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Cabin pressure open loop control system

A cockpit pressure and open-loop control technology, which is applied in air handling equipment, aircraft parts, transportation and packaging, etc., can solve the problems of improving control accuracy, achieve the effect of improving control accuracy, ensuring comfort, and ensuring the safety of aircraft structure

Inactive Publication Date: 2016-11-02
XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] Digital cockpit pressure control technology is currently widely used in aircraft cockpit pressure control systems. Classical control theory is applied to realize closed-loop control of cockpit pressure and realize information interaction and sharing of the whole aircraft. However, the control accuracy needs to be further improved during the control process.

Method used

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  • Cabin pressure open loop control system

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Embodiment Construction

[0015] In order to make the objectives, technical solutions and advantages of the present invention clearer, the technical solutions in the embodiments of the present invention will be described in more detail below in conjunction with the drawings in the embodiments of the present invention. In the drawings, the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The described embodiments are some, but not all, embodiments of the invention. The embodiments described below by referring to the figures are exemplary and are intended to explain the present invention and should not be construed as limiting the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention. Embodiments of the present invention will be described in detail below ...

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Abstract

The invention discloses a cabin pressure open loop control system, and belongs to the airplane environment control technical field; one end of the cabin is provided with an air supply pipeline; a cabin air supply flow device is arranged in the air supply pipeline; a cabin pressure sensor and a cabin temperature sensor are arranged in the cabin; the bottom of the cabin is provided with an exhaust valve; the exhaust valve is connected with an exhaust valve motor, an exhaust valve driver and an exhaust valve order forming module in sequence from top to bottom; the exhaust valve order forming module is respectively connected with the cabin pressure sensor, the cabin temperature sensor, the cabin air supply flow device, and a cabin pressure system module; the cabin air supply flow, the cabin temperature, the cabin pressure and flight height parameters are combined so as to realize the cabin pressure open loop control, thus improving cabin pressure control precision, and ensuring passengers comfortable and airplane composition safety.

Description

technical field [0001] The invention belongs to the technical field of aircraft environment control, and in particular relates to a cockpit pressure open-loop control system. Background technique [0002] At present, the main technologies applied in the field of aircraft cockpit pressure control at home and abroad include pneumatic cockpit pressure control technology, electropneumatic cockpit pressure control technology and digital cockpit pressure control technology. [0003] Pneumatic cockpit pressure control technology was used in earlier aircrafts. Since the computer control technology at that time had not been greatly developed, pneumatic cockpit pressure control technology became the main method of cockpit pressure control. Pneumatic cockpit pressure control technology can realize the control of cockpit pressure, but the accuracy of pneumatic cockpit pressure control is poor due to the long connecting pipeline of pneumatic control, high installation requirements, and h...

Claims

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Application Information

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IPC IPC(8): B64D13/04
CPCB64D13/04
Inventor 杨文强张翠峰
Owner XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
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