Exhaust gas temperature indicator for a gas turbine engine

• US 5,479,350 A
• Filed: 08/23/1993
• Issued: 12/26/1995
• Est. Priority Date: 08/23/1993
• Status: Expired due to Fees

• Current Assignee: B&D Instruments and Avionics Incorporated
• Original Assignee: B&D Instruments and Avionics Incorporated
• Inventors: Barakchi, Saied, Black, Jerry C. II
• Primary Examiner(s): Teska, Kevin J.
• Assistant Examiner(s): LOUIS JACQUES, JACQUES H
• Application Number:
  US08/110,245
• Time in Patent Office: 855 Days
• Field of Search: 364/431.01-431.12, 364/424.01, 364/424.02, 364/424.03, 364/550, 364/551.01, 364/424.04, 364/554, 364/508, 364/557, 364/506, 364/569 , 364/511, 364/442, 123/479, 123/489, 123/564, 123/416, 123/483, 123/484, 374/102, 374/144, 374/108-111, 374/170, 374/183, 374/179, 340/438, 340/945, 340/973, 340/959, 340/588, 324/115, 73/117.4, 73/116, 60/603, 60/39.281
• US Class Current: 701/100
• CPC Class Codes: F01D 17/085 to temperature
• CPC Class Codes: F05D 2220/323 for aircraft propulsion, e.g. jet engines
• CPC Class Codes: F05D 2270/112 by limiting temperatures
• CPC Class Codes: F05D 2270/303 Temperature
• CPC Class Codes: G01K 1/02 Means for indicating or recording specially adapted for thermometers
• CPC Class Codes: G07C 3/00 Registering or indicating the condition or the working of machines or other apparatus, other than vehicles

Abstract

An exhaust gas temperature indicator for a gas turbine engine is disclosed in which data representing discrete overtemperature events occurring at different times is stored in a nonvolatile memory for later retrieval and display on an event-by-event basis. A character display is used to provide detailed digital, alphanumeric or other character information relating to each overtemperature event, such as the number, temperature zone, peak temperature and duration of the event. An indicator is provided for indicating the presence of unacknowledged temperature data in the memory device, and a maximum exhaust gas temperature value for an aircraft flight is stored. An analog display for continuously displaying current exhaust gas temperature values is provided in conjunction with a character display for displaying either current or stored values. Separate caution and warning indicators are utilized for alerting the flight crew to developing overtemperature conditions without the need to rely solely on an analog or digital display.

Claims

1. An exhaust gas temperature indicator for detecting, storing and displaying overtemperature events occurring during operation of a gas turbine engine, comprising:

a temperature input for receiving a temperature signal from a sensor associated with the gas turbine engine;

a control device coupled to said temperature input for comparing a sensed exhaust gas temperature represented by said temperature signal with a predetermined temperature limit, and for generating data representing a discrete overtemperature event for each instance in which said sensed temperature exceeds said predetermined temperature limit;

a storage device coupled to said control device for storing overtemperature event data relating to a plurality of discrete overtemperature events occurring at different times; and

a character display coupled to said control device and controlled by said control device in accordance with said overtemperature data stored by said storage device for displaying character information corresponding to each of said discrete overtemperature events;

wherein said control device is effective to compare said sensed temperature with a plurality of predetermined temperature limits corresponding to different temperature zones, and wherein the displayed character information relating to each of said discrete overtemperature events includes the temperature zone of said overtemperature event.

2. An exhaust gas temperature indicator as claimed in claim 1, wherein the displayed character information relating to each of said discrete overtemperature events further includes a numerical display of the peak temperature attained during said overtemperature event.

3. An exhaust gas temperature indicator as claimed in claim 1, wherein the displayed character information relating to each of said discrete overtemperature events further includes a numerical display of the duration of said overtemperature event.

4. An exhaust gas temperature indicator as claimed in claim 1, wherein the displayed character information relating to each of said discrete overtemperature events further includes the order of occurrence of said overtemperature event relative to at least one other overtemperature event.

5. An exhaust gas temperature indicator as claimed in claim 1, wherein said storage device comprises a nonvolatile memory.

