Method for controlling a trim-adjustment mechanism for a centrifugal compressor

Patent metadata

Field	Value
Publication number	US-10859097-B2
Application number	US-201815925713-A
Country	US
Kind code	B2
Filing date	Mar 19, 2018
Priority date	Mar 19, 2018
Publication date	Dec 8, 2020
Grant date	Dec 8, 2020

Abstract

A method for controlling an inlet-adjustment mechanism in an air inlet for a compressor so as to switch the mechanism in a binary fashion between open and closed positions for adjusting a flow area of the inlet. The method includes identifying a threshold line on a compressor map of pressure ratio versus corrected flow rate for the compressor, at which the inlet-adjustment mechanism is switched from one of its positions to the other. A fixed switch band straddling the threshold line can be used for determining when to initiate the switch of positions so as to time the switch to coincide with the operating point reaching the threshold line. Alternatively, a time to reach the threshold line can be instantaneously computed and compared to the actuator/mechanism response time.

First claim

What is claimed is:

1. A method for controlling a compressor inlet-adjustment mechanism disposed in an air inlet of a centrifugal compressor of a turbocharger for boosting intake pressure of an internal combustion engine, the inlet-adjustment mechanism being actuatable to switch between a closed position that reduces a flow area of the air inlet and an open position that increases the flow area of the air inlet, the method comprising:
identifying a threshold line on a compressor map of pressure ratio PR versus corrected flow rate W c for the compressor, the threshold line being a line at which the inlet-adjustment mechanism is to be moved from the open position to the closed position when an operating point of the compressor on the compressor map reaches the threshold line under a condition of quasi-static movement of the operating point, starting from a high-flow side of the threshold line;
tracking, by detecting at periodic time intervals, movement of an operating point of the compressor on the compressor map;
determining, at each said time interval, whether the operating point is on the high-flow side of the threshold line or is on a low-flow side of the threshold line;
determining, at each said time interval, whether the operating point is moving toward the threshold line;
when the operating point is determined to be on the high-flow side of the threshold line and to be moving toward the threshold line, initiating actuation of the inlet-adjustment mechanism to switch from the open position to the closed position, wherein said initiating is begun before the operating point reaches the threshold line; and
when the operating point is determined to be on the low-flow side of the threshold line and to be moving toward the threshold line, initiating actuation of the inlet-adjustment mechanism to switch from the closed position to the open position before the operating point reaches the threshold line, the method further comprising:
at each said time interval, calculating a time rate of change ΔQ/Δt, where Q is one of speed of the engine Ne, speed of the turbocharger Nt, and flow rate of the compressor Wc;
at each said time interval, calculating a distance D between the operating point and the threshold line on the compressor map;
at each said time interval, calculating, based on said distance D and said time rate of change ΔQ/Δt, a time period T TL it will take for the operating point to reach the threshold line; and
at each said time interval, making a comparison between said time period T TL and a known response time Tr for the inlet-adjustment mechanism to transition between the open and closed positions;
wherein the step of initiating actuation of the inlet-adjustment mechanism is performed based on said comparison.

2. The method of claim 1 , wherein the step of initiating actuation of the inlet-adjustment mechanism is performed when said time period T TL is approximately equal to the response time Tr.

3. A computer program product comprising at least one computer-readable storage medium having computer-executable program code instructions stored therein for controlling a compressor inlet-adjustment mechanism disposed in an air inlet of a centrifugal compressor of a turbocharger for boosting intake pressure of an internal combustion engine, the inlet-adjustment mechanism being actuatable to switch between a closed position that reduces a flow area of the air inlet and an open position that increases the flow area of the air inlet, the compressor having a compressor map of pressure ratio PR versus corrected flow rate We for the compressor, the compressor map including a threshold line at which the inlet-adjustment mechanism is to be moved from the open position to the closed position when an operating point of the compressor on the compressor map reaches the threshold line under a condition of quasi-static movement of the operating point, starting from a high-flow side of the threshold line, the computer-executable program code instructions comprising:
program code instructions for tracking, by detecting at periodic time intervals, movement of an operating point of the compressor on the compressor map;
program code instructions for determining, at each said time interval, whether the operating point is on the high-flow side of the threshold line or is on a low-flow side of the threshold line;
program code instructions for determining, at each said time interval, whether the operating point is moving toward the threshold line;
program code instructions for, in response to a determination that the operating point is on the high-flow side of the threshold line and is moving toward the threshold line, initiating actuation of the inlet-adjustment mechanism to switch from the open position to the closed position, wherein said initiating is begun before the operating point reaches the threshold line; and
program code instructions for, in response to a determination that the operating point is on the low-flow side of the threshold line and is moving toward the threshold line, initiating actuation of the inlet-adjustment mechanism to switch from the closed position to the open position before the operating point reaches the threshold line, the computer program product further comprising:
program code instructions for, at each said time interval, calculating a time rate of change ΔQ/Δt, where Q is one of speed of the engine Ne, speed of the turbocharger Nt, and flow rate of the compressor Wc;
program code instructions for, at each said time interval, calculating a distance D between the operating point and the threshold line on the compressor map;
program code instructions for, at each said time interval, calculating, based on said distance D and said time rate of change ΔQ/Δt, a time period T TL , it will take for the operating point to reach the threshold line; and
program code instructions for, at each said time interval, making a comparison between said time period T TL and a known response time Tr for the inlet-adjustment mechanism to transition between the open and closed positions, and initiating actuation of the inlet-adjustment mechanism based on said comparison.

4. The computer program product of claim 3 , wherein the step of initiating actuation of the inlet-adjustment mechanism is performed when said time period T TL is approximately equal to the response time Tr.

Assignees

• Honeywell Int Inc
• Garrett Transportation I Inc

Inventors

• Mohtar Hani
• Pohorelsky Ludek
• Davies Peter
• Pees Stephane

Classifications

• Y02T10/12

  Improving ICE efficiencies · CPC title

• F05D2270/44

  active, predictive, or anticipative · CPC title

• F05D2250/51

  Inlet · CPC title

• F05D2260/821

  Parameter estimation or prediction · CPC title

• F04D27/0253 Primary

  by throttling (F04D27/0246 takes precedence) · CPC title