System and method for acquiring weight center of gravity of aircraft passenger

An aircraft passenger and weight technology, which is used in the testing of machine/structural components, measuring devices, computer components, etc., can solve the problems of increased system failure rate, heavy sensor equipment, and difficulty in accurately measuring the center of gravity of passenger weight, achieving universal Good performance, reduce weight burden, reduce the effect of system failure rate

Pending Publication Date: 2022-03-22
COMAC +1
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  • Application Information

AI Technical Summary

Problems solved by technology

[0005] However, load cells are arranged in front of each passenger seat, which brings an additional cost to the total weight of the aircraft, especially in medium and long-range wide-body aircraft, the aircraft with 300 or 400 seats needs to be arranged Too many sensors, the weight of the sensor device is too heavy
In addition, as the number of load cells increases, the system complexity and the number of connected wires increase, and the failure rate of the system also increases
When some of these load cells fail, it is difficult to accurately measure the center of gravity of the passenger's weight

Method used

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  • System and method for acquiring weight center of gravity of aircraft passenger
  • System and method for acquiring weight center of gravity of aircraft passenger
  • System and method for acquiring weight center of gravity of aircraft passenger

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Embodiment Construction

[0039] The present invention will be further described below in conjunction with specific embodiment and accompanying drawing, set forth more details in the following description in order to fully understand the present invention, but the present invention can obviously be implemented in many other ways different from this description , those skilled in the art can make similar promotions and deductions based on actual application situations without violating the connotation of the present invention, so the content of this specific embodiment should not limit the protection scope of the present invention.

[0040] figure 1 A system for obtaining the center of gravity of aircraft passengers according to a preferred embodiment of the present invention is schematically shown, which includes a data collection module 10 for collecting passenger information and a data processing module 20 in electrical communication with the data collection module 10 .

[0041] In a preferred embodi...

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Abstract

The invention provides a system and method for obtaining the gravity center of the weight of an aircraft passenger. The system comprises a data acquisition module, the data acquisition module is provided with an identity acquisition module, and the identity acquisition module is used for acquiring seat information corresponding to each passenger in passengers; the weight acquisition module is used for correspondingly acquiring weight information corresponding to each passenger in the passengers; the data processing module is in electrical communication with the data acquisition module, and the data processing module is provided with a data storage module which stores the acquired seat information and weight information corresponding to each passenger in the passengers as reference data; and the data calculation module calculates the reference data to obtain the total weight and the gravity center of the passenger.

Description

technical field [0001] The invention relates to a system and method for obtaining the weight center of gravity of aircraft passengers, belonging to the field of overall design weight and balance. Background technique [0002] In the process of aircraft operation, the center of gravity of aircraft weight is of great significance to flight safety. Among them, the center of gravity of passenger weight, as an important part of the total weight and center of gravity of the aircraft, plays a decisive role in judging whether the aircraft is safe to fly. [0003] However, in the current aircraft operation, the weight of passengers is usually determined according to the preset value of the airline or operating regulations, there is a certain deviation from the actual weight, and the flight attendants walk through the cockpit and manually count the adult passengers and passengers in each area. The manual process of calculating an approximate aircraft center of gravity based on the num...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01M1/12G06K7/10
CPCG01M1/125G06K7/10821
Inventor 王瑞沈轶钒陈勇
Owner COMAC
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