6. An exhaust gas temperature indicator as claimed in claim 1, further comprising an event switch coupled to said control device, said event switch when actuated causing said character display to display character information corresponding to at least one discrete overtemperature event for which overtemperature event data is stored in said storage device, and causing said control device to record an acknowledgment of the overtemperature event information for which the corresponding character information has been displayed by said charcter display.

7. An exhaust gas temperature indicator as claimed in claim 6, wherein said event switch comprises a momentary switch, and wherein said control device is responsive to repeated actuation of said event switch to cause said character display to successively display character information relating to other discrete overtemperature events for which overtemperature event data is stored in said storage device.

8. An exhaust gas temperature indicator as claimed in claim 6, further comprising an overtemperature event indicator coupled to said control device for indicating the presence of unacknowledged overtemperature event data in said storage device, said control device being operative to disable said overtemperature event indicator when no unacknowledged overtemperature event data remains in said storage device.

9. An exhaust gas temperature indicator as claimed in claim 6, further comprising a reset switch coupled to said control device, said control device being responsive to the actuation of said reset switch and the absence of unacknowledged overtemperature event data in said storage device to erase said overtemperature event data from said storage device.

10. An exhaust gas temperature indicator as claimed in claim 6, wherein said character display in the absence of event switch actuation displays a numerical indication of the current exhaust gas temperature represented by said temperature signal.

11. An exhaust gas temperature indicator as claimed in claim 10, further comprising an analog display coupled to said control device for providing a continuous analog display of the current exhaust gas temperature represented by said temperature signal.

12. An exhaust gas temperature indicator as claimed in claim 1, wherein the displayed character information corresponding to each of said discrete overtemperature events includes at least one overtemperature parameter in addition to said temperature zone, only one of said parameters being displayed at any given time by said character display, and further comprising a recall switch coupled to said control device, said control device being responsive to actuation of said recall switch to cause said character display to display a different one of said overtemperature parameters relating to the same discrete overtemperature event.

13. An exhaust gas temperature indicator as claimed in claim 12, wherein said additional overtemperature parameter is selected from the group consisting of:

a numerical display of the peak temperature attained during said overtemperature event;

a numerical display of the duration of said overtemperature event; and

the order of occurrence of said overtemperature event relative to at least one other overtemperature event.

14. An exhaust gas temperature indicator as claimed in claim 12, wherein said recall switch comprises a momentary switch, and wherein said control device is responsive to repeated actuation of said recall switch to cause said character display to successively display each of said overtemperature parameters.

15. An exhaust gas temperature indicator for detecting, storing and displaying an overtemperature event occurring during operation of a gas turbine engine, comprising:

a temperature input for receiving a temperature signal from a sensor associated with the gas turbine engine;

a control device coupled to said temperature input for comparing a sensed exhaust gas temperature represented by said temperature signal with a predetermined temperature limit, and for generating overtemperature data when said sensed temperature exceeds said predetermined temperature limit;

a storage device coupled to said control device for storing said overtemperature data;

a display device coupled to said control device and controlled by said control device in accordance with said overtemperature data stored by said storage device to display said stored overtemperature data;

a first switch coupled to said control device, said first switch when actuated causing said display device to display said stored overtemperature data, and causing said control device to record an acknowledgement that the data has been displayed; and

an indicator coupled to said control device for indicating a presence of unacknowledged overtemperature data in said storage device, said control device being operative to disable said indicator when no unacknowledged overtemperature event data remains in said storage device.

16. An exhaust gas temperature indicator as claimed in claim 15, wherein:

said storage device is operative to store and recall overtemperature data relating to a plurality of discrete overtemperature events occurring at different times;

said first switch comprises a momentary switch; and

said control device is responsive to repeated actuation of said first switch to cause said display device to successively display overtemperature data relating to different ones of said discrete overtemperature events.

17. An exhaust gas temperature indicator as claimed in claim 15, further comprising a second switch coupled to said control device, said control device between responsive to the actuation of said second switch and the absence of unacknowledged overtemperature data in said storage device to erase said overtemperature data from said storage device.

