{"id":21250,"date":"2022-07-23T16:07:37","date_gmt":"2022-07-23T08:07:37","guid":{"rendered":"https:\/\/www.meetyoucarbide.com\/?p=21250"},"modified":"2022-07-27T11:24:16","modified_gmt":"2022-07-27T03:24:16","slug":"august-wohlers-experiment-statics-showing-you-how-the-4-elements-impact-on-fatigue-crack","status":"publish","type":"post","link":"https:\/\/www.meetyoucarbide.com\/vi\/august-wohlers-thu-nghiem-tinh-hien-thi-ban-cach-4-yeu-to-tac-dong-tren-su-met-moi-crack\/","title":{"rendered":"Th\u00ed nghi\u1ec7m c\u1ee7a August W\u00f6hler cho b\u1ea1n th\u1ea5y c\u00e1ch 4 y\u1ebfu t\u1ed1 t\u00e1c \u0111\u1ed9ng \u0111\u1ebfn v\u1ebft n\u1ee9t m\u1ec7t m\u1ecfi"},"content":{"rendered":"
Fatigue cracks are generally the result of periodic plastic deformation in local areas. Fatigue is defined as “failure under repeated load or other types of load conditions, and this load level is not sufficient to cause failure when applied only once.” This plastic deformation occurs not because of the theoretical stress on the ideal component, but because the component surface can not be actually detected.<\/a><\/a><\/a><\/a><\/a><\/a><\/p> August W\u00f6hler l\u00e0 ng\u01b0\u1eddi ti\u00ean phong trong nghi\u00ean c\u1ee9u v\u1ec1 s\u1ef1 m\u1ec7t m\u1ecfi v\u00e0 \u0111\u01b0a ra m\u1ed9t ph\u01b0\u01a1ng ph\u00e1p th\u1ef1c nghi\u1ec7m. T\u1eeb n\u0103m 1852 \u0111\u1ebfn n\u0103m 1870, w \u00f6 hler \u0111\u00e3 nghi\u00ean c\u1ee9u s\u1ef1 h\u01b0 h\u1ecfng d\u1ea7n d\u1ea7n c\u1ee7a c\u00e1c tr\u1ee5c \u0111\u01b0\u1eddng s\u1eaft. \u00d4ng \u0111\u00e3 ch\u1ebf t\u1ea1o gi\u01b0\u1eddng th\u1eed nh\u01b0 trong H\u00ecnh 1. Gi\u01b0\u1eddng th\u1eed n\u00e0y cho ph\u00e9p quay v\u00e0 u\u1ed1n hai tr\u1ee5c \u0111\u01b0\u1eddng s\u1eaft c\u00f9ng m\u1ed9t l\u00fac. W \u00f6 hler v\u1ebd bi\u1ec3u \u0111\u1ed3 m\u1ed1i quan h\u1ec7 gi\u1eefa \u1ee9ng su\u1ea5t danh ngh\u0129a v\u00e0 s\u1ed1 chu k\u1ef3 d\u1eabn \u0111\u1ebfn h\u01b0 h\u1ecfng, sau n\u00e0y \u0111\u01b0\u1ee3c g\u1ecdi l\u00e0 bi\u1ec3u \u0111\u1ed3 SN. M\u1ed7i \u0111\u01b0\u1eddng cong v\u1eabn \u0111\u01b0\u1ee3c g\u1ecdi l\u00e0 \u0111\u01b0\u1eddng aw \u00f6 hler. Ph\u01b0\u01a1ng ph\u00e1p Sn v\u1eabn l\u00e0 ph\u01b0\u01a1ng ph\u00e1p \u0111\u01b0\u1ee3c s\u1eed d\u1ee5ng r\u1ed9ng r\u00e3i nh\u1ea5t hi\u1ec7n nay. M\u1ed9t v\u00ed d\u1ee5 \u0111i\u1ec3n h\u00ecnh c\u1ee7a \u0111\u01b0\u1eddng cong n\u00e0y \u0111\u01b0\u1ee3c th\u1ec3 hi\u1ec7n trong H\u00ecnh 1.<\/p> <\/a><\/p> <\/a><\/p> Several effects can be observed through the w \u00f6 hler line. First, we note that the SN curve below the transition point (about 1000 cycles) is invalid because the nominal stress here is elastoplastic. We will show later that fatigue is caused by the release of plastic shear strain energy. Therefore, there is no linear relationship between stress and strain before fracture, and it cannot be used. Between the transition point and the fatigue limit (about 107 cycles), the Sn based analysis is valid. Above the fatigue limit, the slope of the curve decreases sharply, so this region is often referred to as the “infinite life” region. But this is not the case. For example, aluminum alloy will not have infinite life, and even steel will not have infinite life under variable amplitude load.