IP Library Granted Patent US 7,448,853
Granted Patent B2
US 7,448,853 · App. 11/103,864 · Granted Nov 11, 2008

System and method of determining centrifugal turbomachinery remaining life

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Quick Facts
Patent No.
US 7,448,853
App. No.
11/103,864
Granted
Nov 11, 2008
Kind
B2
Abstract

A centrifugal turbomachine includes an impeller and a speed sensor arranged to detect a speed associated with an impeller speed. A temperature sensor is arranged to detect a temperature associated with an impeller exit temperature. A controls system has impeller parameters, which includes the impeller speed and exit temperature. A calculation methodology is used to mathematically manipulate the impeller parameters to determine a remaining life of the impeller. A program response, such as a warning indication, is triggered by the control system in response to the remaining life reaching a threshold. The controls system monitors the speed and temperature of the impeller. The controls system internally calculates the remaining life based upon the speed and the temperature. In one example, a change in remaining life is calculated in response to a change in speed that results in an impeller stress that exceeds an endurance strength for the impeller.

Claims (30)

1. A turbomachine comprising:

an impeller;

a speed sensor arranged to detect a speed associated with an impeller speed;

a temperature sensor arranged to detect a temperature associated with an impeller exit temperature;

a controls system having impeller parameters including impeller speed and exit temperature, a calculation methodology mathematically manipulating the impeller parameters to determine a remaining life of the impeller, and a programmed response triggered by the controls system in response to the remaining life reaching a threshold; and

wherein the impeller parameters include stress characteristics of the impeller having fatigue strength modification factors including at least one of impeller surface finish, load on an impeller area, and size of an impeller feature.

2. The centrifugal turbomachine according to claim 1 , wherein said speed sensor detects a speed of a shaft supporting the impeller.

3. The centrifugal turbomachine according to claim 1 , wherein the temperature sensor is arranged near an impeller exit.

4. The centrifugal turbomachine according to claim 1 , wherein the calculation methodology is based upon Palmgren-Miner cycle-ratio summation.

5. The centrifugal turbomachine according to claim 1 , wherein the calculation methodology is based upon Manson's approach.

6. The centrifugal turbomachine according to claim 1 , wherein the impeller parameters include material properties of the impeller.

7. The centrifugal turbomachine according to claim 1 , wherein the stress characteristics include at least one of maximum impeller stress as a function of speed, fatigue strength as a function of temperature, stress ratio, and cycles to failure relative to maximum stress.

8. The centrifugal turbomachine according to claim 1 , wherein the programmed response is a warning indication.

9. A method of calculating impeller remaining life comprising the steps of:

a) monitoring a speed of an impeller;

b) monitoring a temperature associated with the impeller;

c) iteratively calculating a remaining life of the impeller based upon a change in the speed and the temperature;

d) producing a warning indication when the remaining life reaches a threshold; and

e) avoiding an undesired change in speed when the remaining life reaches the threshold.

10. The method according to claim 9 , wherein step c) includes iteratively calculating remaining life at a rate corresponding a stress cycle produced by the change in speed.

11. The method according to claim 10 , wherein step c) includes calculating a change in life attributable to the change in speed.

12. The method according to claim 9 , wherein step c) is based upon calculating the remaining life as a function of a stress ratio.

13. The method according to claim 9 , wherein step c) uses a maximum design stress of the impeller.

14. A turbomachine comprising:

an impeller;

a speed sensor arranged to detect a speed associated with an impeller speed;

a temperature sensor arranged to detect a temperature associated with an impeller exit temperature; and

a controls system having impeller parameters including impeller speed and exit temperature, a calculation methodology mathematically manipulating the impeller parameters to determine a remaining life of the impeller based upon changes in the impeller speed, and a programmed response triggered by the controls system in response to the remaining life reaching a threshold, the programmed response including avoidance of undesired changes in the impeller speed.

15. The turbomachine according to claim 14 , wherein the avoidance of undesired changes in the impeller speed includes operating the impeller at a fixed speed.

16. The turbomachine according to claim 15 , wherein the fixed speed includes a full speed condition.

Assignments (13)
RELEASE OF FIRST LIEN PATENT SECURITY INTERESTS Recorded Jun 6, 2025
From: MORGAN STANLEY SENIOR FUNDING, INC.
To: HMD SEAL/LESS PUMPS LIMITED; SUNDYNE, LLC
Reel/Frame 071530/0267 →
RELEASE OF SECOND LIEN PATENT SECURITY INTERESTS Recorded Dec 19, 2023
From: BANK OF MONTREAL
To: HMD SEAL/LESS PUMPS LIMITED; SUNDYNE, LLC
Reel/Frame 066075/0120 →
SECOND LIEN SECURITY AGREEMENT Recorded Jun 22, 2022
From: SUNDYNE, LLC
To: BANK OF MONTREAL
Reel/Frame 060404/0239 →
RELEASE OF SECURITY INTEREST Recorded Mar 17, 2020
From: MORGAN STANLEY SENIOR FUNDING, INC., AS COLLATERAL AGENT
To: HMD SEAL/LESS PUMPS LIMITED; SUNDYNE, LLC
Reel/Frame 052142/0908 →
SECURITY AGREEMENT Recorded Mar 17, 2020
From: SUNDYNE, LLC
To: MORGAN STANLEY SENIOR FUNDING, INC.
Reel/Frame 052184/0691 →
RELEASE OF SECURITY INTEREST Recorded May 21, 2019
From: MORGAN STANLEY SENIOR FUNDING, INC., AS COLLATERAL AGENT
To: ACCUDYNE INDUSTRIES, LLC; HASKEL INTERNATIONAL, LLC; MILTON ROY, LLC; SUNDYNE, LLC
Reel/Frame 049243/0092 →
SECURITY INTEREST Recorded May 21, 2019
From: HMD SEAL/LESS PUMPS LIMITED; SUNDYNE, LLC
To: MORGAN STANLEY SENIOR FUNDING, INC., AS COLLATERAL AGENT
Reel/Frame 049242/0255 →
SECURITY INTEREST Recorded Aug 23, 2017
From: ACCUDYNE INDUSTRIES, LLC; HASKEL INTERNATIONAL, LLC; MILTON ROY, LLC; SUNDYNE, LLC
To: MORGAN STANLEY SENIOR FUNDING, INC., AS COLLATERAL AGENT
Reel/Frame 043373/0798 →
TERMINATION AND RELEASE OF SECURITY INTEREST IN PATENTS RECORDED AT REEL/FRAME 029530/0539 Recorded Aug 18, 2017
From: DEUTSCHE BANK AG NEW YORK BRANCH, AS COLLATERAL AGENT
To: SUNDYNE, LLC
Reel/Frame 043602/0619 →
SECURITY AGREEMENT Recorded Dec 20, 2012
From: SUNDYNE, LLC
To: DEUTSCHE BANK AG NEW YORK BRANCH, AS COLLATERAL AGENT
Reel/Frame 029530/0539 →
CONVERSION OF CORPORATION TO LLC Recorded Dec 4, 2012
From: SUNDYNE CORPORATION
To: SUNDYNE, LLC
Reel/Frame 029405/0017 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 16, 2012
From: SUNDYNE CORPORATION
To: SUNDYNE CORPORATION; GARDNER DENVER DEUTSCHLAND GMBH
Reel/Frame 027536/0541 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 12, 2005
From: MABE, WILLIAM J.; MAYS, HAROLD J.
To: SUNDYNE CORPORATION
Reel/Frame 016467/0670 →