The invention provides an aircraft cabin exhaust flow guide structure and method, and belongs to the technical field of aircraft inner runners, the aircraft cabin exhaust flow guide structure is characterized in that a flow baffle is arranged at the position, behind an air inlet opening, in an aircraft cabin, a sealing assembly is arranged between the flow baffle and the aircraft cabin, and an air inlet hole is formed in a flow guide plate. An air guide pipeline with one end communicated with the air inlet is arranged in the aircraft cabin, and the other end of the air guide pipeline is communicated with the outside of the aircraft cabin. And air entering from the air inlet opening is transmitted to the outside of the aircraft cabin through the air inlet hole and the air guide pipeline in sequence. The structure is isolated from the interior of the cabin, when the aircraft flies, high-temperature airflow entering from the front structure can be guided out, and the temperature in the cabin is prevented from rising.
本发明提供一种飞行器舱体排气导流结构及方法,属于飞行器内流道技术领域,包括在飞行器舱体内部位于进气开口后方的位置设置挡流板,在挡流板与飞行器舱体之间设有密封组件,并在导流板上开设进气孔。在飞行器舱体内部设置一端与进气孔连通的导气管路,并将导气管路的另一端与飞行器舱体外部连通。从进气开口进入的空气依次通过进气孔和导气管路传输至飞行器舱体的外部。本发明的结构与舱体内部隔绝,在飞行器飞行时,能够将前部结构进入的高温气流导出,避免舱内温度升高。
Aircraft cabin exhaust flow guide structure and method
一种飞行器舱体排气导流结构及方法
2022-07-12
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
European Patent Office | 2018
|Guide rail mounting device and aircraft or aircraft cabin
European Patent Office | 2023
|Electric automobile front cabin exhaust structure, front cabin and automobile
European Patent Office | 2024
|AIRCRAFT AIR CONDITIONING SYSTEM WITH A CABIN EXHAUST AIR TURBINE
European Patent Office | 2020
|AIRCRAFT AIR CONDITIONING SYSTEM WITH A CABIN EXHAUST AIR TURBINE
European Patent Office | 2018
|