Engine monitoring apparatus
First Claim
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.
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Accused Products
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.
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Citations
11 Claims
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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. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9)
- means for deriving a first signal indicative of spool speed;
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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.
- means for deriving a first signal indicative of spool speed;
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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.
- means for deriving a signal indicative of fuel flow;
Specification