A fastening system for an aircraft configured to fasten at least one tank intended to contain liquid hydrogen. The fastening system (1) comprises a longitudinal tank (4), an upper structure (7) fastened to an upper side (9) of the longitudinal tank (4), a lower structure (8) fastened to a lower side (10) of the longitudinal tank (4), and at least two fastening frames (11) comprising fastening means (12) on either side of a vertical plane of symmetry (P1) for connecting the tank (2) to the upper structure (7). The fastening system (1) further comprises at least two fastening means (13) for connecting the fastening point (151) of the tank (2) to the longitudinal box (4) and at least two fastening means (14) for connecting the fastening point (152) of the tank (2) to the substructure (8). The fastening system (1) makes it possible to securely fasten at least one hydrogen tank (2) to an aircraft (AC).
构造成紧固旨在容纳液态氢的至少一个罐的用于飞机的紧固系统。该紧固系统(1)包括纵向箱(4)、紧固到纵向箱(4)的上侧(9)的上部结构(7)、紧固到纵向箱(4)的下侧(10)的下部结构(8)以及至少两个紧固框架(11),该紧固框架(11)在竖直对称平面(P1)的任一侧上包括紧固装置(12),以用于将罐(2)连接到上部结构(7)。该紧固系统(1)还包括用于将罐(2)的紧固点(151)连接到纵向箱(4)的至少两个紧固装置(13)以及用于将罐(2)的紧固点(152)连接到下部结构(8)的至少两个紧固装置(14)。该紧固系统(1)使得可将至少一个氢罐(2)牢固地紧固在飞机(AC)上。
Fastening system for aircraft configured to fasten at least one tank intended to contain liquid hydrogen
构造成紧固旨在容纳液态氢的至少一个罐的用于飞机的紧固系统
2023-12-01
Patent
Electronic Resource
Chinese
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