Counter-flow heat exchange systems
US-2015114611-A1 · Apr 30, 2015 · US
US10289772B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10289772-B2 |
| Application number | US-201715737008-A |
| Country | US |
| Kind code | B2 |
| Filing date | Sep 15, 2017 |
| Priority date | Nov 9, 2016 |
| Publication date | May 14, 2019 |
| Grant date | May 14, 2019 |
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A design method for creep-fatigue strength of a plate-fin heat exchanger. The method includes preliminarily designing the plate-fin heat exchanger according to its service requirements, making a primary stress assessment for the plate-fin heat exchanger, calculating the equivalent mechanical and thermophysical parameters of the plate-fin heat exchanger core to satisfy the allowable stress requirement, performing a thermal fatigue analysis for the plate-fin heat exchanger based on these parameters and then calculating the fatigue life and creep life of the plate-fin heat exchanger to accomplish the comprehensive design of the plate-fin heat exchanger in the high-temperature service. The design method provides an effective method for the high temperature design of the plate-fin heat exchanger.
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What is claimed is: 1. A design method for creep fatigue strength of a plate-fin heat exchanger, wherein the method comprises the following steps: Step 1: preliminarily designing a structure of the plate-fin heat exchanger according to its design temperature and design pressure requirements and defining operating temperature, number of operating cycles and service life of the plate-fin heat exchanger; Step 2: making a primary stress analysis for the plate-fin structure with a finite element software to identify stress concentration parts and determining allowable stress S t ; Step 3: judging whether a stress level of the stress concentration parts satisfies the following conditions: P m ≤S t ;P L +P b ≤K t *S t ; wherein, P m means primary membrane stress, P L means local membrane stress, P b means the primary bending, stress, S t means time-dependent allowable stress and K t assumes a value between 1.05 and 1.16; if these conditions are satisfied, then performing Step 4; and if the primary stress is assessed unsatisfactory, chancing the structure and plate thickness of the plate-fin heat exchanger core and going back to Step 2; Step 4: carrying out creep rupture experiment and fatigue experiment on the plate-fin structure and on an aged base material in service environment, calculating stress magnification factor K σ and strain magnification factor K s and correcting fatigue design curve and creep rupture design curve for the base material according to the calculated results of K σ and K s ; K σ = σ B B B * , K s = Δ s Δ s * , wherein, and σ B mean σ* B rupture strength of the base material and plate-fin structure in a same creep rupture time respectively, Δ t and Δ* t mean a macro-strain range of the base material and plate-fin structure in a same fatigue life respectively; Step 5: acquiring equivalent mechanical parameters and equivalent thermophysical parameters of the plate-fin structure thus to perform a finite element analysis for thermal fatigue for the plate-fin heat exchanger, finding a time history of micro-stress σ* th of the plate-fin heat exchanger core in a height direction and calculating a total strain Δε at a fillet, Δε=Δε ph +K s Δε* th , wherein, Δε ph means a strain range that is derived from a stress range Δσ ph obtained from the primary stress analysis; Δε* th means a ratio of a difference between a maximum value and a minimum value of the macro stress σ* th obtained from the thermal fatigue analysis to an elastic modulus of the plate-fin heat exchanger core in the height direction; Step 6: calculating fatigue damage D f and creep damage D c of the plate-fin heat exchanger core, D f = N t N f ( Δɛ * K s ) , wherein, N t means a number of fatigue cycles, N f (ε) means a corresponding fatigue life on the corrected fatigue design curve if the strain range is ε; D c = N i * ∫ 0 t h dt tr [ σ e * ( t ) * K σ ] , wherein, N i means a number of fatigue cycles, t h means strain retention time, σ ε *(t) means macro stress at the moment, t, tr(σ) means a corresponding creep rupture life on the corrected creep rupture design curve if the stress is a: Step 7: if D f +D c is less than 1, design requirements for the plate-fin heat exchanger are satisfied and then performing Step 8: if D f +D c is greater than or equal to 1, then performing Step 1 exchanger; Step 8: completing the design of the plate-fin heat exchanger, based on satisfying the design requirements. 2. The design method for creep fatigue strength of a plate-fin heat exchanger according to claim 1 , wherein, the allowable stress S t as described in Step 2 and Step 3 includes allowable stress S t1 of a fin area and allowable stress S t2 of a seal area. 3. The design method for creep fatigue strength of a plate-fin heat exchanger according to claim 1 , wherein, the step of acquiring the equivalent mechanical parameters and equivalent thermophysical parameters of the plate-fin heat exchanger core as described in Step 5 comprises the substeps of: a. dividing the plate-fin heat exchanger core into multiple plate-fin cells of a same shape; b. considering the plate-fin cells equivalent to uniform solid plates; e. acquiring equivalent mechanical parameters and equivalent thermophysical parameters of one of the multiple plate-fin cells, thus obtaining equivalent mechanical parameters and equivalent thermophysical parameters of the whole plate-fin heat exchanger core. 4. The design method for creep fatigue strength of a pla
Thermal analysis or thermal optimisation · CPC title
using finite element methods [FEM] or finite difference methods [FDM] · CPC title
the means being corrugated, plate-like elements · CPC title
Design verification, e.g. using simulation, simulation program with integrated circuit emphasis [SPICE], direct methods or relaxation methods · CPC title
heat exchangers {or parts thereof}, e.g. radiators, condensers {fins, headers}(making finned or ribbed tubes by fixing strip material or the like to tubes B21C37/22) · CPC title
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