Warning before pump limit or in case of blade failure on a turbomachine
AssigneeMTU Aero Engines AG
InventorFrank Grauer
Life of this patent
Estimating the term…
Loading patent…
AssigneeMTU Aero Engines AG
InventorFrank Grauer
Estimating the term…
In a method for determination of a surge limit warning (W) for a turbocompressor, or a warning of blade damage, at least two measurement signals (p1, p2; {tilde over (p)}1, {tilde over (p)}2), are determined, a periodicity value (W1; {tilde over (W)}1) is calculated from at least one of the measurement signals (p1, p2; {tilde over (p)}1, {tilde over (p)}2), indicating a measure for the occurrence of periodic signal level changes in the at least one measurement signal (p1, p2; {tilde over (p)}1, {tilde over (p)}2) for a predetermined first time offset (t1), a correlation value (w2; {tilde over (w)}2) is calculated from the at least two measurement signals (p1, p2; {tilde over (p)}1, {tilde over (p)}2), indicating a measure for the similarity of the at least two measurement signals (p1, p2; {tilde over (p)}1, {tilde over (p)}2) to one another for a predetermined second time offset (t2), and the surge limit warning (W) or the warning of blade damage (W) is determined from the periodicity value (W1; {tilde over (W)}1) and the correlation value (W2; {tilde over (W)}2). A method for operation of a gas turbine or of a turbomachine as well as a turbocompressor and a gas turbine have corresponding features.
1-15. (Canceled)
A method for determining a warning regarding a surge limit for a turbocompressor or of blade damage to a rotor in a turbomachine, the method comprising:
A turbocompressor comprising:
A gas turbine comprising:
A method for determining a surge limit warning for a turbocompressor or a warning of blade damage to a rotor in a turbomachine, said method comprising:
Dependencies are inferred from the claim text.