IP Library Granted Patent US 8,108,156
Granted Patent B2
US 8,108,156 · App. 12/266,059 · Granted Jan 31, 2012

Methods, program products, and systems for estimating the stress-strain relationship of a toughened structural adhesive polymer

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Quick Facts
Patent No.
US 8,108,156
App. No.
12/266,059
Granted
Jan 31, 2012
Kind
B2
Abstract

Methods, program products, and computer systems for estimating a stress of a toughened structural adhesive polymer are provided. One method comprises selecting a strain, a strain rate, a temperature, or a combination thereof at which the stress is to be estimated. A value of a strain-hardening stress of the toughened structural adhesive polymer is determined, wherein the value of the strain-hardening stress is dependent on the temperature and the strain. A value of a non-strain-hardening stress of the toughened structural adhesive polymer is determined, wherein the value of the non-strain-hardening stress is dependent on the strain, the strain rate, and the temperature. The value of the strain-hardening stress is added to the value of the non-strain-hardening stress to obtain an estimated total stress.

Claims (308)

1. A method for estimating a total stress of a toughened structural adhesive polymer, the method comprising the steps of:

receiving via an input device a strain, a strain rate, a temperature, or a combination thereof at which the total stress is to be estimated;

accessing from a memory device computer instructions and causing the computer to perform:

determining a value of a strain-hardening stress of the toughened structural adhesive polymer, wherein strain-hardening stress of the toughened structural adhesive polymer is assigned a value of zero if the temperature is no greater than about 23° C. and wherein the strain-hardening stress is determined using an equation:

σ

H

=

11

×

T

(

°

C

.

)

-

23

°

C

.

82

°

C

.

-

23

°

C

.

×

ɛ

,

if the temperature is greater than about 23° C., wherein σ H is in units of megapascals (MPa), wherein ε is the strain, T is the temperature, and wherein constants 11, 23° C., and 82° C. deviate by about zero to about ±5° C.;

determining a value of a non-strain-hardening stress of the toughened structural adhesive polymer, wherein the value of the non-strain-hardening stress is dependent on the strain, the strain rate, and the temperature; and

adding the value of the strain-hardening stress to the value of the non-strain-hardening stress to obtain an estimated total stress.

2. The method of claim 1 , wherein the step of determining a value of the non-strain-hardening stress comprises the steps of:

determining a value for a baseline stress (σ 0 ), a strain-rate-dependent stress (φ), and a temperature-dependent factor (η); and

multiplying the values of the baseline stress, the strain-rate-dependent stress and the temperature-dependent factor together.

3. The method of claim 2 , wherein the step of determining a value for a baseline stress (σ 0 ), a strain-rate-dependent stress (φ), and a temperature-dependent factor (η) comprises determining the value for the baseline stress using an equation:

σ 0 (ε)=59.5×(1 −e −45·ε ),

wherein σ 0 (ε) is in units of megapascals and wherein constants 59.5, 1, and −45 deviate by from about zero to about ±5%.

4. The method of claim 2 , wherein the step of determining a value for a baseline stress (σ 0 ), a strain-rate-dependent stress (φ), and a temperature-dependent factor (η) comprises determining the value for the strain-rate-dependent stress using an equation:

φ

(

ɛ

,

T

)

=

1

+

18.2

100

-

1.07

·

T

×

lg

(

ɛ

/

ɛ

0

)

,

wherein φ({acute over (ε)}, T) is unitless, wherein {acute over (ε)} 0 is a reference strain rate, and wherein constants 1, 18.2, 100, and 1.07 deviate by from about zero to about ±5%.

5. The method of claim 2 , wherein the step of determining a value for a baseline stress (σ 0 ), a strain-rate-dependent stress (φ), and a temperature-dependent factor (η) comprises determining the value for the temperature-dependent factor using an equation:

η

(

T

)

=

1

-

(

T

+

40

129

)

0.75

,

wherein η(T) is unitless and wherein constants 1, 40, 129, and 0.75 can deviate by from about zero to about ±5%.

6. The method of claim 1 , further comprising the step of selecting a second strain, a second strain rate, a second temperature, or a combination thereof and repeating the steps of determining and adding to obtain a second estimated total stress of the toughened structural adhesive polymer.

