# Presentation: 379426

## Weibull Strength Parameter Requirements for Si3N4 Turbine Rotor Reliability

*DER Program*

***Weibull Strength Parameter Requirements for Si******3******N******4****** Turbine Rotor Reliability***

*Steve Duffy & Eric Baker*
*Connecticut Reserve Technologies, LLC*
*Jim Kesseli*
*Ingersoll-Rand Energy Systems*
*Andy Wereszczak*
*Oak Ridge National Laboratory*
*Curt Johnson*
*General Electric Corporate Research & Development*

***Presented at the*** ***Environmental Barrier Coatings Workshop***
***November 18-19, 2003***
***Gaylord Opryland Resort & Convention Center***
***Nashville, Tennessee, USA***

## DER Program

*DER Program*

***Scope***
*A method to define Weibull distribution metrics for Si**3**N**4** vendors, in particular, and ceramic material developers, in general, using component level analysis is presented.   This presentation provides an overview of work-in-progress.*
*The combination of service stress states and a requisite probability of survival for an Ingersoll-Rand microturbine rotor are used to determine Weibull distribution parameters for an arbitrary Si**3**N**4** material. Associated pairs of parameters, the Weibull modulus and the Weibull material characteristic strength, are plotted as “material performance curves.” *
*The “material performance curve” is then scaled to standard test coupons (e.g., ORNL button-head).*
*The “material performance curve” for a generic thin walled pressure vessel subjected to an internal pressure is also presented.  Based upon a surface flaw analysis, the material characteristic strengths are scaled to a bend bar specimen.*
*The number of failed specimens in a data set effects the quality of the parameter estimates.   This effect is depicted relative to the material performance curves using likelihood ratio contours in a surface flaw analysis.*

## DER Program

***Procedural Overview -***
***Material Performance Curves***
*Conduct a finite element analysis on a ceramic component.*
* *
*Establish an acceptable component failure rate. *
*Utilize NASA/CARES to back-calculate** **Weibull parameter pairs that when applied to the component exhibit the desired failure rate.   (Currently this step is executed manually for the examples presented.)*
*Graph the Weibull parameter pairs and establish the “Material Performance Curve” relative to the component. *
*Scale this curve to standard test specimens. *

## DER Program

*DER Program*

- = 535°C

- = 905°C

## DER Program

*DER Program*

## DER Program

***Material Performance Curves***
*From the finite element analysis of the microturbine rotor the NASA/CARES algorithm was used to establish material performance curves based on the following assumptions:*
*	**Failure rate must be established a priori.  Here a rate of 1 in 500,000 *
*	**was assumed (Reliability = 0.999998).*
*	**A single pair of Weibull distribution parameters was used initially for  *
*	**demonstration purposes.  This corresponds to using a set of parameters*
*	**characterized at high **	**temperature for the entire reliability solution.  This   *
*	**high temperature assumption would be conservative.  The ability to relax *
*	**this assumption is discussed later.*
*Based on the assumptions above Weibull moduli and material characteristic strength pairs were found which satisfy the assumed failure rate as computed through NASA/CARES.*

## DER Program

***Material Performance Curve -***
***Volume Flaw Analysis***

## DER Program

***Material Performance Curve - ***
***ORNL Button Head Tensile Specimen***

*Effective volume (referred to as  k**V** ****·****V ) relationship is used to transform ****0**  from the previous graph into ******for a tensile specimen in the presented here.*

*This graph can be used as a target performance curve for material vendors using tensile specimens to characterize their material*

## Material Performance Curves – Surface Flaw Analysis

***Material Performance Curves – Surface Flaw Analysis***
*An attempt was made to conduct a surface flaw analysis using the Ingersoll-Rand rotor.** **This  analysis is particularly relevant since the greatest tensile stresses were located at the rotor surface.  The surface flaws would be assumed concurrent with volume flaws.  Unfortunately the ANSYS model provided had been optimized in a way as to preclude the execution of a surface flaw analysis with CARES at this point in time.*
*Alternatively, a simple generic component was used to illustrate a surface flaw analysis, i.e., a thin walled pressure vessel.   Model geometry is as follows:*
*	**Inner Radius = 100 mm*
*	*
*	**Thickness = 5 mm*
*	**Length = 400 mm*
*	**Applied Pressure = 10 MPa*
*	**Estimated Stress (pr/t) = 200 MPa*
*	**Inner Surface FEA Stress = 205 MPa*

*DER Program*

## DER Program

***Material Performance Curve –***
***Surface Flaw Analysis***

## DER Program

***Material Performance Curve - ***
***Four Point Bend Specimen***

*Generic data sets were generated via Monte Carlo simulation.  The green curve corresponds to a data set with 30 test specimens.  The red curve corresponds to a data set with 100 test specimens.  *

*Both curves represent the 90**th** percentile confidence interval.*

## DER Program

***Material Performance Curves – ***
***Multiple Temperature Regime***

*Previous analyses assumed that ****01** = ****02*

*Previously a temperature independent regime was assumed.*
*Now assume that test data is available at two temperatures - ambient temperature and maximum component operating temperature (or higher).  *
*Further take the Weibull modulus as being independent of temperature.  *
*Now there are two material characteristic strength parameters in need of being characterized, i.e., ****02**  (ambient) and ****01* *(high temperature)*

## DER Program

***Material Performance Response Surface – ***
***Multiple Temperature Regime***

*Need to automate CARES to generate points on the response surface.  This can be done by looking at curves with fixed ratios of ****01** to ****02**.*
*The approach can be extended to multiple temperatures, but the ability to present results in a graphic fashion is soon lost. *

*Response surface will be constrained to map within this region*

## DER Program

***Summary***

*A methodology is established for generating material performance curves/surfaces for any given component geometry - stress state combination.  Curves were determined for standard test specimen geometries.*
*The effect that the number of test specimens per failure data set has on the size of the likelihood ratio confidence rings was demonstrated.*
*The approach for volume-flaw or surface-flaw strength limiting populations was demonstrated using a DER component and a generic component, respectively. *
*Further programming required to automate CARES to generate performance curves/surfaces.*
*Once response surface generation is automated look to develop optimization routines to establish the best set of Weibull parameters for a given component.*