Granted Patent B2

US 12,416,311 · App. 19/004,286 · Granted Sep 16, 2025

Inventors: Alberto Traverso (Novi Ligure, IT); Paolo Silvestri (Genoa, IT); Federico Reggio (Genoa, IT); Carlo Alberto Niccolini (Genoa, IT); Marco Ferrando (Genoa, IT); William T. Cousins (East Hartford, CT); Raffaele Spezia (Genoa, IT)

F04D27/02F04D25/06F04D27/0292

Abstract

Claims (112)

1. A method of determining an operating state of a compressor, equipped with a rotor that exchanges energy with a known fluid by rotating at a speed (N) and with a driving mechanical torque (Tor), and of determining an operating point of the compressor and a distance of the operating point from a surge limit curve, the surge limit curve delimiting a stable operation zone from an unstable operation zone of the compressor, the method comprising:

defining a compressor map to be provided as a two-dimensional locus of possible operating points of the compressor and expressed as a function of a reduced mechanical torque Tor red of a rotor and a reduced number of revolutions N red of the rotor, being

Tor

red

=

⁢

Tor

kp

0

⁢

i

⁢

n

and

N

red

=

N

kZRT

0

⁢

i

⁢

n

;

determining a surge limit curve as a set of points within the compressor map;

periodically detecting instantaneous operating parameters of the compressor during operation, from: mechanical torque of the rotor (Tor), number of revolutions of the rotor (N), pressure (p 0in ) of a fluid entering the compressor, and/or temperature (T 0in ) of the fluid entering the compressor;

determining instantaneous operating conditions from a value of a reduced mechanical torque (Tor red ) of the rotor and a reduced number of revolutions (N red ) of the rotor;

comparing the instantaneous operating conditions as detected with the surge limit curve within the compressor map; and

generating one or more notifications about the operating state of the compressor and/or control signals of the compressor from a comparison with the preceding step.

2. The method according to claim 1 , wherein the compressor map is determined as a two-dimensional map in a x-y plane having, as a first coordinate, a ratio between the reduced mechanical torque (Tor red ) and the reduced number of revolutions (N red ), and having, as a second coordinate, a mathematical power of the reduced number of revolutions (N red ) to an exponent (exp) greater than 1.

3. The method according to claim 2 , wherein the exponent is between 2 and 10.

4. The method according to claim 2 , wherein a value of the exponent (exp) is further determined as a function of a specific thermal ratio (k) of the fluid that exchanges energy with the compressor.

5. The method according to claim 1 , wherein generating one or more notifications about the operating state of the compressor and/or control signals of the compressor further comprises defining a surge margin curve, provided as a locus of points belonging to a stable operating zone of the compressor and arranged at a known and predefined distance from the surge limit curve.

6. The method according to claim 5 , wherein a distance between the surge margin curve and the surge limit curve constitutes a surge margin (Kp) and is calculated in such a way that for a same reduced number of revolutions (Nred), there is a linear relationship between a stability margin and a reduced flow rate defined as

m

˙

red

=

m

.

⁢

ZRT

0

⁢

i

⁢

n

p

0

⁢

i

⁢

n

/

m

˙

crit

.

7. The method according to claim 5 , further comprising:

providing the compressor as a dynamic compressor equipped with variable guiding vanes;

measuring an opening angle of the variable guiding vanes; and

replicating the compressor maps and stability limit curves as the opening angle varies.

8. The method according to claim 5 , further comprising:

providing the compressor as a dynamic compressor connected to, and driven by, an electric driver;

detecting an amount of electrical current absorbed by the electric driver connected to the compressor and an electrical operating voltage of the electric driver of the compressor;

determining the driving torque (Tor) of the compressor as a function of the electric current absorbed by the electric driver; and

determining the rotation speed of the rotor (N) as a function of the electrical operating voltage and/or as a function of an operating frequency of the electric driver.

9. The method according to claim 8 , wherein the step of generating one or more notifications and/or control signals comprises:

determining an electrical current signal representative of an instantaneous current of the electric driver during operation;

determining an electrical frequency signal representative of an instantaneous electrical frequency of a supply voltage of the electric driver during operation;

performing a first bandpass filtering of the electric current signal using a bandpass filter centered around the instantaneous electrical frequency of the supply voltage of the electric driver;

determining an envelope of a previously filtered signal;

performing a second bandpass filtering of a previously determined envelope signal;

comparing the signal thus obtained with a reference value or with a range of reference values; and

generating a notification and/or control signal based on a comparison obtained in the preceding step.

10. The method according to claim 8 , further comprising:

connecting the dynamic compressor to, and operating the compressor by, an electric machine:

determining a time scale of compressor instability phenomena; and

using a driving system for the electric machine that drives the dynamic compressor, the driving system being of inverter type and being equipped with a control module operating with an internal clock at a frequency equal to, or greater than, at least one order of magnitude of a largest frequency of unstable phenomena of the dynamic compressor.

11. A system for monitoring an operating state of a compressor comprising a rotor, and for predicting and determining a surge state of the compressor, the system comprising:

means for detecting the operating state of the compressor in terms of mechanical driving torque (Tor) and rotation speed (N) of the rotor;

sensors to detect pressure (p 0in ) and temperature (T 0in ) of a fluid entering the compressor;

an electronic control unit comprising a processor and a memory where a map of the compressor is loaded, provided as a two-dimensional location of possible operating points of the compressor and expressed as a function of a reduced mechanical torque Tor red of the rotor and a reduced number of revolutions N red of the rotor, being

Tor

red

=

⁢

Tor

kp

0

⁢

i

⁢

n

and

N

red

=

N

kZRT

0

⁢

i

⁢

n

;

a set of software instructions loaded into the memory which, when executed by the processor, carry out the method according to claim 1 for predicting and determining a surge state of the compressor; and

a module that generates at least one notification signal for the operating state of the compressor and/or a control signal for the compressor.

12. The system according to claim 11 , wherein the means for detecting the operating state of the compressor in terms of the mechanical driving torque (Tor) consist of an electric current sensor for detecting an electric current absorbed by a compressor driver.

13. The system according to claim 11 , further comprising an additional module for processing an electrical signal detected by the means for detecting the operating state of the compressor and the sensor to detect the pressure (p 0in ) and temperature (T 0in ) of the fluid entering the compressor.

14. The system according to claim 13 , wherein the additional module for processing the electrical signal is of electronic type with passive and/or active components and/or is provided with digital signal processing submodules.

Assignments (1)

Priority Claims (1)

Continuity (1)

References Cited (20)