Method for mounting aerial remote sensing equipment on aircraft

Abstract

Disclosed is a method for mounting aerial remote sensing equipment on an aircraft. A square reinforcing opening is designed in the belly part of an aircraft cabin, a mounting base and an airtight cover of the aerial remote sensing equipment matched with the reinforcing opening are additionally arranged, the mounting base is in sealed connection with the reinforcing opening, the airtight cover is arranged in the aircraft cabin, and the periphery of the bottom of the airtight cover is in sealed connection with the mounting base to form an equipment cabin; in addition, a cabin door capable of being opened towards the two sides is mounted in an aircraft body, the shape of the cabin door is consistent with the aerodynamic shape of the aircraft, the remote sensing equipment is mounted on the mounting base in the equipment cabin, and the airtight cover, the mounting base and the reinforcing opening of the belly part of the aircraft cabin are in sealed connection to form a new airtight line ofthe aircraft.

Description

technical field [0001] The invention belongs to the field of aircraft structure design, and in particular relates to an installation method of aviation remote sensing equipment. Background technique [0002] Remote sensing equipment is used for aerial remote sensing, mainly used to measure ocean wind field, etc. According to the requirements of the task load, no shelter is allowed directly below it. When installing and designing this equipment, the traditional scheme is as follows: Scheme 1: Install directly on the belly of the aircraft, design a rectification structure, and design openings on the rectification structure to ensure that there is no shelter directly below the remote sensing equipment. The advantage of this solution is that it does not change the airtight line of the aircraft, but the disadvantage is that it changes the aerodynamic shape of the aircraft, increases the flight resistance of the aircraft, and the rectification structure with openings has high aero...

AI Technical Summary

Problems solved by technology

The advantage of this solution is that it does not change the aerodynamic shape and airtight line of the aircraft. The disadvantage is that the non-airtight area of ​​the aircraft fuselage has a small space and a weak structure, making it impossible to install remote sensing equipment.

Therefore, the traditional solution is not feasible. We can only consider installing aviation remote sensing equipment in the aircraft cabin, designing a large opening in the belly of the aircraft cabin and greatly changing the airtight line of the aircraft.

Images