FR2974268B1 - METHOD FOR DETERMINING THE ANGULAR POSITIONING OF A COMPONENT MOUNTED ON A FILIFORM PATH, ASSEMBLY METHOD, AND ASSOCIATED SYSTEM - Google Patents

METHOD FOR DETERMINING THE ANGULAR POSITIONING OF A COMPONENT MOUNTED ON A FILIFORM PATH, ASSEMBLY METHOD, AND ASSOCIATED SYSTEM

Info

Publication number
FR2974268B1
FR2974268B1 FR1101129A FR1101129A FR2974268B1 FR 2974268 B1 FR2974268 B1 FR 2974268B1 FR 1101129 A FR1101129 A FR 1101129A FR 1101129 A FR1101129 A FR 1101129A FR 2974268 B1 FR2974268 B1 FR 2974268B1
Authority
FR
France
Prior art keywords
line
determining
reference plane
path
filiform
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.)
Active
Application number
FR1101129A
Other languages
French (fr)
Other versions
FR2974268A1 (en
Inventor
Gregory Mouge
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Dassault Aviation SA
Original Assignee
Dassault Aviation SA
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Dassault Aviation SA filed Critical Dassault Aviation SA
Priority to FR1101129A priority Critical patent/FR2974268B1/en
Publication of FR2974268A1 publication Critical patent/FR2974268A1/en
Application granted granted Critical
Publication of FR2974268B1 publication Critical patent/FR2974268B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02G—INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINED OPTICAL AND ELECTRIC CABLES OR LINES
    • H02G3/00—Installations of electric cables or lines or protective tubing therefor in or on buildings, equivalent structures or vehicles
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F30/00—Computer-aided design [CAD]
    • G06F30/10—Geometric CAD
    • G06F30/15—Vehicle, aircraft or watercraft design
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F2113/00—Details relating to the application field
    • G06F2113/16—Cables, cable trees or wire harnesses

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Geometry (AREA)
  • Theoretical Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Computational Mathematics (AREA)
  • Pure & Applied Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Structural Engineering (AREA)
  • Civil Engineering (AREA)
  • Mathematical Analysis (AREA)
  • Mathematical Optimization (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Computer Hardware Design (AREA)
  • Evolutionary Computation (AREA)
  • General Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • Automatic Assembly (AREA)
  • Supply And Installment Of Electrical Components (AREA)

Abstract

The method involves determining a line (70) representing a spatial arrangement of a threaded path (16), and defining a reference plane (P1) passing via a point (76) of the line that is located at components (18A) i.e. connectors. Another reference plane (P2) passing through another point (90) of the line is defined, where another line (78) is arranged parallel to the former line and passes through the former reference plane. An angular position of the components is calculated with respect to the latter reference plane. The latter line is formed as generating line. Independent claims are also included for the following: (1) a method for manufacturing a wiring element of a platform (2) a system for determining an angular position of a component.
FR1101129A 2011-04-13 2011-04-13 METHOD FOR DETERMINING THE ANGULAR POSITIONING OF A COMPONENT MOUNTED ON A FILIFORM PATH, ASSEMBLY METHOD, AND ASSOCIATED SYSTEM Active FR2974268B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1101129A FR2974268B1 (en) 2011-04-13 2011-04-13 METHOD FOR DETERMINING THE ANGULAR POSITIONING OF A COMPONENT MOUNTED ON A FILIFORM PATH, ASSEMBLY METHOD, AND ASSOCIATED SYSTEM

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1101129A FR2974268B1 (en) 2011-04-13 2011-04-13 METHOD FOR DETERMINING THE ANGULAR POSITIONING OF A COMPONENT MOUNTED ON A FILIFORM PATH, ASSEMBLY METHOD, AND ASSOCIATED SYSTEM

Publications (2)

Publication Number Publication Date
FR2974268A1 FR2974268A1 (en) 2012-10-19
FR2974268B1 true FR2974268B1 (en) 2013-05-31

Family

ID=44550223

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1101129A Active FR2974268B1 (en) 2011-04-13 2011-04-13 METHOD FOR DETERMINING THE ANGULAR POSITIONING OF A COMPONENT MOUNTED ON A FILIFORM PATH, ASSEMBLY METHOD, AND ASSOCIATED SYSTEM

