AIR OR SPACE VEHICLE CAP AND AIR OR SPACE VEHICLE

DE602022037473T2Active Publication Date: 2026-05-27AIRBUS OPERATIONS GMBH
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Patent Information

Authority / Receiving Office
DE · DE
Patent Type
Patents
Current Assignee / Owner
AIRBUS OPERATIONS GMBH
Filing Date
2022-12-19
Publication Date
2026-05-27

AI Technical Summary

Technical Problem

Aircraft and spacecraft hatches face challenges with high tensile forces and load differences leading to deformations and misalignments of locking elements, which impair the correct orientation and closure of the hatch, especially in large doors like cargo holds, due to manufacturing tolerances and varying loads during flight.

Method used

The invention introduces a hatch locking device with a drivable spindle drive, a pull-in device, and a drive unit that assists in closing the hatch, capable of transmitting forces and torques in multiple directions, and includes eccentric bush assemblies to compensate for misalignments and manufacturing tolerances, ensuring complete closure and secure latching.

Benefits of technology

The solution ensures complete and secure closure of the hatch despite misalignments and varying loads, compensating for manufacturing tolerances and load differences, and maintains proper alignment of locking bolts, enhancing the locking mechanism's reliability and functionality.

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