A display touch interaction system applied to aircraft cockpit

An interactive system and cockpit technology, applied in the field of display touch interactive systems, can solve the problem that the anti-mistouch design cannot meet the needs of flight safety, etc., and achieve the effects of improving user experience, improving communication efficiency, and reducing interference information.

Active Publication Date: 2020-11-17
BEIJING AERONAUTIC SCI & TECH RES INST OF COMAC +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] In summary, the anti-false touch design in the existing touch screen technology cannot meet the needs of flight safety when applied in the cockpit of an aircraft

Method used

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  • A display touch interaction system applied to aircraft cockpit
  • A display touch interaction system applied to aircraft cockpit
  • A display touch interaction system applied to aircraft cockpit

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Embodiment Construction

[0038] In order to make the object, technical solution and advantages of the present invention clearer, the present invention will be further described in detail below in combination with specific embodiments and with reference to the accompanying drawings. It should be understood that these descriptions are exemplary only, and are not intended to limit the scope of the present invention. Also, in the following description, descriptions of well-known structures and techniques are omitted to avoid unnecessarily obscuring the concept of the present invention.

[0039] Such as Figure 1-5As shown, in the first embodiment of the display touch interaction system applied to the aircraft cockpit provided by the present invention, it includes the front control interface at the top of the cockpit, the rear control interface at the top of the cockpit, and the first control interface at the front of the central console. interface, the second control interface in front of the center cons...

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Abstract

The invention discloses a display touch control interactive system applied to an aircraft cockpit, which relates to the aircraft technical field. The system comprises a cockpit top front control interface, a cockpit top rear control interface, a first control interface in front of a central console, a second control interface in front of the central console and a rear control interface of the central console; at least one of a cockpit top front control interface, a cockpit top rear control interface, a first control interface in front of a center console, a second control interface in front ofthe center console, and a center console rear control interface includes a two-position sliding controller; the two-position sliding controller includes a slider, a slideway, ON bit and OFF bit respectively set at both ends of the slideway and APU self-test progress bar. The invention has the advantages of high anti-miscontact performance, saving cockpit space, lightening pilot operation task andthe like.

Description

technical field [0001] The invention relates to the technical field of aircraft, in particular to a display and touch interaction system applied to an aircraft cockpit. Background technique [0002] In the prior art, there are hundreds of physical operation controls (including buttons and knobs) on the operation panel of the aircraft cockpit, which occupy a relatively large space in the cockpit. Among the hundreds of operating controls, usually only a few dozen are used frequently, and most of them are only used occasionally in certain flight scenarios. The operation panel of this kind of physical operation control leads to the waste of cockpit space on the one hand, and makes the pilot's operation task heavy on the other hand. [0003] At present, products equipped with touch screens have been integrated into every aspect of our lives. The touch electronic flight bag (EFB) has also been brought into the cockpit of civil aircraft, and is loved by more and more pilots. The...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64D43/00G06F3/041
CPCB64D43/00G06F3/0412G06F3/0416
Inventor 樊谕涵张炯蒋欣
Owner BEIJING AERONAUTIC SCI & TECH RES INST OF COMAC
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