FR3098500B1 - Method and system for the automatic graphic representation of the calculation points identified in an aircraft structure, on a digital model of the structure of an aircraft - Google Patents

Method and system for the automatic graphic representation of the calculation points identified in an aircraft structure, on a digital model of the structure of an aircraft Download PDF

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Publication number
FR3098500B1
FR3098500B1 FR1907761A FR1907761A FR3098500B1 FR 3098500 B1 FR3098500 B1 FR 3098500B1 FR 1907761 A FR1907761 A FR 1907761A FR 1907761 A FR1907761 A FR 1907761A FR 3098500 B1 FR3098500 B1 FR 3098500B1
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aircraft
digital model
calculation points
points identified
graphic representation
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FR1907761A
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French (fr)
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FR3098500A1 (en
Inventor
Sébastien Salvignol
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Airbus Operations SAS
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Airbus Operations SAS
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Priority to FR1907761A priority Critical patent/FR3098500B1/en
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/10Manufacturing or assembling aircraft, e.g. jigs therefor

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  • Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Transportation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Processing Or Creating Images (AREA)

Abstract

Un système de représentation graphique met en œuvre un procédé de représentation graphique de points de calcul identifiés dans une partie de la structure de l’aéronef. Les point de calcul sont représentés sur une maquette numérique de la partie de la structure de l’aéronef. Le procédé de représentation comporte les étapes suivantes : détermination des coordonnées (E30, E40) d’un point de calcul à partir d’une suite de caractères décrivant le positionnement du point de calcul dans la partie de la structure de l’aéronef, et représentation (E50) du point de calcul, sur la maquette numérique de la partie de la structure de l’aéronef, aux coordonnées déterminées. Figure pour l’abrégé : Fig. 2A graphical representation system implements a method of graphically representing calculation points identified in a part of the structure of the aircraft. The calculation points are represented on a digital model of the part of the structure of the aircraft. The representation method comprises the following steps: determining the coordinates (E30, E40) of a calculation point from a series of characters describing the positioning of the calculation point in the part of the structure of the aircraft, and representation (E50) of the calculation point, on the digital model of the part of the structure of the aircraft, at determined coordinates. Figure for the abstract: Fig. 2

FR1907761A 2019-07-10 2019-07-10 Method and system for the automatic graphic representation of the calculation points identified in an aircraft structure, on a digital model of the structure of an aircraft Active FR3098500B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1907761A FR3098500B1 (en) 2019-07-10 2019-07-10 Method and system for the automatic graphic representation of the calculation points identified in an aircraft structure, on a digital model of the structure of an aircraft

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1907761A FR3098500B1 (en) 2019-07-10 2019-07-10 Method and system for the automatic graphic representation of the calculation points identified in an aircraft structure, on a digital model of the structure of an aircraft
FR1907761 2019-07-10

Publications (2)

Publication Number Publication Date
FR3098500A1 FR3098500A1 (en) 2021-01-15
FR3098500B1 true FR3098500B1 (en) 2021-09-10

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FR1907761A Active FR3098500B1 (en) 2019-07-10 2019-07-10 Method and system for the automatic graphic representation of the calculation points identified in an aircraft structure, on a digital model of the structure of an aircraft

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FR (1) FR3098500B1 (en)

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20070038947A1 (en) * 2005-05-19 2007-02-15 Airbus Method and device for generation of a parametric model associated with a 3D geometry

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Publication number Publication date
FR3098500A1 (en) 2021-01-15

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