IP Library › Granted Patent US 11,650,143
Granted Patent B2
US 11,650,143 · App. 17/733,853 · Granted May 16, 2023

Method for compiling equivalent acceleration spectrum of creep under variable temperatures and loads

Inventors: Yingdong Song (Nanjing, CN); Xu Zhao (Nanjing, CN); Zhigang Sun (Nanjing, CN); Xuming Niu (Nanjing, CN); Yaning Chang (Nanjing, CN); Qiuhong Peng (Nanjing, CN)
Assignee: NANJING UNIVERSITY OF AERONAUTICS AND ASTRONAUTICS
G01N3/18G01N3/36G01N2203/0017G01N2203/0048G01N2203/0071G01N2203/0073G01N2203/0226G01N2203/0676
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Quick Facts
Patent No.
US 11,650,143
App. No.
17/733,853
Granted
May 16, 2023
Kind
B2
Abstract

Disclosed is a method for compiling an equivalent acceleration spectrum of creep under variable temperatures and loads. The method includes following steps: respectively carrying out a material high-temperature tensile test, material high-temperature creep tests and creep tests under two-stage variable temperatures and loads, and calculating values of a parameter p in a creep damage accumulation model under two-stage variable temperatures and loads; based on a nonlinear damage accumulation model under multi-stage variable temperatures and loads, calculating a damage D caused by a multi-stage variable temperatures and loads creep load spectrum by utilizing values of parameter p; based on the principle of consistency of damage D, transforming the multi-stage variable temperatures and loads creep load spectrum into an equivalent acceleration spectrum of a first-order maximum creep load, and finally compiling the equivalent acceleration spectrum of creep under variable temperatures and loads.

Claims (265)

1. A method for compiling an equivalent acceleration spectrum of creep under variable temperatures and loads, comprising:

S 1 : obtaining a corresponding tensile strength σ bi at different temperatures T i through a high-temperature tensile test of materials, wherein i=1, 2, 3 . . . , n;

S 2 : obtaining a corresponding creep fracture time t fi under different stress-temperature (σ i ,T i ) combinations through high-temperature creep tests of materials;

S 3 : obtaining a creep duration t i corresponding to each stage of load through creep tests under two-stage variable temperatures and loads;

S 4 : calculating values of parameter p in the creep damage accumulation model by combining a tensile strength σ b1 and a tensile strength σ b2 obtained in S 1 , a creep fracture time t f1 and a creep fracture time t f2 obtained in S 2 and a creep duration t 1 and a creep duration t 2 obtained in S 3 based on a creep damage accumulation model under two-stage variable temperatures and loads;

wherein the creep damage accumulation model under two-stage variable temperatures and loads is

(

t

1

t

f

1

)

φ

1

,

2

+

t

2

t

f

2

=

1

,

wherein,

φ

1

,

2

=

ln

⁡

(

-

ln

⁡

(

σ

2

/

σ

b

⁢

2

)

-

p

)

/

ln

⁡

(

-

ln

⁡

(

σ

1

/

σ

b

⁢

1

)

-

p

)

;

 and

S 5 : calculating a damage D caused by a creep load spectrum under multi-stage variable temperatures and loads by utilizing the values of parameter p obtained in S 4 according to a nonlinear creep damage accumulation model load under multi-stage variable temperatures and loads; converting the creep load spectrum under multi-stage variable temperatures and loads into the equivalent acceleration spectrum of a single-stage maximum creep load based on the principle of consistency of the damage D, and finally compiling the equivalent acceleration spectrum of creep under variable temperatures and loads;

wherein the nonlinear creep damage accumulation model load under multi-stage variable temperatures and loads is

D

=

(

(

(

(

t

1

t

f

⁢

1

)

φ

1

,

2

+

t

2

t

f

⁢

2

)

φ

2

,

3

+

t

3

t

f

⁢

3

)

φ

3

,

4

+

…

+

t

n

-

1

t

fn

-

1

)

φ

n

-

1

,

n

+

t

n

t

fn

,

wherein,

φ

n

-

1

,

n

=

ln

⁡

(

-

ln

⁡

(

σ

n

/

σ

b

⁢

n

)

-

p

)

/

ln

⁡

(

-

ln

⁡

(

σ

n

-

1

/

σ

bn

-

1

)

-

p

)

;

assuming a state with maximum creep load in the creep load spectrum under multi-stage variable temperatures and loads to be (σ 2 ,T 2 ), then according to the principle of the damage D equivalence represented by

D

=

(

(

(

(

t

1

t

f

⁢

1

)

φ

1

,

2

+

t

2

t

f

⁢

2

)

φ

2

,

3

+

t

3

t

f

⁢

3

)

φ

3

,

4

+

…

+

t

n

-

1

t

fn

-

1

)

φ

n

-

1

,

n

+

t

n

t

fn

=

t

equal

t

f

⁢

2

,

 other states with smaller creep loads are equivalently accelerated to the state (σ 2 ,T 2 ) with maximum creep load, and a duration of the creep load spectrum of original multi-stage variable temperatures and loads could be accelerated to t equal of the equivalent acceleration spectrum of creep from t 1 +t 2 + . . . +t n , so as to compile the equivalent acceleration spectrum of creep under variable temperatures and loads.

2. The method according to claim 1 , wherein in S 1 , the high-temperature tensile test of materials is carried out on an electro-hydraulic servo fatigue tester.

3. The method according to claim 1 , wherein in S 2 , the high-temperature creep tests of materials are carried out on a creep tester, and a series of high-temperature creep tests of materials under different stress-temperature (σ i ,T i ) combinations are carried out.

4. The method according to claim 1 , wherein in S 3 , according to results of the high-temperature creep tests, the creep tests under two-stage variable temperatures and loads are carried out on a creep tester until fracture occurs, and the creep duration t i corresponding to each stage of load is recorded.

5. The method according to claim 4 , wherein in S 3 , the creep tests under two-stage variable temperatures and loads are carried out manually or by a computer to change a stress and a temperature.

6. The method according to claim 1 , wherein in S 4 , p is an average value of results obtained from multiple tests.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 29, 2022
From: SONG, YINGDONG; ZHAO, XU; SUN, ZHIGANG; NIU, XUMING; CHANG, YANING; PENG, QIUHONG
To: NANJING UNIVERSITY OF AERONAUTICS AND ASTRONAUTICS
Reel/Frame 059717/0519 →
Priority Claims (1)
CN 202011556547.1 · Dec 24, 2020 · national
Continuity (2)
Continuation PCTCN2021129576 · Nov 9, 2021
Related Publication 20220260468A1 · Aug 18, 2022