The invention provides a method for determining fatigue test loads of typical lap joint test pieces. The method comprises the following steps: selecting a plurality of test pieces; wherein the test piece comprises a test piece A and a test piece B; obtaining a fatigue limit load Pjxs of each test piece in the test pieces B according to a fatigue limit cut-and-try method; determining an average fatigue limit load Pjxa based on the fatigue limit load Pjxs of each test piece; wherein the rivet connection number of the test piece B is recorded as n1; on the basis of the average fatigue limit load Pjxa, the number of connected rivets and the maximum load proportionality coefficient of the rivets, the maximum extrusion load borne by the rivets and the bypass load at the sections of the rivets are obtained; a stress severity coefficient method is adopted, the maximum stress of the rivet hole edge is calculated, and the maximum stress of the rivet hole edge represents the fatigue limit of the structure; obtaining the yield limit of the structure, and obtaining the fatigue loading load of the test piece A based on the fatigue limit of the structure and the yield limit of the structure.
本申请提供了一种确定典型搭接连接试验件疲劳试验载荷的方法,所述方法包括:选择多个试验件;其中,所述试验件包括试验件A和试验件B;根据疲劳极限试凑法得到所述试验件B中每件试验件的疲劳极限载荷Pjxs;基于所述每件试验件的疲劳极限载荷Pjxs,确定平均疲劳极限载荷Pjxa;其中,所述试验件B的铆钉连接个数记为n1;基于所述平均疲劳极限载荷Pjxa、铆钉连接个数和铆钉最大载荷比例系数,得到铆钉所受最大挤压载荷和钉截面处旁路载荷;采用应力严重系数法,计算铆钉孔边最大应力,其中,所述铆钉孔边最大应力表征结构的疲劳极限;获取结构的屈服极限,基于所述结构的疲劳极限和所述结构的屈服极限,得到所述试验件A的疲劳加载载荷。
Method for determining fatigue test load of typical lap joint test piece
一种确定典型搭接连接试验件疲劳试验载荷的方法
2024-12-06
Patent
Electronic Resource
Chinese
IPC: | G01N Untersuchen oder Analysieren von Stoffen durch Bestimmen ihrer chemischen oder physikalischen Eigenschaften , INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / G01M TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES , Prüfen der statischen oder dynamischen Massenverteilung rotierender Teile von Maschinen oder Konstruktionen |
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