Configurable control panel for an aircraft cockpit and method of configuration for such a panel

US2016362175A1 · US · A1

Patent metadata
FieldValue
Publication numberUS-2016362175-A1
Application numberUS-201615179580-A
CountryUS
Kind codeA1
Filing dateJun 10, 2016
Priority dateJun 11, 2015
Publication dateDec 15, 2016
Grant date

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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.

A configurable control panel for an aircraft cockpit includes a set of universal control modules each comprising at least one screen including at least one manually manipulable control key. Each of the control modules further includes at least one master control module, and at least one universal slave module associated with the master module, and including a screen and at least one control key. The at least one master module is configured to control the screen and the at least one control key of the at least one universal slave module.

First claim

Opening claim text (preview).

What is claimed is: 1 . A configurable control panel for an aircraft cockpit, comprising: a set of universal control modules each comprising at least one screen including at least one manually manipulable control key, wherein each of the control modules further comprises: at least one master control module; and at least one universal slave module associated with the master module, and comprising a screen and at least one control key, and wherein the at least one master module is configured to control the screen and the at least one control key of the at least one universal slave module. 2 . The control panel according to claim 1 , wherein the at least one control key of the at least one master module is configured to select functional systems to be controlled by the control panel, and the at least one slave module is adapted based on the functional systems selected. 3 . The control panel according to claim 1 , further comprising at least one non-configurable control module to control a function of a system of the control panel. 4 . The control panel according to claim 1 , wherein the at least one master control module and slave control module include at least one controller comprising a control algorithm for the control panel. 5 . The control panel according to claim 4 , wherein the controller of the at least one slave control module is configured to control a display on the screen of the at least one slave control module and to configure the at least one control key of the slave control module according to a function dictated by the master control module. 6 . The control panel according to claim 1 , wherein the at least one control key comprises a key selected from the group consisting of a digital control key and an electromechanical control key. 7 . The control panel according to claim 1 , wherein the at least one screen of the set of universal control modules comprises a touch screen. 8 . The control panel according to claim 1 , wherein the at least one screen of the set of universal control modules comprises a non touch-sensitive screen. 9 . A method of configuration of a configurable control panel for an aircraft, the method comprising: manipulating at least one master control module, for selection of a system configured to perform a function controllable by the control panel; and controlling, by a controller, of at least one screen and at least one control key of a set of slave control modules according to the functional system selected, wherein the control panel comprises a set of universal control modules each comprising at least one screen and at least one manually manipulable control key, wherein each of the control modules further comprises: the at least one master control module; and at least one of the slave control modules associated with the at least one master module, and comprising the at least one screen of the set of slave control modules and the at least one control key, and wherein the at least one master control module is configured to control the at least one screen and the at least one control key of the at least one slave control module.

Assignees

Inventors

Classifications

  • Digitisers, e.g. for touch screens or touch pads, characterised by the transducing means · CPC title

  • Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed or acceleration · CPC title

  • controlling a plurality of local displays, e.g. CRT and flat panel display · CPC title

  • B64D43/00Primary

    Arrangements or adaptations of instruments · CPC title

  • B64C13/042Primary

    operated by hand · CPC title

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Frequently asked questions

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What does patent US2016362175A1 cover?
A configurable control panel for an aircraft cockpit includes a set of universal control modules each comprising at least one screen including at least one manually manipulable control key. Each of the control modules further includes at least one master control module, and at least one universal slave module associated with the master module, and including a screen and at least one control key…
Who is the assignee on this patent?
Zodiac Aero Electric
What technology area does this patent fall under?
Primary CPC classification B64D43/00. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Thu Dec 15 2016 00:00:00 GMT+0000 (Coordinated Universal Time) (A1). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).