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Diagnosing system for detecting ergent state for assembling process for body of airplane, and the method thereof

A technology of emergency state, diagnosis system, applied in the direction of registering/instructing the work of machines, instruments, registering/instructing, etc., can solve problems such as damage to the fuselage

Inactive Publication Date: 2009-10-28
AIRBUS OPERATIONS GMBH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

This is a difficult process and may cause damage to the airframe

Method used

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  • Diagnosing system for detecting ergent state for assembling process for body of airplane, and the method thereof
  • Diagnosing system for detecting ergent state for assembling process for body of airplane, and the method thereof
  • Diagnosing system for detecting ergent state for assembling process for body of airplane, and the method thereof

Examples

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Embodiment Construction

[0040] figure 1 Shown is a schematic view of a fuselage 101 with references 102 , 103 , 104 , 105 , 106 , 107 , 108 and 109 according to an exemplary embodiment of the present invention. Body 101 and marks 102 to 109 can be displayed on an output unit 100 (shown in Figure 4 middle) on the screen.

[0041] In case of an emergency - which occurs eg at the location indicated by the arrow 105 - the arrow 105 is highlighted or changes color (eg from green to red) on the output screen.

[0042] It should be noted, however, that other types of indication methods may be used in order to indicate where the emergency situation has occurred. For example, the coordinates of the present invention may be output to the screen, or a picture of the location where the emergency occurred may be displayed on the screen, thereby indicating to the user the area involved in the emergency.

[0043] Thus, the user can quickly determine where the fault has occurred and determine what steps should b...

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PUM

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Abstract

According to an exemplary embodiment of the present invention, there is provided a diagnostic system for detecting an emergency during the assembly of an aircraft fuselage, the diagnostic system being adapted to detect the emergency and to output information about the actual location of the emergency information. This provides rapid identification of errors during aircraft assembly.

Description

technical field [0001] The invention relates to the field of aircraft assembly. More specifically, the invention relates to a diagnostic system for detecting an emergency during the assembly of an aircraft fuselage, and to a method, a computer-readable medium, a data processing unit and a program unit for detecting an emergency. Background technique [0002] In order to assemble an aircraft, the fuselage of the aircraft must be moved from its construction site to a final assembly location, which may be located at a different construction site. This is a difficult process that can cause damage to the airframe. Contents of the invention [0003] The object of the invention is to improve the assembly of aircraft fuselages. [0004] According to an exemplary embodiment of the present invention, a diagnostic system for detecting an emergency during an aircraft fuselage assembly process is provided, the diagnostic system includes a system for detecting an emergency when the fu...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G07C3/00
Inventor 霍斯特·科特
Owner AIRBUS OPERATIONS GMBH
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