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Method for assembling an aircraft fuselage section, and multipurpose mounting support, gear and fuselage section production unit for implementing said method

A technology for installing brackets and sections, which is applied in the field of production units for producing fuselage sections, and can solve problems such as low utilization rate and increase in the number of production units.

Pending Publication Date: 2020-03-31
AIRBUS OPERATIONS (SAS) +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Therefore, each production unit is dedicated to one aircraft family, which tends to increase the number of production units
Also, depending on each aircraft family to be produced, one production unit may be underutilized while others are at maximum production capacity

Method used

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  • Method for assembling an aircraft fuselage section, and multipurpose mounting support, gear and fuselage section production unit for implementing said method
  • Method for assembling an aircraft fuselage section, and multipurpose mounting support, gear and fuselage section production unit for implementing said method
  • Method for assembling an aircraft fuselage section, and multipurpose mounting support, gear and fuselage section production unit for implementing said method

Examples

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Embodiment Construction

[0056] exist figure 1 In , a fuselage section 10 is shown, which has an approximately cylindrical shape and an axis A10 (parallel to the longitudinal direction). The fuselage section 10 extends between a first transverse peripheral edge 10a and a second transverse peripheral edge 10b arranged in a transverse plane. The fuselage section 10 comprises a structure 12 comprising longitudinal reinforcements 14.1 (referred to as smooths) and transverse reinforcements 14.2 (referred to as frames) and a skin 16 attached to the structure 12.

[0057] like figure 2 As shown, according to the first embodiment, the fuselage section 10 has an approximately circular cross section S1 or, in the second embodiment, an approximately oval cross section S2.

[0058] According to one arrangement, the fuselage section 10 comprises six circumferentially distributed panels 18.1 to 18.6: a lower panel 18.1, a lower right transverse panel 18.2 and a lower left transverse panel 18.3, an upper right tr...

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Abstract

The invention relates to a method for assembling a fuselage section (10). The method comprises producing a lower part of the section from at least two panels (18.4 to 18.6) and an upper part of the section from at least two panels (18.1 to 18.3), then assembling the lower and upper parts (34, 36) so as to obtain the fuselage section (10). A lower mounting support (54) or an upper mounting support(56), a gear and a production unit are used in the method.

Description

technical field [0001] The present application relates to a method for assembling an aircraft fuselage section from two superimposed upper and lower sections, a multifunctional mounting bracket and a tool for carrying out the above method and a production unit for producing a fuselage section for carrying out the above method. Background technique [0002] For the purposes of this disclosure, the longitudinal direction is parallel to the axis of the aircraft fuselage, which extends generally between the nose and the rear tip of the fuselage. The transverse plane is perpendicular to the longitudinal direction. [0003] The fuselage consists of a structure consisting of longitudinal and transverse stiffeners and panels attached to the structure. The fuselage is obtained by assembling several sections end-to-end, each section obtained by assembling several panels according to the cross-section of the fuselage. Thus, for a civil aircraft with a small cross-section, the fuselag...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F5/10B64F5/50
CPCB64F5/10B64F5/50B64C1/061B64C1/069B64C1/12B64C2211/00B21J15/142B21J15/42B23K37/0408B23K37/0426B23K37/053B23K2101/006B23K2101/06B23P11/00Y10T29/49826B23P13/00Y10T29/49622
Inventor J-M·达塔斯J-M·布兰多A·阿奎拉P·吉贝尔
Owner AIRBUS OPERATIONS (SAS)