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 PDFInfo
- 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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- FR
- France
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- aircraft
- digital model
- calculation points
- points identified
- graphic representation
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND 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
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/10—Manufacturing 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
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 |
Family
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
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 |
Country Status (1)
Country | Link |
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FR (1) | FR3098500B1 (en) |
Family Cites Families (1)
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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2019
- 2019-07-10 FR FR1907761A patent/FR3098500B1/en active Active
Also Published As
Publication number | Publication date |
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FR3098500A1 (en) | 2021-01-15 |
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