Device for the control of an aircraft system in manual pilot mode using notably a head-up display
First Claim
1. A device formed as a replacement for a previously existing portion of a right-hand part of an aircraft instrument panel wherein said device functions to provide control indicators allowing control of an aircraft system in manual pilot mode, said device including a display screen for displaying first information elements normally displayed by said previously existing portion and second information elements for allowing control of approach parameters and providing indications of deviations of said aircraft from a predetermined landing path including providing guidance symbols representing maximum permissible deviation values of said aircraft from said predetermined landing path and wherein said second information elements further include an alarm indicator when said maximum permissable deviation values are exceeded, said alarm indicator including a visual display including providing a visible indication resulting from a change in the background color of the predetermined bounded area where said guidance symbols are located.
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Accused Products
Abstract
A device to control an aircraft system in manual pilot mode, using notably a head-up display, is constituted by a display screen located at the position of a piece of equipment of the right-hand part of the instrument panel, the screen displaying information elements delivered by the replaced equipment and information elements to control the piloting task. Application for the controlling of a manual pilot phase by a co-pilot in an aircraft using a head-up display.
36 Citations
11 Claims
- 1. A device formed as a replacement for a previously existing portion of a right-hand part of an aircraft instrument panel wherein said device functions to provide control indicators allowing control of an aircraft system in manual pilot mode, said device including a display screen for displaying first information elements normally displayed by said previously existing portion and second information elements for allowing control of approach parameters and providing indications of deviations of said aircraft from a predetermined landing path including providing guidance symbols representing maximum permissible deviation values of said aircraft from said predetermined landing path and wherein said second information elements further include an alarm indicator when said maximum permissable deviation values are exceeded, said alarm indicator including a visual display including providing a visible indication resulting from a change in the background color of the predetermined bounded area where said guidance symbols are located.
Specification