Method and system for diagnoses and prognoses of low temperature limit control valve

• US 9,784,638 B1
• Filed: 08/31/2015
• Issued: 10/10/2017
• Est. Priority Date: 08/31/2015
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Followell, David Allan, Nicks, Eric Lee, Hanov, Nail
• Primary Examiner(s): Gray, Francis
• Application Number:
  US14/841,219
• Time in Patent Office: 771 Days
• CPC Class Codes: B64D 13/00 Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space , or structural parts of the aircraft treatment rooms with artificial climate for medical purposes A61G10/02; respiratory apparatus in general A62B; for vehicles in general B60H
• CPC Class Codes: B64D 13/06 the air being conditioned pressurising B64D13/02
• CPC Class Codes: B64D 2045/0085 Devices for aircraft health monitoring, e.g. monitoring flutter or vibration
• CPC Class Codes: B64D 45/00 Aircraft indicators or protectors not otherwise provided for camouflage F41H3/00
• CPC Class Codes: G01M 3/2876 for valves G01M3/30 takes precedence
• CPC Class Codes: Y02T 50/50 On board measures aiming to increase energy efficiency

Abstract

Method and apparatus for determining a probability of below-specified performance of a low temperature limit control valve. During operation of an environmental control system (ECS) for a vehicle, current operation parameters related to the ECS are sensed. Historical operation parameters related to the ECS are retrieved. A probability of below-specified performance of the low temperature limit control valve is determined based on a predetermined relationship between the stored current operation parameters, the historical operation parameters, and the probability of below-specified performance of the low temperature limit valve.

Claims

1. A method, comprising:

during operation of an environmental control system (ECS) for a vehicle, sensing current operation parameters related to the ECS;

retrieving historical operation parameters related to the ECS; and

determining a probability of below-specified performance of a low temperature limit valve of the ECS, based on a predetermined relationship between the sensed current operation parameters and the probability of below-specified performance, wherein the predetermined relationship is based on the current operation parameters, the historical operation parameters, and the probability of below-specified performance of the low temperature limit valve.

2. The method of claim 1, further comprising:

calculating the predetermined relationship between the sensed current operation parameters, the historical operation parameters, and the probability of below-specified performance of the low temperature limit valve.

3. The method of claim 1, wherein the current operation parameters include a current commanded position of the low temperature limit valve and a detected position of the low temperature limit valve.

4. The method of claim 1, wherein the current operation parameters include a pressure at a location upstream of the low temperature limit valve and a pressure at a location downstream of the low temperature limit valve.

5. The method of claim 1, wherein the current operation parameters include a temperature at a location upstream of the low temperature limit valve and a temperature at a location downstream of the low temperature limit valve.

6. The method of claim 1, wherein the current operation parameters include at least one of:

an ambient pressure, an ambient temperature, an altitude, and a position of a flow control valve for the ECS.

7. The method of claim 1, wherein the historical operation parameters include at least one of:

historical ambient pressures, historical ambient temperatures, historical altitudes, and positions of a flow control valve for the ECS at different time samples.

8. An environmental control system (ECS) for a vehicle, comprising:

a first duct arranged to supply cold air from a cold air source;

a second duct arranged to supply warm air from a warm air source;

a junction where the first duct and the second duct intersect, wherein the junction includes an output duct that outputs a mixture of the cold air and the warm air;

a low temperature limit valve arranged in the second duct, wherein the low temperature limit valve is operable to control flow of the warm air from the warm air source;

a valve position sensor arranged relative to the low temperature limit valve, wherein the valve position sensor is operable detect a position of the low temperature limit valve;

a first pressure sensor operable to detect an air pressure downstream of the low temperature limit valve;

a first temperature sensor operable to detect an air temperature downstream of the low temperature limit valve; and

a valve controller operable to;

send valve position commands to the low temperature limit valve, based on the temperature detected by the first temperature sensor; and

sense current operation parameters related to the low temperature limit valve, wherein the current operation parameters include commanded positions of the low temperature limit valve, detected positions of the low temperature limit valve, and detected pressures detected by the first pressure sensor at different sample times.

9. The ECS of claim 8, wherein the valve controller is further operable to perform diagnostics on the low temperature limit valve by:

retrieving historical operation parameters related to the ECS; and

determining a probability of below-specified performance of the low temperature limit valve, based on a predetermined relationship between the sensed current operation parameters and the probability of below-specified performance, wherein the predetermined relationship is based on the current operation parameters, the historical operation parameters, and the probability of below-specified performance of the low temperature limit valve.

