The invention belongs to the technical field of aircraft rear fuselage structure manufacturing, and particularly relates to an aircraft rear fuselage structure integral manufacturing method which comprises the steps that firstly, a rear fuselage integral structure is designed; 2, the rear fuselage structure is divided into multiple sections, specifically, the frame beam integral piece configuration serves as a basic segmentation unit, the rear fuselage structure is divided into multiple sections, and the number of segments of the rear fuselage structure is the same as the number of frames in a rear fuselage force bearing component; selecting a segmented interface of a rear fuselage structure, wherein the segmented interface is located at a part with relatively low stress level between two adjacent frames; thirdly, the rear fuselage structures of all the sections are manufactured through forge pieces or additional materials; and 4, sequentially connecting all the sections of the rear fuselage structure by adopting a forming connection mode of electron beam fuse forming and conformal annealing to obtain an integral structure of the rear fuselage.
本申请属于飞机后机身结构制造技术领域,具体涉及一种飞机后机身结构整体制造方法,包括:步骤一、设计后机身整体结构;步骤二、将后机身结构分为多段:以框梁整体件构型为基本分段单元,将后机身结构分为多段,后机身结构的分段数与后机身承力构件中框的个数相同;选择后机身结构分段界面,处于相邻两个框之间应力水平比较低的部位;步骤三、采用锻件或者增材制造各段后机身结构;步骤四、采用电子束熔丝成形+随形退火的成形连接方式,对各段后机身结构依次进行连接,得到后机身整体结构。
Integral manufacturing method for rear fuselage structure of airplane
一种飞机后机身结构整体制造方法
2025-03-21
Patent
Electronic Resource
Chinese
IPC: | 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 |
Aircraft rear fuselage section and manufacturing method thereof
European Patent Office | 2021
|AIRCRAFT REAR FUSELAGE SECTION AND MANUFACTURING METHOD THEREOF
European Patent Office | 2019
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