<\/a><\/p> V\u1edbi s\u1ef1 xu\u1ea5t hi\u1ec7n c\u1ee7a c\u00f4ng ngh\u1ec7 khu\u1ebfch \u0111\u1ea1i hi\u1ec7n \u0111\u1ea1i, ng\u01b0\u1eddi ta c\u00f3 th\u1ec3 nghi\u00ean c\u1ee9u c\u00e1c v\u1ebft n\u1ee9t m\u1ecfi m\u1ed9t c\u00e1ch chi ti\u1ebft h\u01a1n. B\u00e2y gi\u1edd ch\u00fang ta bi\u1ebft r\u1eb1ng s\u1ef1 xu\u1ea5t hi\u1ec7n v\u00e0 lan truy\u1ec1n c\u1ee7a v\u1ebft n\u1ee9t m\u1ecfi c\u00f3 th\u1ec3 \u0111\u01b0\u1ee3c chia th\u00e0nh hai giai \u0111o\u1ea1n. Trong giai \u0111o\u1ea1n \u0111\u1ea7u, v\u1ebft n\u1ee9t truy\u1ec1n theo m\u1ed9t g\u00f3c kho\u1ea3ng 45 \u0111\u1ed9 so v\u1edbi t\u1ea3i tr\u1ecdng t\u00e1c d\u1ee5ng (d\u1ecdc theo \u0111\u01b0\u1eddng \u1ee9ng su\u1ea5t c\u1eaft l\u1edbn nh\u1ea5t). Sau khi v\u01b0\u1ee3t qua hai ho\u1eb7c ba ranh gi\u1edbi h\u1ea1t, h\u01b0\u1edbng c\u1ee7a n\u00f3 thay \u0111\u1ed5i v\u00e0 m\u1edf r\u1ed9ng d\u1ecdc theo h\u01b0\u1edbng kho\u1ea3ng 90 \u0111\u1ed9 so v\u1edbi t\u1ea3i tr\u1ecdng t\u00e1c d\u1ee5ng. Hai giai \u0111o\u1ea1n n\u00e0y \u0111\u01b0\u1ee3c g\u1ecdi l\u00e0 n\u1ee9t giai \u0111o\u1ea1n I v\u00e0 n\u1ee9t giai \u0111o\u1ea1n II, nh\u01b0 trong H\u00ecnh 2.<\/a><\/a><\/a><\/a><\/p> If we observe a stage I crack at high magnification, we can see that the alternating stress will lead to the formation of a continuous slip band along the maximum shear plane. These slip bands slide back and forth, much like a deck of cards, resulting in uneven surfaces. The concave surface finally forms a “budding” crack, as shown in Figure 3. In phase I, the crack will expand in this mode until it meets the grain boundary and will stop temporarily. When enough energy is applied to the adjacent crystals, then the process will continue.<\/p> <\/a><\/p> <\/a><\/a><\/a><\/a><\/a><\/a><\/p> Sau khi v\u01b0\u1ee3t qua hai ho\u1eb7c ba ranh gi\u1edbi h\u1ea1t, h\u01b0\u1edbng lan truy\u1ec1n v\u1ebft n\u1ee9t l\u00fac n\u00e0y chuy\u1ec3n sang ch\u1ebf \u0111\u1ed9 pha II. \u1ede giai \u0111o\u1ea1n n\u00e0y, c\u00e1c t\u00ednh ch\u1ea5t v\u1eadt l\u00fd c\u1ee7a s\u1ef1 lan truy\u1ec1n v\u1ebft n\u1ee9t \u0111\u00e3 thay \u0111\u1ed5i. B\u1ea3n th\u00e2n v\u1ebft n\u1ee9t t\u1ea1o th\u00e0nh v\u1eadt c\u1ea3n v\u0129 m\u00f4 \u0111\u1ed1i v\u1edbi d\u00f2ng \u1ee9ng su\u1ea5t, l\u00e0m cho \u1ee9ng su\u1ea5t d\u1ebbo t\u1eadp trung cao \u1edf \u0111\u1ea7u v\u1ebft n\u1ee9t. Nh\u01b0 trong H\u00ecnh 4. C\u1ea7n l\u01b0u \u00fd r\u1eb1ng kh\u00f4ng ph\u1ea3i t\u1ea5t c\u1ea3 c\u00e1c v\u1ebft n\u1ee9t \u1edf giai \u0111o\u1ea1n I s\u1ebd ph\u00e1t tri\u1ec3n sang giai \u0111o\u1ea1n II.<\/a><\/p> In order to understand the propagation mechanism of stage II, we need to consider the situation of crack tip cross-section during the stress cycle. As shown in Figure 5. The fatigue cycle begins when the nominal stress is at point “a”. As the stress intensity increases and passes through point “B”, we notice that the crack tip opens, resulting in local plastic shear deformation, and the crack extends to point “C” in the original metal. When the tensile stress decreases through the “d” point, we observe that the crack tip closes, but the permanent plastic deformation leaves a unique serration, the so-called “cut line”. When the whole cycle ends at the “e” point, we observe that the crack has now increased the “Da” length and formed additional section lines. It is now understood that the range of crack growth is proportional to the range of applied elastic-plastic crack tip strain. A larger cycle range can form a larger Da.<\/a><\/p> <\/p> \u1ea2nh h\u01b0\u1edfng c\u1ee7a c\u00e1c th\u00f4ng s\u1ed1 sau \u0111\u1ebfn t\u1ed1c \u0111\u1ed9 ph\u00e1t tri\u1ec3n v\u1ebft n\u1ee9t m\u1ecfi \u0111\u01b0\u1ee3c nghi\u00ean c\u1ee9u v\u00e0 gi\u1ea3i th\u00edch v\u1ec1 m\u1eb7t kh\u00e1i ni\u1ec7m:<\/p> From the diagram, we can see that a certain “amount” of shear stress is released during the periodic change of the strength of the nominal stress. And the larger the range of stress changes, the greater the energy released. Through the SN curve shown in Figure 1, we can see that the fatigue life decreases exponentially with the increase of the stress cycle range.<\/a><\/p>C\u00e1c y\u1ebfu t\u1ed1 \u1ea3nh h\u01b0\u1edfng \u0111\u1ebfn t\u1ed1c \u0111\u1ed9 ph\u00e1t tri\u1ec3n v\u1ebft n\u1ee9t m\u1ecfi<\/h2>
1 Gi\u1ea3m c\u0103ng th\u1eb3ng<\/h3>