Analog cabin boost gauge

A cabin and instrument technology, applied in simulators, simulation devices and instruments of space navigation conditions, etc., can solve the problems of weak sense of reality, inability to perceive instrument devices, and inability to achieve training effects, and achieve the improvement of realism. Effect

Inactive Publication Date: 2015-06-17
天津奥捷航空科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

The shortcoming of this simulated operation form is that the sense of reality is not strong,

Method used

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  • Analog cabin boost gauge

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Embodiment Construction

[0008] The patent of the present invention will be further described in detail below in conjunction with specific embodiments.

[0009] Such as figure 1 As shown, the structural principle diagram of the simulated cabin pressurization meter of the patent of the present invention; the simulated cabin pressurization meter includes a servo control circuit board, a cabin pressurization pointer, a cabin pressurization scale surface sticker, a cabin pressurization scale panel, and a cabin pressurization front panel ; It is characterized in that: under the control of the servo control circuit board, the cabin pressurization pointer moves to the position indicated by the cabin pressurization scale sticker. The control circuit board 2 of the cabin pressurization server is equipped with a screw column 3 for fixing the cabin pressurization scale panel 4, the cabin pressurization pointer 1 is installed in the middle of the cabin pressurization scale panel 4, and the cabin pressurization sc...

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Abstract

The invention discloses an analog cabin boost gauge. The analog cabin boost gauge comprises a server control circuit board, a cabin pressure-boost pointer, a cabin pressure-boost scaled patch, a cabin pressure-boost scaled panel wherein a cabin pressure-boost front panel, wherein the server control circuit board controls the cabin pressure-boost pointer to be moved to a position indicated by the cabin pressure-boost scaled patch. Through analog machine climbing instrument equipment, a trainee can experience the cabin pressure-boost reading value consistent with a real instrument; and through the cabin pressure-boost instrument consistent with a real aircraft during aircraft take-off and landing simulation, the reality of aircraft simulation can be greatly improved.

Description

technical field [0001] The patent of the present invention relates to a simulated cabin pressurization gauge. Background technique [0002] The analog cabin pressurization gauge is an instrument used to display the cabin pressurization readings of an aircraft simulator. The cabin pressurization instrument is a device that displays the aircraft cabin pressurization. By simulating the cabin pressurization instrument equipment in a real aircraft, flight training is provided. A realistic simulated environment. That is, it is a device used during take-off and landing to show the location of aircraft cabin pressurization through instrument reading indication. At present, the simulated cabin pressurization gauge is replaced by software to realize the cabin pressurization instrument in the real environment. The shortcoming of this simulated operation form is that the sense of reality is not strong, and the real instrument device cannot be perceived, so the training effect cannot b...

Claims

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Application Information

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IPC IPC(8): G09B9/16
CPCG09B9/165
Inventor 胡伟
Owner 天津奥捷航空科技有限公司
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