The invention relates to the technical field of aircraft structure design, in particular to an aircraft leading edge tower type bird impact resisting structure which comprises a leading edge skin assembly, a first protection assembly, a second protection assembly, a third protection assembly and a rear beam assembly. The front edge skin assembly and the rear beam assembly are located at the front ends and the rear ends of the first protection assembly, the second protection assembly and the third protection assembly which are connected in sequence correspondingly and wrap the first protection assembly, the second protection assembly and the third protection assembly. The rear end of the first protection assembly is fixedly connected with the front end of the second protection assembly and used for resisting high-speed impact birds, and the rear end of the second protection assembly is fixedly connected with the front end of the third protection assembly and used for resisting medium-speed impact birds. And the rear end of the third protection assembly is fixedly connected with the rear beam assembly and is used for resisting a bird body which is impacted at a low speed. The airplane leading edge tower type bird impact resisting structure aims at solving the problem that an existing airplane leading edge bird impact resisting structure is low in structural efficiency.
本发明涉及飞机结构设计技术领域,具体涉及一种飞机前缘塔式抗鸟撞结构,其包括前缘蒙皮组件、第一防护组件、第二防护组件、第三防护组件和后梁组件,前缘蒙皮组件、后梁组件分别位于依次连接的第一防护组件、第二防护组件及第三防护组件的前后端且裹设于第一防护组件、第二防护组件及第三防护组件;第一防护组件的后端与第二防护组件的前端固定连接且用于抗击高速冲击的鸟体,第二防护组件的后端与第三防护组件的前端固定连接且用于抗击中速冲击的鸟体,第三防护组件的后端与后梁组件固定连接且用于抗击低速冲击的鸟体。该飞机前缘塔式抗鸟撞结构的目的是解决现有的飞机前缘抗鸟撞结构的结构效率较低的问题。
Tower-type bird-impact-resistant structure at leading edge of airplane
一种飞机前缘塔式抗鸟撞结构
2023-08-15
Patent
Elektronische Ressource
Chinesisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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