18. An exhaust gas temperature indicator for monitoring the peak temperature value occurring during operation of a gas turbine engine, comprising:

a temperature input for receiving a temperature signal from a sensor associated with the gas turbine engine;

a control device coupled to said temperature input; and

a storage device coupled to said control device for storing a peak temperature value under the control of said control device;

said control device being operative to compare a sensed exhaust gas temperature represented by said temperature signal with a predetermined minimum operating temperature, to monitor the peak temperature value represented by said temperature signal after said sensed exhaust gas temperature exceeds said predetermined minimum operating temperature, and to cause said storage device to store said peak temperature value.

19. An exhaust gas temperature monitor as claimed in claim 18, wherein said control device is operative to erase a previously stored peak temperature value after said sensed exhaust gas temperature exceeds said predetermined minimum operating temperature.

20. An exhaust gas temperature monitor as claimed in claim 18, further comprising:

a display device coupled to said control device; and

a switch coupled to said control device;

wherein said control device is responsive to actuation of said switch to cause said display device to display said peak temperature value.

21. An exhaust gas temperature indicator for displaying exhaust gas temperatures occurring during operation of a gas turbine engine, comprising:

a temperature input for receiving a temperature signal from a sensor associated with the gas turbine engine;

a control device coupled to said temperature input for monitoring a sensed exhaust gas temperature represented by said temperature signal, and for generating data to be stored when said sensed temperature meets a predetermined condition;

a storage device coupled to said control device for storing said data;

a switch coupled to said control device;

a character display coupled to and controlled by said control device for displaying character information, said control device being operative to cause said character display to normally display a numerical indication of the current exhaust gas temperature represented by said temperature signal, and said control device being operative in response to actuation of said switch and to said data stored in said storage device to cause said character display to display character information derived from the data stored in said storage device; and

an analog display coupled to said control device for providing a continuous analog display of the current exhaust gas temperature represented by said temperature signal.

22. An exhaust gas temperature indicator as claimed in claim 21, wherein said predetermined condition is selected from the group consisting of an overtemperature condition and a peak temperature condition.

23. An exhaust gas temperature indicator as claimed in claim 21, wherein said character display comprises a digital display device, and wherein said analog display comprises a pointer display.

24. An exhaust gas temperature indicator for providing indications of overtemperature conditions occurring during operation of a gas turbine engine, comprising:

a temperature input for receiving a temperature signal from a sensor associated with the gas turbine engine;

a control device coupled to said temperature input for monitoring a sensed exhaust gas temperature represented by said temperature signal, and for comparing said sensed temperature with a predetermined caution level temperature and a predetermined warning level temperature, respectively, said warning level temperature being higher than said caution level temperature;

a display device coupled to and controlled by said control device for providing a quantitative indication of the current exhaust gas temperature represented by said temperature signal;

an overtemperature caution indicator coupled to and controlled by said control device for indicating a current exhaust gas temperature in excess of said predetermined caution level temperature; and

an overtemperature warning indicator coupled to and controlled by said control device for indicating a current exhaust gas temperature in excess of said predetermined warning level temperature.

25. An exhaust gas temperature indicator as claimed in claim 24, wherein said display device comprises an analog pointer display.

26. An exhaust gas temperature indicator as claimed in claim 24, wherein said display device comprises a digital display device.

27. An exhaust gas temperature indicator as claimed in claim 24, wherein said overtemperature caution indicator and said overtemperature warning indicator comprise lighted indicators having different colors.

28. A method for detecting, storing and displaying exhaust gas overtemperature events occurring during operation of a gas turbine engine, comprising the steps of:

receiving a temperature signal from a sensor associated with the gas turbine engine;

comparing a sensed exhaust gas temperature represented by said temperature signal with a predetermined temperature limit;

generating data representing a discrete overtemperature event for each instance in which said sensed temperature exceeds said predetermined temperature limit;

storing overtemperature event data relating to a plurality of discrete overtemperature events occurring at different times;

recalling said overtemperature event data; and

utilizing said recalled overtemperature event data to control a display of character information corresponding to each of said discrete overtemperature events;

wherein the displayed character information relating to each of said discrete overtemperature events includes a numerical display of the peak temperature attained during said overtemperature event.

