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Aircraft engine compartment fire alarm detection system

An engine compartment and fire alarm detection technology, which is applied to aircraft fire prevention/corrosion protection, aircraft parts, aircraft indicating devices, etc. The effect of reducing the false alarm rate

Active Publication Date: 2022-03-25
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

In the traditional single-loop fire detection system, once the fire detector fails, it is easy to cause false fire alarms, which increases the burden on the crew and affects the flight mission.

Method used

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  • Aircraft engine compartment fire alarm detection system

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Embodiment Construction

[0022] In order to make the purpose, technical solution and advantages of the application more clear, the technical solution in the embodiment of the application will be described in more detail below in conjunction with the drawings in the embodiment of the application. 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 application. The embodiments described below by referring to the figures are exemplary, and are intended to explain the present application, and should not be construed as limiting the present application. Based on the embodiments in this application, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of this application. Embodiments of the present application will be described in detail below in conjunction with th...

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PUM

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Abstract

The invention belongs to the field of aero-engines, and particularly relates to an aircraft engine compartment fire alarm detection system. Fire alarm detectors in a single engine compartment are divided into two groups, and the two fire alarm detectors arranged in parallel in each group are connected in series, so that the possibility of false alarm of a fire alarm detection system caused by false alarm faults of a single fire alarm detector is reduced, and the false alarm rate is reduced; the two groups of fire alarm detectors are connected in parallel in a fire alarm manner, so that missed alarms are reduced, and the reliability of the fire alarm detection system is improved. The fire alarm in each engine compartment can be displayed in the aviation cockpit through independent voice alarm and light alarm, and can be positioned to any engine compartment. Fault alarms of the four fire detectors in each engine compartment are connected in parallel, and faults of any fire detector can be alarmed and displayed in the engine compartment through lamplight. Fire alarm and fault information of each fire alarm detector is independently sent to the display control computer and the flight parameter system for recording.

Description

technical field [0001] The application belongs to the field of aero-engines, and in particular relates to a fire detection system for an aircraft engine compartment. Background technique [0002] The fire in the aircraft engine compartment seriously threatens flight safety. When a fire occurs in the engine compartment, it should be able to send a timely and reliable alarm to the crew. The engine compartment fire detection system should not only avoid missing alarms, but also reduce the false alarm rate. In the traditional single-circuit fire detection system, once a false alarm failure occurs in the fire detector, it is easy to cause the system to report a false fire alarm, increase the burden on the crew, and affect the flight mission. However, the dual-circuit fire detection system, which uses electromechanical computer for logical judgment, has higher requirements on the aircraft's own electromechanical management system. [0003] Therefore, it is desirable to have a te...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D45/00
CPCB64D45/00B64D2045/009
Inventor 孔雪张沛王娟闫伟伟
Owner XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
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