7. A non-transitory computer readable medium containing a computer program product comprising a computer program for estimating a total stress of a structural adhesive polymer at a selected strain, a selected strain rate, and a selected temperature, the:

computer program configured to at least facilitate:

determining a value of a strain-hardening stress of the toughened structural adhesive polymer, wherein the strain-hardening stress of the toughened structural adhesive polymer is assigned a value of zero if the temperature is no greater than about 23° C. and wherein the strain-hardening stress is determined using an equation:

σ

H

=

11

×

T

(

°

C

.

)

-

23

°

C

.

82

°

C

.

-

23

°

C

.

×

ɛ

,

if the temperature is greater than about 23° C., wherein σ H is in units of megapascals (MPa),

wherein ε is the strain, and wherein constants 11, 23° C., and 82° C. deviate by about zero to about ±5° C.;

determining a value of a non-strain-hardening stress of the toughened structural adhesive polymer, wherein the value of the non-strain-hardening stress is dependent on the selected strain, the selected strain rate, and the selected temperature; and

adding the value of the strain-hardening stress to the value of the non-strain-hardening stress to obtain an estimated total stress.

8. The non-transitory computer readable medium of claim 7 , wherein the computer program is configured to at least facilitate determining a value of the non-strain-hardening stress by:

determining a value for a baseline stress (σ 0 ), a strain-rate-dependent stress (φ), and a temperature-dependent factor (η); and

multiplying the values of the baseline stress, the strain-rate-dependent stress, and the temperature-dependent factor together.

9. The non-transitory computer readable medium of claim 8 , wherein the computer program is configured to at least facilitate determining the value for the baseline stress using an equation:

σ 0 (ε)=59.5×(1 e −45·ε ),

wherein σ 0 (ε) is in units of megapascals and wherein constants 59.5, 1, and −45 deviate by from about zero to about ±5%.

10. The non-transitory computer readable medium of claim 8 , wherein the computer program is configured to at least facilitate determining the value for the strain-rate-dependent stress using an equation:

φ

(

ɛ

,

T

)

=

1

+

18.2

100

-

1.07

·

T

×

lg

(

ɛ

/

ɛ

0

)

,

wherein ε({acute over (ε)}, T) is unitless, wherein {acute over (ε)} 0 is a reference strain rate, and wherein constants 1, 18.2, 100, and 1.07 deviate by from about zero to about ±5%.

11. The non-transitory computer readable medium of claim 8 , wherein the computer program is configured to at least facilitate determining the value for the temperature-dependent factor using an equation:

η

(

T

)

=

1

-

(

T

+

40

129

)

0.75

,

wherein η(T) is unitless and wherein constants 1, 40, 129, and 0.75 deviate by from about zero to about ±5%.

12. A computer system for estimating a total stress of a toughened structural adhesive polymer at a selected strain, a selected strain rate, and a selected temperature, the computer system comprising:

a processor configured to at least facilitate:

receiving input signals derived from the selected strain, the selected strain rate, and the selected temperature;

determining a value of a strain-hardening stress of the toughened structural adhesive polymer, wherein the value of the strain-hardening stress is dependent on the selected temperature and the selected strain;

determining a value of a strain-hardening stress of the toughened structural adhesive polymer, wherein the strain-hardening stress of the toughened structural adhesive polymer is assigned a value of zero if the selected temperature is no greater than about 23° C. and wherein the strain-hardening stress is determined using an equation:

σ

H

=

11

×

T

(

°

C

.

)

-

23

°

C

.

82

°

C

.

-

23

°

C

.

×

ɛ

,

if the selected temperature is greater than about 23° C., wherein σ H is in units of megapascals (MPa), wherein ε is the selected strain, and wherein constants 11, 23° C., and 82° C. deviate by about zero to about ±5° C.;

determining a value of a non-strain-hardening stress of the toughened structural adhesive polymer, wherein the value of the non-strain-hardening stress is dependent on the selected strain, the selected strain rate, and the selected temperature; and

adding the value of the strain-hardening stress to the value of the non-strain-hardening stress to obtain an estimated total stress; and

an output device coupled to the processor and configured to at least facilitate displaying the estimated total stress.

