Method for securing the operation of a turbomachine

Patent metadata

Field	Value
Publication number	US-10323538-B2
Application number	US-201314379921-A
Country	US
Kind code	B2
Filing date	Feb 19, 2013
Priority date	Feb 20, 2012
Publication date	Jun 18, 2019
Grant date	Jun 18, 2019

Abstract

A method of making safe operation of a rotary assembly of a turbomachine including a turbine and a rotary machine, the method anticipating an event of exceeding a predetermined threshold speed by repetitively performing a prediction cycle including: measuring magnitudes relating to operation of the turbomachine, including real speed of rotation of its rotary assembly; based on the magnitudes, estimating driving and resisting torques applied to the rotary assembly; preparing a representative value representative of the difference between these two torques; and calculating a predicted speed of rotation for the rotary assembly at a given time horizon based on the representative value and the real speed of rotation. An action is taken on the operation of the turbomachine to limit an extent to which its rotary assembly exceeds the threshold speed in the event of the predicted speed of rotation exceeding the threshold speed.

First claim

The invention claimed is:

1. A method of ensuring safe operation of a rotary assembly of a turbomachine, wherein the rotary assembly includes a turbine that is caused to rotate by expansion of a drive fluid that flows through the turbine, and a rotary machine that is driven mechanically into rotation by the turbine to move a driven fluid that flows through the rotary machine, wherein an event of the rotary assembly exceeding a predetermined threshold speed is anticipated by repetitively performing a prediction cycle comprising:
measuring the following magnitudes during a predetermined time interval:
a real speed of rotation of the rotary assembly at a given observation instant of the time interval;
at least one fluid/turbine interaction parameter that is representative of an interaction between the turbine and the drive fluid; and
at least one fluid/rotary machine interaction parameter that is representative of an interaction between the rotary machine and the driven fluid;

estimating driving torque applied by the turbine to the rotary assembly, based on the real speed of rotation and the at least one fluid/turbine interaction parameter;
estimating, independently of estimating the driving torque, resisting torque applied by the rotary machine to the rotary assembly, based on the real speed of rotation and the at least one fluid/rotary machine interaction parameter;
preparing a representative value that is representative of a difference between the estimated driving torque and the estimated resisting torque;
calculating a predicted speed of rotation for the rotary assembly at a prediction instant later than the observation instant based on the real speed of rotation, the representative value, and a time difference between the prediction instant and the observation instant; and
determining that a first condition is satisfied when the predicted speed of rotation exceeds the predetermined threshold speed,
wherein
an action is taken on an operation of the turbomachine to limit an extent to which the speed of the rotary assembly exceeds the threshold speed when, during the prediction cycle, it is determined that at least the first condition is satisfied, and
said action that is taken comprises modifying at least a flow rate of the drive fluid at an inlet of the turbine.

2. A method according to claim 1 , wherein the action that is taken includes an emergency stop of the turbomachine.

3. A method according to claim 1 , wherein the flow rate modification is performed by tripping at least partial opening of at least one bypass valve connected in parallel with the inlet of the turbine to reduce the flow rate of the drive fluid at the inlet of the turbine.

4. A method according to claim 1 , wherein, during the prediction cycle, it is determined that a second condition is satisfied in the event that the turbomachine is not operating under transient conditions; and
wherein the action is taken when, during the prediction cycle, it is determined that at least the first and the second conditions are both satisfied.

5. A method according to claim 4 , wherein the second condition is satisfied when a derivative of an inlet flow rate to the rotary machine is greater than a predetermined threshold.

6. A method according to claim 1 , wherein, to prepare the representative value during the prediction cycle, at least one of the torques estimated from among the driving torque and the resisting torque is corrected to attenuate measurement noise associated with the measured magnitudes.

7. A method according to claim 1 , wherein, to prepare the representative value during the prediction cycle, a value bias that exists between the driving torque and the resisting torque as a result of the driving torque and the resisting torque being estimated independently of each other is attenuated.

8. A method according to claim 7 , wherein, to prepare the representative value during the prediction cycle, the driving torque and the resisting torque are corrected to attenuate measurement noise associated with the measured magnitudes, and then the difference is calculated between the corrected driving torque and the corrected resisting torque, and then the difference is corrected to attenuate the value bias.

9. A method according to claim 1 , wherein, during the prediction cycle, three fluid/turbine interaction parameters, consisting of an inlet pressure of the turbine, an outlet pressure of the turbine, and a temperature of the drive fluid at the inlet of the turbine are measured, and the driving torque is estimated based on the real speed of rotation and the three fluid/turbine interaction parameters.

10. A method according to claim 1 used to ensure safe operation of the rotary assembly of a turbomachine, the turbomachine including the turbine and a pump.

11. A method according to claim 10 , wherein, during the prediction cycle, a flow rate of the driven fluid is measured at an inlet of the pump as the fluid/rotary machine interaction parameter; and the resisting torque is estimated based on the real speed of rotation and the measured flow rate.

12. A method according to claim 1 , wherein the time difference between the prediction instant and the observation instant is between 1 millisecond and 25 milliseconds.

Assignees

• Safran Aircraft Engines

Inventors

• Lemaitre Alban
• Le Gonidec Serge

Classifications

• F01D17/08

  responsive to condition of working-fluid, e.g. pressure · CPC title

• F02K9/48

  driven by a gas turbine fed by propellant combustion gases {or fed by vaporized propellants or other gases} · CPC title

• F02C9/00

  Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants (controlling air intakes F02C7/057; controlling turbines F01D; controlling compressors F04D27/00; controlling in general G05) · CPC title

• F05D2270/44

  active, predictive, or anticipative · CPC title

• F04D13/04

  the pump being fluid driven · CPC title