29. A method for detecting, storing and displaying exhaust gas overtemperature events occurring during operation of a gas turbine engine, comprising the steps of:

receiving a temperature signal from a sensor associated with the gas turbine engine;

comparing a sensed exhaust gas temperature represented by said temperature signal with a predetermined temperature limit;

generating data representing a discrete overtemperature event for each instance in which said sensed temperature exceeds said predetermined temperature limit;

storing overtemperature event data relating to a plurality of discrete overtemperature events occurring at different times;

recalling said overtemperature event data; and

utilizing said recalled overtemperature event data to control a display of character information corresponding to each of said discrete overtemperature events;

wherein the displayed character information relating to each of said discrete overtemperature events includes a numerical display of the duration of said overtemperature event.

30. A method for detecting, storing and displaying exhaust gas overtemperature events occurring during the operation of a gas turbine engine, comprising the steps of:

receiving a temperature signal from a sensor associated with a gas turbine engine;

comparing a sensed exhaust gas temperature represented by said temperature signal with a predetermined temperature limit;

generating data representing a discrete overtemperature event for each instance in which said sensed temperature exceeds said predetermined temperature limit;

storing overtemperature event data relating to a plurality of discrete overtemperature events occurring at different times;

recalling said overtemperature event data; and

utilizing said recalled overtemperature event data to control a display of character information corresponding to each of said discrete overtemperature events;

wherein the step of comparing said sensed temperature with a predetermined temperature limit comprises comparing said sensed temperature with a plurality of predetermined temperature limits corresponding to different temperature zones, and wherein the displayed character information relating to each of said discrete overtemperature events includes the temperature zone of said overtemperature event.

31. A method for detecting, storing and displaying exhaust gas overtemperature events occurring during operation of a gas turbine engine, comprising the steps of:

receiving a temperature signal from a sensor associated with the gas turbine engine;

comparing a sensed exhaust gas temperature represented by said temperature signal with a predetermined temperature limit;

generating data representing a discrete overtemperature event for each instance in which said sensed temperature exceeds said predetermined temperature limit;

storing overtemperature event data relating to a plurality of discrete overtemperature events occurring at different times;

recalling said overtemperature event data;

utilizing said recalled overtemperature event data to control a display of character information corresponding to each of said discrete overtemperature events; and

recording an acknowledgement of the overtemperature event information for which the corresponding character information has been displayed by said character display.

32. A method as claimed in claim 31, further comprising the steps of:

producing an overtemperature event indication when overtemperature event data has been stored;

disabling said overtemperature event indicator when all stored overtemperature event data has been acknowledged.

33. A method as claimed in claim 31, further comprising the steps of;

receiving a reset signal;

erasing said stored overtemperature event data in response to said reset signal if said overtemperature event data has been acknowledged;

retaining said stored overtemperature event data following said reset signal if said overtemperature event data has not been acknowledged.

34. A method for detecting, storing and displaying exhaust gas overtemperature events occurring during operation of a gas turbine engine, comprising the steps of:

receiving a temperature signal from a sensor associated with the gas turbine engine;

comparing a sensed exhaust gas temperature represented by said temperature signal with a predetermined temperature limit;

generating data representing a discrete overtemperature event for each instance in which said sensed temperature exceeds said predetermined temperature limit;

storing overtemperature event data relating to a plurality of discrete overtemperature events occurring at different times;

recalling said overtemperature event data; and

utilizing said recalled overtemperature event data to control a display of character information corresponding to each of said discrete overtemperature events;

wherein the step of displaying said character information comprises the steps of;

during a first time interval, displaying a first overtemperature parameter relating to a discrete overtemperature event; and

during a second time interval, displaying a second overtemperature parameter relating to the same discrete overtemperature event.

35. A method as claimed in claim 34, wherein said overtemperature parameters are selected from the group consisting of:

a numerical display of the peak temperature attained during said overtemperature event;

a numerical display of the duration of said overtemperature event; and

the order of occurrence of said overtemperature event relative to at least one other overtemperature event.

