Cabin Door Adjustment Analysis for 28 Aircraft Ground Power Units_News Center Co., Ltd._Shandong Hangtai Aeronautical Equipment Co., Ltd. 
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Home > News Center Co., Ltd. > Cabin Door Adjustment Analysis for 28 Aircraft Ground Power Units
News Center Co., Ltd.
Cabin Door Adjustment Analysis for 28 Aircraft Ground Power Units
Publish Time:2024-12-17        View Count:158         Return to List

Cabin Door Adjustment Analysis28Ground Power Unit for Aircraft

1Theoretical Analysis

The aircraft enters pressurization mode as it begins its takeoff roll, and this continues until the cabin pressure returns to the landing field's level after touchdown.

   Jinfly Analyzes that during the pressurization process, the pressure difference between the inside and outside of the aircraft generates an outward pressure, which presses the cabin door against the door frame.

Pressure differential fluctuations can cause pressure variations, simulating a non-linear or irregular force applied to the cabin door outwardly. The pressure changes affect the door's mechanism and also influence the cabin door warning system.400HZPower Source Aircraft Power Vehicle

Hatch Mechanism Analysis

The main mechanisms of the door can be divided into the following two types:

1Gripper Mechanism: Handle Cam Disc-Hinge shaft torsion tube rotating mechanism.

2Locking Mechanism: Handle Cam Disc-Up-and-down flipping leaflet motion mechanism.


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