Method and system for controlling a turbocompressor group
View Patent ↗A method for controlling at least two turbocompressors ( 1.1, 2.1 ), each having a control device ( 1.2, 2.2 ) for maintaining a distance relative to a surge limit curve (P 1 , P 2 ) of the respective turbocompressor; wherein a first distance (A 1.1 , A 2.1 ) is determined for each turbocompressor from its surge limit curve; wherein the distance to be maintained can be trimmed relative to this first distance in the control devices; and wherein the distance (A 2.2 ) of a control device ( 2.2 ) to be maintained is trimmed relative to its first distance (A 2.1 ) based on a trimming (A 1.1 →A 1.2 ) of another control device ( 1.2 ) in such a way that a total process variable (dV/dt) remains substantially constant.
1. A method for controlling at least two turbocompressors ( 1 . 1 , 2 . 1 ), each having a control device ( 1 . 2 , 2 . 2 ) for maintaining a distance of an operating point (B 1 . 1 , B 2 . 1 ) relative to a surge limit curve (P 1 , P 2 ) of the respective turbocompressor, said method comprising:
(a) determining a first distance (A 1 . 1 , A 2 . 1 ) of an operating point for each turbocompressor from its respective surge limit curve (P 1 , P 2 );
(b) trimming the first distance of the operating point (B 1 . 1 ) of a first turbocompressor to arrive at a desired distance (A 1 . 2 ) of an operating point (B 1 . 2 ) relative to the surge limit curve; and
(c) trimming the first distance of the operating point (B 2 . 1 ) of at least a second turbocompressor based on the trimming of the first turbocompressor so that a total process variable remains substantially constant,
wherein step (a) is performed so that the first distance is substantially identical for all turbocompressors.
2. The method according to claim 1 , wherein the total process variable comprises one or more of a total flow rate, a total flow capacity (dV/dt), a total suction pressure, a total final pressure and a total pressure ratio (Δp).
3. The method according to claim 1 , comprising controlling three or more turbocompressors; and wherein the desired distance of an operating point to the respective surge limit curve is trimmed relative to the first distance based on the trimming of the remaining turbocompressors in such a way that a total process variable remains substantially constant.
4. The method according to claim 1 , wherein the desired distances are trimmed relative to their respective first distance based on the trimming of the other turbocompressors.
5. The method of claim 1 , additionally comprising the step of communicating the respective trimming distance between the at least two turbocompressors; and trimming the desired distance of an operating point of a turbocompressor to its surge limit curve relative to its first distance based on said communicated trimming.
6. A system for controlling at least two turbocompressors ( 1 . 1 , 2 . 1 ) comprising control devices ( 1 . 2 , 2 . 2 ) for maintaining distances from the surge limit curves of the respective turbocompressors; and wherein said control devices are configured for implementing the method according to claim 1 .
7. A non-transitory computer readable medium comprising a program code for carrying out the method according to claim 1 .