Data link for gas turbine engine control

• US 4,992,946 A
• Filed: 06/20/1988
• Issued: 02/12/1991
• Est. Priority Date: 06/20/1988
• Status: Expired due to Term

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Butz, Mark G., Berg, James A.
• Primary Examiner(s): NOT, DEFINED
• Application Number:
  US07/208,720
• Time in Patent Office: 967 Days
• Field of Search: 364/431.01, 364/431.02, 364/550, 364/551.01, 364/900, 340/973
• US Class Current: 701/100
• CPC Class Codes: F02C 9/48 Control of fuel supply conjointly with another control of the plant with nozzle section control F02K1/17
• CPC Class Codes: G07C 3/00 Registering or indicating the condition or the working of machines or other apparatus, other than vehicles
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

The invention concerns an interface for a digital electronic control for a gas turbine engine. The interface allows one to gain access to random access memory in the control, wherein data of interest is stored. The data includes information about present operating conditions of the engine, such as component speeds and temperatures, as well as data concerning the health of components. The data is in digital format, but is converted into analog format within the control and transmitted from the control in analog format. The analog data is used to drive a recording device, such as a strip chart recorder, thus allowing information about the engine to be transmitted to a location remote from the engine, in real time.

Claims

1. In a digital electronic control for a gas turbine engine, which controls fuel metering to the engine, and which includes a microprocessor, memory, and digital-to-analog convertors (D/A'"'"'s), the improvement comprising:

(a) interface means, located remote from the control, for instructing the microprocessor to transmit data to a D/A, the interface means being removable from the control without disrupting engine operation; and

(b) display means, located remote from the control, for receiving output signals from the D/A.

2. Apparatus according to claim 1 in which the display means comprises a recording means for recording the data which is displayed.

3. In a digital electronic control, having a microprocessor, for a gas turbine engine, and which meters fuel delivery to the engine, the improvement comprising:

(a) a first group of digital-to-analog convertors (D/A'"'"'s) for

(i) receiving digital signals from the microprocessor,

(ii) converting the digital signals to analog signals, and

(iii) sending analog signals to actuators which actuate engine components; and

(b) a second group of one or more D/A'"'"'s for

(i) receiving digital signals from the microprocessor,

(ii) converting the digital signals to analog signals, and

(iii) sending analog signals to a recording system located external to the engine, the recording system being removable from the D/A'"'"'s without disrupting engine operation.

4. An electronic control for a gas turbine engine, which controls fuel delivery to the engine, comprising:

(a) a processor;

(b) memory for storing digital words;

(c) a digital data bus for carrying digital words between the memory and the processor;

(d) at least one digital-to-analog (D/A) converter which can receive input from the digital data bus;

(e) a recording device located remote from the control, the recording device being removable from the control without disrupting engine operation; and

(f) a line for carrying analog signals to the recording device from the D/A.

5. In a digital electronic control for a gas turbine engine, which controls fuel delivery to the engine, the improvement comprising:

(a) a processor for

(i) receiving information, from a source external to the control, as to memory addresses of data and, for each address, types of computational processing for the data therein, the source being removable from the control without disrupting engine operation; and

(ii) sending the data, after the processing, to a digital data bus; and

(b) one or more digital-to-analog signal convertors for

(i) receiving processed data from the bus;

(ii) converting the processed data to analog form; and

(iii) sending the data in analog form to a recording device external to the engine.

6. In a digital electronic control for a gas turbine engine, the improvement comprising:

(a) a processor for

(i) receiving information as to

(A) memory addresses of data and,

(B) for each address, types of computational processing to be performed on the data located there,

the information being sent by a computer located external to the engine, which comprises means for performing one or more of the following procedures;

(A) masking the data,

(B) shifting the data,

(C) scaling the data, and

(D) biasing the data; and

(ii) sending the data, after the processing, to a digital data bus; and

(b) one or more digital-to-analog signal convertors for

(i) receiving processed data from the bus;

(ii) converting the processed data to analog form; and

(iii) sending the data in analog form to a recording device external to the engine.

7. In a gas turbine engine, a method of obtaining printed data from a digital electronic engine control, which controls fuel delivery to the engine, and which includes a microprocessor, a random access memory (RAM), and digital-to-analog convertors (D/A'"'"'s), all linked by a common digital data bus, comprising the following steps:

(a) using one of the D/A'"'"'s, transmitting an analog signal derived from data at a RAM address to a location remote from the control; and

(b) recording the analog signal during transmission on a recording device which is removable from the control without disrupting operation of the engine.

8. In a digital electronic control for a gas turbine engine which controls fuel delivery to the engine, and which includes digital-to-analog convertors (D/A'"'"'s), the method comprising the steps of:

(a) transmitting digital data to a D/A for conversion to analog form; and

(b) transmitting the data in analog form to a recording device outside the engine, the recording device being removable from the control without disrupting operation of the engine.

9. A method according to claim 8 and further comprising the steps of storing the digital data in memory prior to transmission to a D/A, and updating the stored digital data more often that once every 0.015 seconds.

10. In a digital electronic control for a gas turbine engine which controls fuel delivery to the engine, and includes digital-to-analog convertors (D/A'"'"'s) which are contained in integrated circuit packages, each package of which contains two or more D/A'"'"'s, the method comprising the steps of:

(a) transmitting digital data to a D/A for conversion to analog form; and

(b) transmitting the data in analog form to a recording device outside the engine, the recording device being removable from the control without disrupting operation of the engine.

11. In a gas turbine engine, a method of obtaining printed data from a digital electronic engine control, which controls fuel deliver to the engine, and which includes a microprocessor, random access memory (RAM), and digital-to-analog convertors (D/A'"'"'s), all linked by a common digital data bus, comprising the following steps:

(a) using a first D/A, providing a first analog signal based on a first digital word in RAM to a first line;

(b) using a second D/A, providing a second analog signal based on a second digital word in RAM to a second line;

(c) displaying, remote from the control, a visual indication of the first analog signal substantially at the same time as it occurs; and

(d) displaying, remote from the control, indications when a change occurs in the second analog signal.

12. The method according to claim 11 in which the first digital word indicates engine speed.

13. The method according to claim 11 in which the changes in the second analog signal indicate status of engine components.

14. The method according to claim 11 in which the first and second lines provide signals to respective first and second pens of a strip chart recorder.

15. In a gas turbine engine, a method of obtaining printed data from a digital electronic engine control, which controls fuel delivery to the engine, and which includes a microprocessor, random access memory (RAM), and digital-to-analog convertors (D/A'"'"'s), all linked by a common digital data bus, comprising the following steps:

(a) instructing the microprocessor to periodically provide, to a first D/A, a first digital signal derived from a first digital word residing at a first RAM location;

(b) instructing the microprocessor to periodically provide, to a second D/A, a second digital signal derived from a second digital word residing at a second RAM location;

(c) transmitting signals from the first and second D/A'"'"'s to a display located remote from the control; and

(d) displaying, on the display, a visual representation of the time-history of the first and second digital words.

16. The method according to claim 15 in which the first digital word indicates engine speed.

17. The method according to claim 15 in which the second digital word indicates a failure in an engine component.

18. In a digital control for a gas turbine engine which controls fuel delivery to the engine, and which includes a plurality of digital-to-analog converters (D/A'"'"'s), the improvement comprising

(a) means for connecting one or more D/A'"'"'s to a recording device located remote from the engine, the recording device being removable without disrupting normal engine operation;

and

(b) means for causing the control to transmit selected data to the recording device.