Methods and apparatus for model based shrouded bellows stiffness determinations

• US 7,103,520 B1
• Filed: 08/31/2000
• Issued: 09/05/2006
• Est. Priority Date: 08/31/2000
• Status: Expired due to Term

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Shaw, Mark Richard, Vonderau, Christen Staton
• Primary Examiner(s): Knight, Anthony
• Assistant Examiner(s): STEVENS, THOMAS H
• Application Number:
  US09/652,097
• Time in Patent Office: 2,196 Days
• Field of Search: 703/9, 703/1, 703/7, 736/22
• US Class Current: 703/9
• CPC Class Codes: G06F 2111/10 Numerical modelling
• CPC Class Codes: G06F 2113/14 Pipes
• CPC Class Codes: G06F 30/23 using finite element methods [FEM] or finite difference methods [FDM]

Abstract

A modeling system predicts natural frequency responses in tube sub-systems including shrouded bellows components. The system determines a stiffness multiplier from input values and uses the determined flexibility factor to determine the natural frequency responses. The input values include geometry inputs and dynamic operating condition inputs. The flexibility factor is determined with a regression equation. The regression equation, based on dynamic stiffness test data of various shrouded bellows configurations, permits the system to characterize the shrouded bellows using a geometry element that includes an assigned flexibility factor based on dynamic stiffness test data.

Claims

1. A computer-implemented method for predicting natural frequency responses, said method comprising the steps of:

providing at least one tube sub-system including a plurality of shrouded bellows components;

determining a stiffness multiplier within each of the shrouded bellows components using a regression technique based on dynamic stiffness test data;

inputting the determined stiffness multiplier into a computer model that applies a standard geometry element and a flexibility factor based upon the stiffness multiplier to predict a natural frequency response; and

determining locations for duct supports based on the natural frequency response.

2. A method in accordance with claim 1 further comprising the step of inputting dynamic system operating inputs into the model.

3. A method in accordance with claim 2 wherein said step of inputting dynamic system operating inputs further comprises the step of inputting at least an operating pressure and vibratory environment into the model.

4. A method in accordance with claim 2 further comprising the step of inputting geometry inputs including at least one of a bellows pitch and a mating tube diameter into the model.

5. A method in accordance with claim 3 further comprising the step of determining the stiffness of the at least one tube sub-system as a function of the stiffness multiplier.

6. Apparatus for determining natural frequency response of shrouded bellows components, said apparatus comprising a processor configured to:

determine a stiffness multiplier within the shrouded bellows components using a regression technique based on dynamic stiffness test data;

use the determined stiffness multiplier in a model that applies a standard geometry element and a flexibility factor based upon the stiffness multiplier to predict a natural frequency response of the bellows; and

determine a location of a duct support based on the natural frequency response.

7. Apparatus in accordance with claim 6 wherein said model is configured to utilize shrouded bellows geometry inputs and dynamic operating condition inputs to determine the stiffness multiplier.

8. Apparatus in accordance with claim 7 wherein the bellows geometry inputs include at least one of a tube sub-system diameter and a bellows pitch.

9. Apparatus in accordance with claim 7 wherein the dynamic operating condition inputs include at least an operating pressure.

10. Apparatus in accordance with claim 6 wherein the stiffness multiplier is adjustable such that a dynamic stiffness of the shrouded bellows is selectively variable.