10, wherein performing a comparison of the mission duration to the maximum oil system duration and outputting a signal occur prior to the aerial vehicle embarking on a mission plan.

19. The method of claim 10, wherein performing a comparison of the mission duration to the maximum oil system duration and outputting a signal occur after the aerial vehicle embarks on a mission plan.

20. The method of claim 15, wherein the aerial vehicle is an unmanned aerial vehicle and further comprises:

controlling the unmanned aerial vehicle via a vehicle management computer based upon information received wirelessly from a ground control station.

21. The method of claim 10, and further comprising:

setting a reserve mission duration to a length of time that the aerial vehicle can be expected to operate in excess of the mission duration.

22. The method of claim 21, wherein outputting a signal comprises:

notifying a ground control station that the reserve mission duration has been exceeded.

23. The method of claim 10, and further comprising:

transferring oil from an auxiliary oil tank to a main oil tank in response to the mission duration exceeding the maximum oil system duration.