Temperature monitoring system

• US 4,114,442 A
• Filed: 09/03/1976
• Issued: 09/19/1978
• Est. Priority Date: 09/03/1976
• Status: Expired due to Term

• Current Assignee: Avicon
• Original Assignee: Avicon
• Inventors: Pratt, Wayne L.
• Primary Examiner(s): Swisher, S. Clement
• Application Number:
  US05/720,406
• Time in Patent Office: 746 Days
• Field of Search: 73/341, 73/346, 364/557, 340/413
• US Class Current: 374/113
• CPC Class Codes: F02B 2075/1856 fourteen
• CPC Class Codes: G01K 1/026 arrangements for monitoring a plurality of temperatures, e.g. by multiplexing
• CPC Class Codes: G01K 1/028 arrangements for numerical indication
• CPC Class Codes: G01K 3/08 giving differences of values using thermoelectric elements G01K7/02; giving differentiated values
• CPC Class Codes: G01K 7/021 Particular circuit arrangements G01K7/026, G01K7/12, G01K7/14 take precedence

Abstract

The specification discloses a temperature monitoring system for monitoring thermal operating characteristics of aircraft engines. The system includes a plurality of temperature sensors located in different temperature monitoring zones within the aircraft engine to produce electrical sensor output signals proportional to the temperature of the corresponding zones. The temperature monitoring system further includes circuitry for automatically and sequentially scanning the sensor output signals. An electronic processor generates temperature difference signals representing the temperature difference between the hottest and coldest scanned sensor output signals. A visual display displays the generated temperature difference signal, the number of the temperature monitoring zone being monitored and the temperature of the hottest temperature monitoring zone. The system thus enables the aircraft operator to accurately and quickly observe the thermal operating characteristics of the aircraft'"'"'s engine.

Claims

1. A monitoring device for monitoring thermal operating characteristics of an engine including turbine and piston engines comprising:

a first plurality of thermocouples located in first temperature monitoring zones within the engine for measuring the temperature of said first temperature monitoring zones and for generating corresponding first temperature output signals;

a second plurality of thermocouples located in second temperature monitoring zones within the engine for measuring the temperature of said second temperature monitoring zones and for generating corresponding second temperature output signals;

a third plurality of thermocouples located in third temperature monitoring zones within the engine for measuring the temperature of said third temperature monitoring zones and for generating corresponding third temperature output signals;

a multiplexing circuit for automatically and sequentially scanning and detecting said first, second and third temperature output signals;

means for converting said scanned temperature output signals to digital information;

an electronic processor for continuously generating a first temperature difference signal representing the temperature difference between the hottest and coldest zone of said first temperature monitoring zones, a second temperature difference signal representing the temperature difference between the hottest and coldest zone within said second temperature monitoring zones and a third temperature difference signal representing the temperature difference between the hottest and coldest zone within said third temperature monitoring zones;

means for storing said digital information and said first, second and third temperature difference signals;

first display means for alternately displaying the number of the temperature monitoring zone within said first, second and third temperature monitoring zones having the hottest temperature;

second display means for alternately displaying said first, second and third temperature difference signals; and

third display means for alternately displaying the temperature of the hottest zone within said first, second and third temperature monitoring zones.

2. The monitoring device of claim 1 wherein said first temperature monitoring zones comprise the exhaust pipes of the engine cylinders, such that said first plurality of thermocouples measure the exhaust gas temperature of each of the engine cylinders.

3. The monitoring device of claim 2 wherein said first display means displays the number of the engine cylinder having the hottest temperature, said second display means displays the temperature difference between the exhaust gas temperature of the hottest and coldest engine cylinders and said third display means displays the exhaust gas temperature of the engine cylinder having the hottest temperature.

4. The monitoring device of claim 2 and further including means for generating an alarm signal if the temperature of the exhaust gas of the hottest engine cylinder exceeds a predetermined temperature value stored in said electronic processor.

