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Human-computer interaction terminal for manned spacecraft

A human-computer interaction terminal and manned spacecraft technology, applied in the field of spacecraft, can solve the problems of equipment occupying a large space, hidden dangers to user safety, fragile, etc., so as to increase equipment reliability, reduce interference, and reduce power consumption. Effect

Pending Publication Date: 2020-04-17
BEIJING SPACE TECH RES & TEST CENT
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Liquid crystal OLED displays are heavy, and the device takes up a lot of space. The surface of the liquid crystal display device is glass, which is fragile. Once broken, it will bring great safety hazards to users in the space environment
In summary, the existing spacecraft displays can no longer meet the requirements for display equipment in the third phase of the manned phase

Method used

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  • Human-computer interaction terminal for manned spacecraft
  • Human-computer interaction terminal for manned spacecraft
  • Human-computer interaction terminal for manned spacecraft

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Embodiment Construction

[0048] In order to more clearly describe the embodiments of the present invention or the technical solutions in the prior art, the following will briefly introduce the drawings that are used in the embodiments. Apparently, the drawings in the following description are only some embodiments of the present invention, and those skilled in the art can also obtain other drawings according to these drawings without creative efforts.

[0049] When describing the embodiments of the present invention, the terms "vertical", "transverse", "upper", "lower", "front", "rear", "left", "right", "vertical", " The orientation or positional relationship expressed by "horizontal", "top", "bottom", "inner" and "outer" is based on the orientation or positional relationship shown in the relevant drawings, which are only for the convenience of describing the present invention and simplifying the description, and It is not to indicate or imply that the device or element referred to must have a particu...

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Abstract

The invention relates to a man-machine interaction terminal for a manned spacecraft. The man-machine interaction terminal comprises a shell (1); a touch display (2) which is arranged on one surface ofthe shell (1); a key group (3) which is arranged on the same surface of the shell (1) together with the touch display (2) and is arranged around the touch display (2); and a processing module which is arranged in the shell (1) and is used for receiving input signals of the key group (3) and the touch display (2) and controlling the display content of the touch display (2); and the touch display (2) comprises a touch screen and an OLED display. According to the man-machine interaction terminal, the OLED displayer is used, no glass component is contained, and therefore the man-machine interaction terminal is high in reliability, not prone to breakage, small in size and light in weight.

Description

technical field [0001] The invention relates to the field of spacecraft, in particular to a human-computer interaction terminal for a manned spacecraft. Background technique [0002] my country's manned spaceflight project has gone through two phases of manned phase I and manned phase II, and is now fully entering the development phase of manned phase III. During this process, information display technology is also following the development of manned spaceflight. Improving constantly. The display equipment of the first-stage manned spacecraft is generally implemented by transplanting ground-use display equipment, which has defects in adapting to the space environment and reliability, and is not suitable for the special use environment of manned spacecraft. In the second phase, the design of the display equipment of the spacecraft has been improved. The backlight source of the liquid crystal display is changed from the traditional cold cathode fluorescent lamp (CCFL) backligh...

Claims

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Application Information

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IPC IPC(8): G06F3/041H01L27/32
CPCG06F3/041H10K59/40
Inventor 张东璞李皖玲郭卫国赵岩松王海龙刘喆梁吴迪张天湘武雯
Owner BEIJING SPACE TECH RES & TEST CENT