13. The system of claim 12 , wherein the processor is configured to at least facilitate determining a value of the non-strain-hardening stress by:

determining a value for a baseline stress (σ 0 ), a strain-rate-dependent stress (φ), and a temperature-dependent factor (η); and

multiplying the values of the baseline stress, the strain-rate-dependent stress and the temperature-dependent factor together.

14. The system of claim 13 , wherein the processor is configured to at least facilitate determining the value for the baseline stress using an equation:

σ 0 (ε)=59.5×(1 e −45· ),

wherein σ 0 (ε) is in units of megapascals and wherein constants 59.5, 1, and −45 deviate by from about zero to about ±5%.

15. The system of claim 13 , wherein the processor is configured to at least facilitate determining the value for the strain-rate-dependent stress using an equation:

φ

(

ɛ

,

T

)

=

1

+

18.2

100

-

1.07

·

T

×

lg

(

ɛ

/

ɛ

0

)

,

wherein φ({acute over (ε)}, T) is unitless, wherein {acute over (ε)} 0 is a reference strain rate, and wherein constants 1, 18.2, 100, and 1.07 deviate by from about zero to about ±5%.

16. The system of claim 13 , wherein the processor is configured to at least facilitate determining the value for the temperature-dependent factor using an equation:

η

(

T

)

=

1

-

(

T

+

40

129

)

0.75

,

wherein η(T) is unitless and wherein constants 1, 40, 129, and 0.75 can deviate by from about zero to about ±5%.

17. The system of claim 12 , further comprising an input device coupled to the processor and configured to at least facilitate obtaining the selected strain, the selected strain rate, the selected temperature, or a combination thereof and transmit data indicative of the selected strain, the selected strain rate, the selected temperature, or a combination thereof to the processor.

18. The method of claim 1 , further comprising sending to an output device the estimated total stress and causing the output device to display the estimated total stress on a display device.

Assignments (12)
RELEASE OF SECURITY INTEREST Recorded Nov 7, 2014
From: WILMINGTON TRUST COMPANY
To: GM GLOBAL TECHNOLOGY OPERATIONS LLC
Reel/Frame 034384/0758 →
CHANGE OF NAME Recorded Feb 10, 2011
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: GM GLOBAL TECHNOLOGY OPERATIONS LLC
Reel/Frame 025781/0245 →
SECURITY AGREEMENT Recorded Nov 8, 2010
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: WILMINGTON TRUST COMPANY
Reel/Frame 025324/0515 →
RELEASE OF SECURITY INTEREST Recorded Nov 5, 2010
From: UAW RETIREE MEDICAL BENEFITS TRUST
To: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
Reel/Frame 025315/0046 →
RELEASE OF SECURITY INTEREST Recorded Nov 4, 2010
From: UNITED STATES DEPARTMENT OF THE TREASURY
To: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
Reel/Frame 025245/0909 →
SECURITY AGREEMENT Recorded Aug 28, 2009
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: UAW RETIREE MEDICAL BENEFITS TRUST
Reel/Frame 023162/0237 →
SECURITY AGREEMENT Recorded Aug 27, 2009
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: UNITED STATES DEPARTMENT OF THE TREASURY
Reel/Frame 023156/0313 →
RELEASE OF SECURITY INTEREST Recorded Aug 21, 2009
From: UNITED STATES DEPARTMENT OF THE TREASURY
To: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
Reel/Frame 023126/0914 →
RELEASE OF SECURITY INTEREST Recorded Aug 21, 2009
From: CITICORP USA, INC. AS AGENT FOR BANK PRIORITY SECURED PARTIES; CITICORP USA, INC. AS AGENT FOR HEDGE PRIORITY SECURED PARTIES
To: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
Reel/Frame 023155/0769 →
SECURITY AGREEMENT Recorded Apr 16, 2009
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: CITICORP USA, INC. AS AGENT FOR BANK PRIORITY SECURED PARTIES; CITICORP USA, INC. AS AGENT FOR HEDGE PRIORITY SECURED PARTIES
Reel/Frame 022554/0538 →
SECURITY AGREEMENT Recorded Feb 3, 2009
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: UNITED STATES DEPARTMENT OF THE TREASURY
Reel/Frame 022201/0363 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 6, 2008
From: WANG, KANGPING; WANG, PEI-CHUNG; FICKES, JOHN D.; DENG, YIH-CHARNG
To: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
Reel/Frame 021796/0936 →