Locking and moving system for an aircraft electric door

US11066864B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11066864-B2
Application numberUS-201916266432-A
CountryUS
Kind codeB2
Filing dateFeb 4, 2019
Priority dateNov 16, 2012
Publication dateJul 20, 2021
Grant dateJul 20, 2021

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

An aircraft electric door for a pressurized airframe having a locking system for locking a safety catch, a system for moving a door arm, and an electric motor activated by a door computer to actuate both systems. The system for moving the door arm includes a guideway linked to the door arm. The guideway is in a mobile cylindrical support rotated by the electric motor. A fixed guide is fitted in a cylindrical sleeve around the cylindrical support. The fixed guide includes a vertical camway and a horizontal camway. The door arm pivots around a vertical hinge and is linked with door lifting devices. The door lifting devices are mounted between a shaft of the safety catch and the door arm.

First claim

Opening claim text (preview).

The invention claimed is: 1. An aircraft electric door for a pressurized airframe comprising: a locking system for locking a safety catch; a moving system for opening and closing the door; an electric motor controlled by a door computer and adapted to actuate the locking system and the moving system; wherein the moving system includes: a vertical threaded rod connected to the door; a helical guideway linked to the door and including a ball nut connected to the vertical threaded rod; wherein the door is pivotally supported by a hinge, the hinge including an upper hinge plate with an upper fitting, a middle hinge plate and lower hinge plate; wherein the vertical threaded rod is rotatable by the electric motor; wherein the moving system is supported by the upper hinge plate, the middle hinge plate, and the lower hinge plate; wherein a guideway sleeve is located on the middle hinge plate, the guideway sleeve including a vertical camway engageable with a first guiding roller mounted on the vertical threaded rod, wherein the first guiding roller engages the vertical camway to prevent the door from rotating and enabling the electric motor to actuate the locking system and the upper hinge plate includes a horizontal camway engageable with a second guiding roller ( 635 , 636 ) located on the vertical threaded rod, wherein the second guiding roller engages the horizontal camway to enable the electric motor to move the door between open and closed positions.

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What does patent US11066864B2 cover?
An aircraft electric door for a pressurized airframe having a locking system for locking a safety catch, a system for moving a door arm, and an electric motor activated by a door computer to actuate both systems. The system for moving the door arm includes a guideway linked to the door arm. The guideway is in a mobile cylindrical support rotated by the electric motor. A fixed guide is fitted in…
Who is the assignee on this patent?
Latecoere, Latecoeye
What technology area does this patent fall under?
Primary CPC classification B64C1/1407. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Jul 20 2021 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 1 related publication on this page (citations in our corpus or others sharing the same primary CPC).