1<\/sub> = 0.541P).<\/p>\nKey aspects include distinguishing between critical defects like cracks, which are often unacceptable, and allowable ones like folds or tool marks under specific conditions. The standard cross-references other GB\/T documents, such as GB\/T 90 for acceptance inspection, GB\/T 3098.12 for mechanical properties, and GB\/T 3098.14 for testing methods. It emphasizes non-destructive and destructive testing to verify compliance, ensuring nuts meet performance requirements for torque, tensile strength, and durability.<\/p>\n
In practice, this standard aids in quality control during production, where defects are monitored at each stage\u2014from raw material selection to final assembly. For instance, raw materials must be free from inherent flaws like inclusions, which could lead to forging cracks. Heat treatment processes are controlled to avoid quench cracks caused by thermal stresses. The limits are designed to balance manufacturability with safety, allowing minor imperfections that do not affect functionality while rejecting those that do.<\/p>\n
This standard is essential for international trade, as it aligns with ISO equivalents in many aspects, facilitating global supply chains. Users should note that for specialized nuts, such as locking types or those with captive washers, additional criteria apply. Overall, GB\/T 5779.2-2000 promotes consistency in fastener quality, reducing downtime and enhancing product lifespan in demanding environments.<\/p>\n
To implement this standard effectively, inspectors use magnification tools and reference samples. Training on defect identification is crucial, as subtle differences between seams and folds can impact acceptance. The standard also considers economic factors, permitting defects within limits to avoid unnecessary scrap, while prioritizing safety. For nuts in high-stress applications, stricter interpretations may be applied via agreements between suppliers and buyers.<\/p>\n
Furthermore, environmental factors during manufacturing, such as lubrication and die conditions, influence defect formation. Regular maintenance of forging equipment helps prevent shear bursts and bursts. Post-processing like coating can mask defects, so inspections are ideally performed before such steps. This comprehensive approach ensures nuts perform reliably under operational loads, vibrations, and corrosive conditions.<\/p>\n
<\/p>\n<\/section>\n\nSurface Defects: Types, Causes, Appearance, and Limits<\/h2>\n
This section details the various surface defects in nuts as per GB\/T 5779.2-2000, including their classifications, origins, visual characteristics, and acceptable thresholds. Understanding these is vital for quality assurance in fastener production. Defects are evaluated based on their potential to initiate failures, with limits tied to nut geometry to ensure mechanical integrity.<\/p>\n
\n
1.1 Cracks<\/h3>\n
Cracks are clear fractures along metal grain boundaries or across grains, potentially containing foreign inclusions. They typically result from high stresses during forging, forming, heat treatment, or pre-existing in raw materials. Upon reheating, cracks may discolor due to oxide scale flaking.<\/p>\n
1.1.1 Quench Cracks<\/h4>\n
Quench cracks arise during heat treatment from excessive thermal stresses and strains. They appear as irregular, intersecting lines without directional pattern on the fastener surface.<\/p>\n
\n
\n\n\n <\/colgroup>\n\n\n| Cause<\/td>\n | In heat treatment, excessive thermal stress and strain can produce quench cracks. They usually appear as irregular intersecting lines without regular direction on the fastener surface.<\/td>\n<\/tr>\n |
\n| Limit<\/td>\n | Quench cracks of any depth, length, or location are not permitted.<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n Quench cracks are particularly dangerous as they can propagate under load, leading to catastrophic failure. Prevention involves controlled cooling rates and proper alloy selection. In inspection, any suspicion of such cracks warrants immediate rejection, as they compromise the nut’s tensile strength and fatigue resistance. This subtype is common in high-carbon steels where martensitic transformation induces stresses.<\/p>\n 1.1.2 Forging Cracks and Inclusion Cracks<\/h4>\nForging cracks occur during blanking or forging, located on top or bottom faces or at intersections with side planes. Inclusion cracks stem from non-metallic inclusions in raw materials.<\/p>\n \n \n\n\n <\/colgroup>\n\n\n| Cause<\/td>\n | Forging cracks may occur during blanking or forging processes and are located on the top or bottom face of the nut, or at the intersection of the top (bottom) face and the side plane. Inclusion cracks are caused by inherent non-metallic inclusions in the raw material.<\/td>\n<\/tr>\n | \n| Limit<\/td>\n | Cracks on the bearing or bottom and top faces shall comply with: a) No more than two forging cracks penetrating the bearing face, with depth not exceeding 0.05D; b) Cracks extending into the threaded hole shall not exceed the first complete thread; c) Crack depth on the first complete thread shall not exceed 0.5H1<\/sub>. D – Nominal thread diameter; H1<\/sub> – Actual thread height, H1<\/sub> = 0.541P; P – Pitch.<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n These cracks can weaken thread engagement, affecting torque retention. Material certification is key to avoiding inclusions. Limits are stringent for bearing faces to maintain load distribution.<\/p>\n <\/p>\n 1.1.3 Cracks in the Locking Element of All-Metal Prevailing Torque Type Nuts<\/h4>\nThese cracks may form during blanking, forging, or closing (flattening) processes, appearing on external or internal surfaces.<\/p>\n \n \n\n\n <\/colgroup>\n\n\n| Cause<\/td>\n | Cracks in the locking portion of all-metal prevailing torque type nuts may occur during blanking, forging, or closing (flattening) processes, appearing on external or internal surfaces.