10. The ECS of claim 9, wherein the valve controller is further operable to calculate the predetermined relationship between the sensed current operation parameters, the historical operation parameters, and the probability of below-specified performance of the low temperature limit valve.

11. The ECS of claim 8, further comprising a maintenance computer, wherein the valve controller is operable to output the sensed current operation parameters to the maintenance computer, and wherein the maintenance computer is operable to perform diagnostics on the low temperature limit valve by:

retrieving historical operation parameters related to the ECS; and

determining a probability of below-specified performance of the low temperature limit valve, based on a predetermined relationship between the sensed current operation parameters, the historical operation parameters, and the probability of below-specified performance of the low temperature limit valve.

12. The ECS of claim 11, wherein the maintenance computer is further operable to calculate the predetermined relationship between the sensed current operation parameters, the historical operation parameters, and the probability of below-specified performance of the low temperature limit valve.

13. The ECS of claim 8, further comprising a second pressure sensor operable to detect an air pressure upstream of the low temperature limit valve, and wherein the current operation parameters include pressures detected by the second pressure sensor at the different time samples.

14. The ECS of claim 8, further comprising a second temperature sensor operable to detect an air temperature upstream of the low temperature limit valve, and wherein the current operation parameters include temperatures detected by the first temperature sensor and temperatures detected by the second temperature sensor at the different time samples.

15. An aircraft, comprising:

an aircraft cabin adapted to be pressurized;

a gas turbine engine, wherein the gas turbine engine includes at least one engine bleed;

an environmental control system (ECS) operable to receive bleed air from the at least one engine bleed and to provide conditioned air to the aircraft cabin, the ECS including;

a first duct arranged to supply cold air from a cold air source;

a second duct arranged to supply warm air from a warm air source;

a junction where the first duct and the second duct intersect, wherein the junction includes an output duct that outputs a mixture of the cold air and the warm air;

a low temperature limit valve arranged in the second duct, wherein the low temperature limit valve is operable to control flow of the warm air from the warm air source;

a valve position sensor arranged relative to the low temperature limit valve, wherein the valve position sensor is operable detect a position of the low temperature limit valve;

a first pressure sensor operable to detect an air pressure downstream of the low temperature limit valve;

a first temperature sensor operable to detect an air temperature downstream of the low temperature limit valve; and

a valve controller operable to;

send valve position commands to the low temperature limit valve, based on a detected temperature of the mixture of the cold air and the warm air in the output duct of the junction; and

sense current operation parameters related to the low temperature limit valve, wherein the current operation parameters include commanded positions of the low temperature limit valve, detected positions of the low temperature limit valve, and detected pressures detected by the first pressure sensor at different sample times.

16. The aircraft of claim 15, wherein the valve controller is further operable to perform diagnostics on the low temperature limit valve by:

retrieving historical operation parameters related to the ECS; and

determining a probability of below-specified performance of the low temperature limit valve, based on a predetermined relationship between the sensed current operation parameters and the probability of below-specified performance, wherein the predetermined relationship is based on the current operation parameters, the historical operation parameters, and the probability of below-specified performance of the low temperature limit valve.

17. The aircraft of claim 15, further comprising a ram air duct, wherein the ram air duct includes a first heat exchanger arranged therein, wherein the warm air source comprises air flow from the at least one engine bleed that passes through the first heat exchanger, wherein the ram air duct includes a second heat exchanger arranged therein, and wherein the cold air source comprises air flow from the warm air source that passes through a compressor, the second heat exchanger, and an air cycle machine.

18. The aircraft of claim 15, wherein the ECS further comprises a flow control valve downstream of the at least one engine bleed, and wherein the current operation parameters include a position of the flow control valve.

19. The aircraft of claim 15, wherein the ECS further comprises a water separator in fluid communication with the output duct of the junction, wherein the first temperature sensor is operable to detect one of:

a temperature of air in the output duct and a temperature of air in the water separator, and wherein the valve controller sends valve position commands to the low temperature limit valve to achieve a detected temperature from the first temperature sensor above a threshold temperature.

20. The aircraft of claim 19, wherein the threshold temperature is 35°

F.