36. A method as claimed in claim 34, wherein the step of comparing said sensed temperature with a predetermined temperature limit comprises comparing said sensed temperature with a plurality of predetermined temperature limits corresponding to different temperature zones, and wherein said overtemperature parameters are selected from the group consisting of:

a numerical display of the peak temperature attained during said overtemperature event;

a numerical display of the duration of said overtemperature event;

the order of occurrence of said overtemperature event relative to at least one other overtemperature event; and

the temperature zone of said overtemperature event.

38. A method as claimed in claim 36, wherein only a portion of said overtemperature data is recalled and displayed in response to each occurrence of said display command, and wherein said indication is disabled only after all of said overtemperature data has been recalled and displayed.

39. A method as claimed in claim 38, further comprising the steps of:

recording an acknowledgement of overtemperature data which has been recalled and displayed;

disabling said indication only after all of said stored overtemperature data has been acknowledged.

40. A method as claimed in claim 38, wherein the portion of said overtemperature data which is recalled in response to each occurrence of said display command comprises data relating to a discrete overtemperature event.

41. A method as claimed in claim 38, further comprising the steps of:

receiving an erase command;

erasing said stored overtemperature data in response to said erase command only if all of said overtemperature data has been recalled and displayed.

37. A method for generating, storing and displaying exhaust gas temperature data during operation of a gas turbine engine, comprising the steps of:

receiving a temperature signal from a sensor associated with the gas turbine engine;

comparing a sensed exhaust gas temperature represented by said temperature signal with a predetermined temperature limit;

generating overtemperature data when said sensed temperature exceeds said predetermined temperature limit;

storing said overtemperature data;

producing an indication signifying that said overtemperature data has been stored;

receiving a display command;

in response to said display command, recalling said overtemperature data and utilizing said recalled overtemperature data to control a display of said data; and

disabling said indication upon recall and display of said overtemperature data.

42. A method for monitoring the peak exhaust gas temperature value occurring during operation of a gas turbine engine, comprising the steps of:

receiving a temperature signal from a sensor associated with the gas turbine engine;

comparing a sensed exhaust gas temperature represented by said temperature signal with a predetermined minimum operating temperature;

in response to said comparison step indicating that said sensed exhaust gas temperature exceeds said predetermined minimum operating temperature, monitoring the peak temperature value represented by said temperature signal; and

storing said peak temperature value.

43. A method as claimed in claim 42, further comprising the step of erasing a previously stored peak temperature value in response to said comparison step indicating that said sensed exhaust gas temperature exceeds said predetermined minimum operating temperature.

44. A method as claimed in claim 42, further comprising the steps of:

receiving a display command; and

displaying said peak temperature value in response to said display command.

45. A method for generating, storing and displaying exhaust gas temperature data during operation of a gas turbine engine, comprising the steps of:

receiving a temperature signal from a sensor associated with the gas turbine engine;

providing a first display of the current exhaust gas temperature represented by said temperature signal;

generating data to be stored when said sensed temperature meets a predetermined condition;

storing said data;

receiving a display command;

recalling said stored data in response to said display command;

utilizing said recalled data to provide a second display of said recalled data concurrently with said first display of the current exhaust gas temperature.

46. A method as claimed in claim 45, wherein one of said first and second displays comprises an analog display, and wherein the other of said first and second displays comprises a character display.

47. A method as claimed in claim 45, wherein said predetermined condition is selected from the group consisting of an overtemperature condition and a peak temperature condition.

48. A method for providing indications of exhaust gas overtemperature conditions occurring during operation of a gas turbine engine, comprising the steps of:

receiving a temperature signal from a sensor associated with the gas turbine engine;

comparing a sensed exhaust gas temperature represented by said temperature signal with a predetermined caution level temperature and a predetermined warning level temperature, respectively, said warning level temperature being higher than said caution level temperature;

providing a first indication in response to said comparison step indicating that the sensed exhaust gas temperature exceeds said predetermined caution level temperature; and

providing a second indication in response to said comparison step indicating that the sensed exhaust gas temperature exceeds said predetermined warning level temperature.

49. A method as claimed in claim 48, further comprising the step of continuously providing a quantitative indication of the current exhaust gas temperature represented by said temperature signal.

50. A method as claimed in claim 48, wherein the steps of providing said first and second indications respectively comprise the steps of enabling first and second visual indicators having different colors.