5. The monitoring device of claim 2 and further including means for generating an alarm signal if the temperature of the exhaust gas of the coldest engine cylinder is less than a predetermined temperature value stored in said electronic processor.

6. The monitoring device of claim 1 wherein said second temperature monitoring zones comprise the cylinder heads of the engine cylinders, such that said second plurality of thermocouples measure the cylinder head temperature of each of the engine cylinders.

7. The monitoring device of claim 6 wherein said first display means displays the number of the engine cylinder having the hottest cylinder head temperature, said second display means displays the temperature difference between the hottest and coldest cylinder head temperatures of the engine cylinders and said third display means displays the temperature of the cylinder head having the hottest temperature.

8. The monitoring device of claim 1 and further including switch means for selecting any of said alternate display means.

9. The monitoring device of claim 1 wherein said third plurality of temperature monitoring zones comprise the inlet pipes of the turbines of the engine, such that said third plurality of thermocouples measure the turbine inlet gas temperature of the engine.

10. The monitoring device of claim 9 wherein said first display means indicates the turbine having the hottest temperature, said second display means displays the temperature difference between the turbine inlet gas temperature of the hottest and coldest turbines and said third display means displays the turbine inlet temperature of the turbine having the hottest temperature.

11. The monitoring device of claim 1 and further including:

means for recording said temperature output signals.

19. The monitoring device of claim 1 and further including switch means for inputting a predetermined temperature value into said electronic processor.

20. The monitoring device of claim 19 wherein said predetermined temperature value equals the temperature of the hottest temperature monitoring zone within one of said first, second and third temperature monitoring zones at the time said switch means is actuated.

21. The monitoring device of claim 20 wherein said electronic processor generates a signal representing the temperature difference between the temperature monitoring zone within one of said first, second and third temperature monitoring zones having the hottest temperature and said predetermined temperature value.

22. The monitoring device of claim 21 and further including means for generating an alarm signal if the temperature monitoring zone within one of said first, second and third temperature monitoring zones having the hottest temperature exceeds said predetermined temperature value.

23. The monitoring device of claim 1 and further including switch means for manually sequentially scanning said thermocouple temperature output signals.

24. The monitoring device of claim 1 and further including an ambient light sensor for controlling the intensity of said displays.

12. A method of monitoring thermal operating characteristics of an aircraft engine comprising the steps of:

sensing the temperature of a first, second and third plurality of temperature monitoring zones within the engine;

generating first, second and third electrical sensor output signals proportional to the temperature of the corresponding first, second and third plurality of temperature monitoring zones;

converting said scanned temperature output signals to digital information;

automatically and sequentially scanning and detecting said electrical sensor output signals;

processing said detected electrical sensor output signals;

generating first, second and third temperature difference signals representing the temperature difference between the hottest and coldest temperature within said first, second and third plurality of temperature monitoring zones; and

displaying said temperature difference signals.

13. The method of claim 12 and further including displaying the number of the temperature monitoring zone within said first, second and third plurality of temperature monitoring zones having the hottest temperature.

14. The method of claim 12 and further including:

displaying the temperature of the temperature monitoring zone within said first, second and third plurality of temperature monitoring zones having the hottest temperature.

15. The method of claim 12 and further including:

generating an alarm signal if the temperature of the hottest temperature monitoring zone exceeds a predetermined temperature value.

16. The method of claim 12 and further including:

generating an alarm signal if the temperature of the coldest temperature monitoring zone is less than a predetermined temperature value.

17. The method of claim 12 and further including:

recording said temperatures corresponding to the temperatures of said monitoring zones and said temperature difference signals.

18. The method of claim 12 wherein the step of sensing the temperature of said first, second and third plurality of temperature monitoring zones comprises:

sensing the temperature of a plurality of engine cylinder heads within the engine;

sensing the temperature of the exhaust gas of the engine cylinders; and

sensing the turbine inlet temperature of the engine.