A dual axis hinge configured for pivotally securing a cowl to a fixed structure of an aircraft is disclosed. In various embodiments, the dual axis hinge includes a link having a first end and a second end; a first pin configured to pivotally secure the first end of the link to the fixed structure and a second pin configured to pivotally secure the second end of the link to the cowl; and a first hinge stop configured for connection to the cowl and a second hinge stop configured for connection to the link.
Dual axis hinge radial displacement limiter
2023-08-22
Patent
Electronic Resource
English
Hub bearing unit with radial and axial displacement limiter
European Patent Office | 2021
|HUB BEARING UNIT WITH RADIAL AND AXIAL DISPLACEMENT LIMITER
European Patent Office | 2021
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