The invention relates to the technical field of components of aviation and aerospace crafts, and particularly relates to an all composite material lightweight fuel tank shell for an aircraft. The whole structure is divided into three sections, namely a front conical section (100), a middle column section (200) and a rear conical section (300). The concrete structure comprises a conical section shell (1), a column section shell (2), a conical section shell (3), an L-shaped ring frame a (4), an L-shaped butt joint ring frame (5), an L-shaped ring frame b (6), a small omega-shaped ring frame (7),a large omega-shaped ring frame (8), an L-shaped ring frame c (9), an L-shaped butt joint b (10), an omega-shaped ring frame (11), a U-shaped ring frame (12), a main lifting point joint (13), a stopblock (14), a rear lifting point joint (15), a concentrated force decomposition structure (16) and an I-shaped beam decomposition joint (17). A cabin section is easy to integrally design and manufacture, high in overall rigidity, light in weight, simple in structure, capable of easily guaranteeing the sealing characteristic of the box body, high in adaptability to severe environments such as saltmist and the like.
本发明涉及航空、航天飞行器的部件技术领域,特别是涉及一种用于飞行器的全复合材料轻质燃料箱壳体;整体结构分为三大段,包括前部锥段(100)、中部柱段(200)、后部锥段(300),具体结构包括锥段壳体(1)、柱段壳体(2)、锥段壳体(3)、L形环框a(4)、L对接环框(5)、L形环框b(6)、小Ω形环框(7)、大Ω形环框(8)、L形环框c(9)、L对接环框b(10)、Ω形环框(11)、U形环框(12)、主吊点接头(13)、止动块(14)、后吊点接头(15)、集中力分解结构(16)、工字梁分解接头(17);本发明舱段易于一体化设计制造、整体刚度高、重量轻,结构简单、容易保证箱体密封特性、盐雾等恶劣环境适应性强等诸多优点。
All composite material lightweight fuel tank shell for aircraft
一种用于飞行器的全复合材料轻质燃料箱壳体
12.03.2021
Patent
Elektronische Ressource
Chinesisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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