Method of detecting a liquid fuel leak in a gas turbine

• US 20110282501A1
• Filed: 12/06/2010
• Published: 11/17/2011
• Est. Priority Date: 12/07/2009
• Status: Abandoned Application

• Current Assignee: GE Energy Products France SNC (GE Vernova, Inc.)
• Original Assignee: GE Energy Products France SNC (GE Vernova, Inc.)
• Inventors: Martin, Denis
• Application Number:
  US12/961,116
• Publication Number:
  US 20110282501A1
• Time in Patent Office: Days
• US Class Current: 700/287
• CPC Class Codes: F01D 19/00 Starting of machines or engines; Regulating, controlling, or safety means in connection therewith warming-up before starting F01D25/10; turning or inching gear F01D25/34
• CPC Class Codes: F01D 21/14 responsive to other specific conditions
• CPC Class Codes: F02C 9/28 Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed F02C9/30 - F02C9/38, F02C9/44 take precedence
• CPC Class Codes: F02C 9/46 Emergency fuel control
• CPC Class Codes: F05D 2260/80 Diagnostics

Abstract

The invention relates to a method of detecting the presence of a liquid fuel leak in a gas turbine (1). During this method:

a reference value (27, 37) is determined for at least a first operating parameter of the turbine,

a value (29, 39) of the said operating parameter is measured during a start-up phase of the turbine,

the measurement value and the reference value are compared,

whether a first anomaly (13, 41) is present is identified,

an alert notification (33, 43) is generated if a first anomaly (31, 41) is detected for the first parameter, and in parallel

shutdown of the turbine (35, 45) is triggered if a second anomaly (34, 44) is detected for a second parameter.

The invention also relates to a device for detecting a liquid fuel leak in a gas turbine, employing such a method.

Claims

1. Method of detecting the presence of a liquid fuel leak in a gas turbine (1), characterized in that:

a reference value is determined for at least a first operating parameter of the turbine,

a value of the said operating parameter is measured during a start-up phase of the turbine,

the measurement value and the reference value are compared,

whether a first anomaly is present is identified,

an alert notification is generated if a first anomaly is detected for the first parameter, and

shutdown of the turbine is triggered if a second anomaly is detected for a second parameter.

2. Method according to claim 1, characterized in that the measurement step for the said operating parameter is carried out during the start-up phase between shutdown of the activating system of the turbine and detection of at least one combustion flame.

3. Method according to one of claims 1 and 2, characterized in that a value of a second operating parameter is measured during the start-up phase, the measured value and a reference value are compared, whether an anomaly is present is identified and shutdown of the turbine is triggered if a second anomaly is detected, a value of a third operating parameter is measured during the start-up phase, the measured value of the third operating parameter is compared with a reference value, whether an anomaly is present is identified and shutdown of the turbine is triggered if a third anomaly is detected.

4. Method according to one of claims 1 to 3, characterized in that the operating parameters comprise the liquid fuel flow rate and/or the acceleration of the rotation speed of the turbine and/or the opening of intake air valves of the compressor and the rotation speed of the turbine.

5. Method according to any one of claims 1 to 4, characterized in that before measuring the value of the said parameter and comparing the said parameter with the reference value, a check is made that the rotation speed of the turbine is less than a predetermined percentage of the full speed of the turbine and that the blades are being opened.

6. Method according to claim 5, characterized in that a check is made that the rotation speed of the turbine is less than 90% of the full speed of the turbine.

7. Method according to one of them claims 5 and 6, in which, if the condition relating to the rotation speed of the turbine being less than a predetermined percentage of the full speed of the turbine, and the condition relating to the opening rate of the blades are satisfactory, the flow rate is measured for a predetermined duration, for example 5 seconds, and a corresponding reference value is determined for the flow rate and, if the measured value is equal to the reference value for the said determined duration, an anomaly is detected and the turbine is shut down.

8. Method according to any one of claims 1 to 7, characterized in that, the operating parameter being the liquid fuel flow rate, its reference value (37) is determined, its value (39) is measured during the start-up phase of the turbine, the reference value and the measured value are compared, and if the measured value is greater than the reference value for a predetermined duration, for example at least 15 seconds, an anomaly is detected and the turbine is shut down.

9. Method according to claim 8, characterized in that the reference value (27) is the maximum value of the liquid fuel flow rate which is permissible during start-up of the turbine.

10. Method according to any one of the preceding claims, characterized in that, the operating parameters being the acceleration of the turbine, its reference value (27) is determined, its value (29) is measured during the start-up of the turbine, the reference value and the measured value are compared, and if the measured value is less than a predetermined percentage of the reference value, a first anomaly (31) is identified and an alert notification (33) is generated.

11. Method according to any one of claims 4 to 10, characterized in that if, simultaneously with a first acceleration anomaly, the measured value (39) of the liquid fuel flow rate is greater than its reference value (37) for at least 15 seconds, a second anomaly (44) is identified and shutdown of the turbine (45) is triggered.

12. Method according to any one of the preceding claims, characterized in that after triggering shutdown of the turbine, a step of purging the ejection duct for the liquid fuel is carried out for at least 5 minutes, at most 5 seconds after the loss of the flame.

13. Device for detecting a liquid fuel leak in a gas turbine (1), the turbine comprising a device (9) for monitoring the operating parameters of the turbine and a storage medium readable by a computer, in which computer program instructions executable by the said device (9) are stored, the instructions of the computer program making the parameter monitoring device (9):

determine a reference value for a first operating parameter of the turbine,

measure a value for the same operating parameter after start-up of the turbine,

compare the reference and measured values,

identify whether a first anomaly is present according to predetermined characteristics,

generate an alert notification if a first anomaly is detected for a first parameter, and in parallel

trigger shutdown of the turbine if a second anomaly is detected for a second parameter.