Engine monitoring apparatus

• US 4,891,971 A
• Filed: 12/21/1988
• Issued: 01/09/1990
• Est. Priority Date: 12/23/1987
• Status: Expired due to Fees

• Current Assignee: Smiths Group plc (Smiths Group International Holdings Ltd.)
• Original Assignee: Smiths PLC
• Inventors: Jones, John W. D., O'Sullivan, Peter F.
• Primary Examiner(s): Myracle, Jerry W.
• Application Number:
  US07/287,238
• Time in Patent Office: 384 Days
• Field of Search: 73/116, 73/117.3, 73/117.2, 340/945, 340/959, 340/132, 364/431.01, 364/431.1, 364/431.02
• US Class Current: 73/112.01
• CPC Class Codes: F02C 7/26 Starting; Ignition

Abstract

Abnormal start conditions, such as hot starts or hung starts, in an aircraft gas-turbine engine are monitored by deriving signals indicative of spool speed, engine temperature and fuel flow. A processor receives these signals and derives an indication of the rate of change of engine temperature. Signals indicative of whether the aircraft is on the ground or in the air are derived from a air speed sensor or undercarriage pressure switch. The processor monitors the relationship between these signals to determine when the relationship between them is indicative of an abnormal start condition and indicates this on a display such as by flashing the display of engine temperature.

Claims

1. Engine monitoring apparatus for detecting abnormal start conditions of a gas-turbine engine comprising:

means for deriving a first signal indicative of spool speed;

means for deriving a second signal indicative of engine temperature ;

processing means arranged to receive the first and second signals, said processing means monitoring the dynamic relationship between the first and second signals such as to determine when the said relationship is indicative of an abnormal start condition ; and

visual display means which signals in real time a visual indication of such an abnormal start condition.

2. Engine monitoring apparatus according to claim 1, including means for deriving a third signal indicative of fuel flow.

3. Engine monitoring apparatus according to claim 1 wherein the said visual display means provides a visual display of spool speed and engine temperature.

4. Engine monitoring apparatus according to claim 1, wherein the visual display means signals abnormal start condition by flashing the visual display.

5. Engine monitoring apparatus according to claim 4, wherein the visual display means signals abnormal start condition by flashing the visual display of engine temperature.

6. Engine monitoring apparatus according to claim 1, wherein the processing unit is arranged to derive an indication of the rate of change of engine temperature and wherein the processing means is arranged to utilize the rate of change of engine temperature in determining when said relationship is indicative of abnormal start conditions.

7. Engine monitoring apparatus for an aircraft engine according to claim 1 including means for providing a fourth signal indicative of whether the aircraft is on the ground or in the air, and wherein the processing means is arranged to receive the fourth signal and to utilize the fourth signal in determining when said relationship is indicative of abnormal start conditions.

8. Engine monitoring apparatus according to claim 7, wherein said means for providing a fourth signal includes air speed sensor means.

9. Engine monitoring apparatus according to claim 7, wherein the said means for providing a fourth signal includes means for sensing pressure on the aircraft undercarriage.

10. Engine monitoring apparatus for detecting abnormal start conditions of a gas-turbine engine comprising:

means for deriving a first signal indicative of spool speed;

means for deriving a second signal indicative of engine temperature;

means for deriving a third signal indicative of fuel flow;

processing means arranged to receive the first, second and third signals, said processing means monitoring the relationship between the first, second and third signals such as to determine when the said relationship is indicative of an abnormal start condition;

visual display means;

means for supplying the first, second and third signals to the visual display means such that the visual display means provides a display of spool speed, engine temperature and fuel flow; and

means for signalling in real time to the visual display means an indication of said abnormal start condition such that the visual display means provides a visual display of said abnormal start condition.

11. Engine monitoring apparatus for detecting abnormal start conditions of a gas-turbine engine comprising:

means for deriving a signal indicative of fuel flow;

processing means arranged to monitor said signal dynamically in time to determine when an abnormal start condition is indicated; and

visual display means which signals in real time a visual indication of such an abnormal start condition.