<\/td>\n<\/tr>\n | \n| Limit<\/td>\n | Cracks due to forging in the locking portion must meet mechanical and performance requirements, and: a) No more than two cracks penetrating the top circumference, with depth not exceeding 0.05D; b) Cracks extending into the threaded hole shall not exceed the first complete thread; c) Crack depth on the first complete thread shall not exceed 0.5H1<\/sub>. Cracks due to closing (flattening) are not allowed. D – Nominal thread diameter; H1<\/sub> = 0.541P; P – Pitch.<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n Locking nuts require special attention as cracks can impair self-locking function. Process optimization during closing is essential.<\/p>\n 1.1.4 Cracks in the Washer Retainer of Nuts with Captive Washers<\/h4>\nWasher retainer cracks occur during assembly when pressure is applied to edges or protrusions, causing metal splitting.<\/p>\n \n \n\n\n <\/colgroup>\n\n\n| Cause<\/td>\n | During washer assembly, pressure on edges or protrusions may produce retainer cracks.<\/td>\n<\/tr>\n | \n| Limit<\/td>\n | Retainer cracks shall be confined within the riveted edge or protrusion after flanging, and the washer shall rotate freely without detaching.<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n Ensuring washer mobility is critical; cracks must not propagate beyond defined areas to maintain assembly integrity.<\/p>\n <\/p>\n<\/div>\n \n 1.2 Shear Bursts<\/h3>\nShear bursts are openings on the metal surface, often at approximately 45\u00b0 to the nut axis, occurring during forging on outer surfaces or flange perimeters.<\/p>\n \n \n\n\n <\/colgroup>\n\n\n| Cause<\/td>\n | Shear bursts may occur during forging, appearing on the outer surface of the nut or on the flange circumference of flanged nuts. Typically, they are at about 45\u00b0 to the nut axis.<\/td>\n<\/tr>\n | \n| Limit<\/td>\n | Shear bursts on flat sides shall not extend to the bearing face of hex nuts or the top circumference of flanged nuts. Diagonal bursts shall not reduce diagonal width below minimum. At intersections of top\/bottom with side planes, width \u2264 (0.25 + 0.02s) mm. On flanged nut circumference, not extending into min dw, width \u2264 0.08dc; s – Width across flats; dc – Flange diameter.<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n Shear bursts result from material flow issues in dies. Limits protect bearing areas to ensure even load distribution. In high-vibration applications, even minor bursts can initiate fatigue. Prevention includes optimized die design and material pre-heating. Inspection often involves tactile checks alongside visual to detect subtle openings. This defect is more prevalent in larger nuts where forging forces are higher. Quantitative limits allow for production tolerances while safeguarding performance. For flanged nuts, flange integrity is paramount for enhanced stability.<\/p>\n <\/p>\n<\/div>\n <\/p>\n \n 1.3 Bursts<\/h3>\nBursts are surface openings caused by raw material defects during forging, appearing on outer surfaces or flange edges.<\/p>\n \n \n\n\n <\/colgroup>\n\n\n| Cause<\/td>\n | Bursts may occur during forging due to surface defects in raw materials, appearing on the outer surface or flange circumference.<\/td>\n<\/tr>\n | \n| Limit<\/td>\n | If cracks from raw materials connect to bursts, cracks may extend to top circumference (2-4), but bursts shall not. Diagonal bursts shall not reduce diagonal width below minimum. At intersections, width \u2264 (0.25 + 0.02s) mm. On flanged nut flange, not extending into min dw, width \u2264 0.08dc; s – Width across flats; dc – Flange diameter.<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n Bursts differ from shear bursts in origin, stemming from material inconsistencies. Raw material testing via ultrasonic methods can mitigate this. Limits are similar to shear bursts but emphasize non-extension of bursts themselves.<\/p>\n <\/p>\n<\/div>\n \n 1.4 Seams<\/h3>\nSeams are longitudinal surface defects from narrow openings in material folds, inherent in raw materials used for fasteners.<\/p>\n \n \n\n\n <\/colgroup>\n\n\n| Cause<\/td>\n | Seams are typically inherent defects in the raw material for manufacturing fasteners.<\/td>\n<\/tr>\n | \n| Limit<\/td>\n | Seam depth shall not exceed 0.05D for all thread sizes. D – Nominal thread diameter.<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n Seams can act as stress concentrators; depth limits prevent crack initiation. Material suppliers must certify seam-free stock for critical applications.<\/p>\n<\/div>\n \n 1.5 Folds<\/h3>\nFolds are metal overlaps on nut surfaces during forging, often at diameter changes or top\/bottom faces due to material displacement.<\/p>\n \n \n\n\n <\/colgroup>\n\n\n| Cause<\/td>\n | During nut forging, at or near diameter (section) changes, or on top or bottom faces, due to material displacement.<\/td>\n<\/tr>\n | \n| Limit<\/td>\n | Folds at flange circumference and bearing face intersection in flanged nuts shall not extend to bearing face. Other folds are permitted.<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n Folds are generally benign unless on load-bearing areas. Die lubrication reduces their occurrence.<\/p>\n<\/div>\n \n 1.6 Voids<\/h3>\nVoids are shallow pits or depressions from incomplete metal filling during forging or upsetting, caused by chips, burrs, or rust.<\/p>\n \n \n\n\n <\/colgroup>\n\n\n| Cause<\/td>\n | Voids are marks or imprints from chips, shearing burrs, or raw material rust layers, not eliminated in forging or upsetting.<\/td>\n<\/tr>\n | \n| Limit<\/td>\n | Void depth h \u2264 0.02D or max 0.25 mm. Total void area on bearing face \u2264 5% for D \u2264 24 mm, \u2264 10% for D > 24 mm. D – Nominal thread diameter.<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n Voids affect surface finish but are limited to avoid weakening. Clean raw materials minimize them.<\/p>\n<\/div>\n | | | | | | | | |