Country Status (1)

Country Link
FR (1) FR2974268B1 (en)

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1267284B1 (en) * 2001-06-13 2007-02-21 Sumitomo Wiring Systems, Ltd. Three-dimensional virtual method, computer program and system
JP4542791B2 (en) * 2003-05-15 2010-09-15 矢崎総業株式会社 Method for calculating torsion angle in wire-like structure, apparatus and program thereof
JP4383114B2 (en) * 2003-07-31 2009-12-16 矢崎総業株式会社 Method for calculating rotation angle of wire harness, apparatus and program thereof

Also Published As

Publication number Publication date
FR2974268A1 (en) 2012-10-19

Similar Documents

Publication Publication Date Title
FR3007461B1 (en) METHOD AND SYSTEM FOR STARTING AN AIRCRAFT TURBOMACHINE
FR3007460B1 (en) METHOD AND SYSTEM FOR STARTING AN AIRCRAFT TURBOMACHINE BY REAL TIME REGULATION OF AIR FLOW.
FR3004250B1 (en) METHOD FOR DETERMINING A TRACKING PATH OF AN AIRCRAFT ON AN AIRPORT ZONE.
MX2013008072A (en) System, method, and article to prompt behavior change.
WO2013160655A9 (en) An outlet module for an emissions cleaning module
IN2014DE01235A (en)
WO2013186629A3 (en) Seismic trace attribute
IN2014DN07382A (en)
FR2995236B1 (en) IMPROVED METHOD AND SYSTEM FOR FRICTION WELDING MIXING OF A STIFFENER ON AN AIRCRAFT PANEL
MX338124B (en) Acoustic string instrument.
TR201905652T4 (en) Assembly for mounting and removing a part on a gas turbine.
FR2974904B1 (en) METHOD AND SYSTEM FOR DETERMINING THE ANTI-BLUE PERFORMANCE OF A TRANSPARENT OPTICAL ARTICLE
FR2998702B1 (en) METHOD FOR DYNAMICALLY DETERMINING THE POSITION OF THE STOPPING POINT OF AN AIRCRAFT ON A FIELD AND ASSOCIATED SYSTEM
FR3010740B1 (en) SYSTEM AND METHOD FOR EMERGENCY STARTING AN AIRCRAFT TURBOMACHINE
FR2979708B1 (en) METHOD FOR CHARACTERIZING THE SENSITIVITY OF AN ELECTRONIC COMPONENT SUBJECT TO IRRADIATION CONDITIONS
FR3004582B1 (en) SYSTEM AND METHOD FOR OPTICALLY INSPECTING ELECTRONIC CIRCUITS
MX2015007897A (en) Electronic device and method for producing an electronic device.
FR3006078B1 (en) METHOD FOR DEFINING FIBER PATHWAYS FROM A VECTOR FIELD
WO2013039796A3 (en) Scale-out system to acquire event data
DE602007003962D1 (en) SAFETY METHOD FOR DIAGNOSTIC SYSTEMS
SA516380575B1 (en) A method for designing an integrated computational element technique
FR2974268B1 (en) METHOD FOR DETERMINING THE ANGULAR POSITIONING OF A COMPONENT MOUNTED ON A FILIFORM PATH, ASSEMBLY METHOD, AND ASSOCIATED SYSTEM
FR2995497B1 (en) AIRCRAFT TURBOMACHINE COMPRISING AT LEAST ONE COOLING SYSTEM OF AT LEAST ONE ELECTRONIC DEVICE
BR112015030239A2 (en) subsea chiller module, subsea chiller, and method for cooling a subsea chiller
BR112013025746A2 (en) top-tensioned offshore riser floating brass system and field development methods

Legal Events

Date Code Title Description
PLFP Fee payment

Year of fee payment: 6

PLFP Fee payment

Year of fee payment: 7

PLFP Fee payment

Year of fee payment: 8

PLFP Fee payment

Year of fee payment: 10

PLFP Fee payment

Year of fee payment: 11

PLFP Fee payment

Year of fee payment: 12

PLFP Fee payment

Year of fee payment: 13

PLFP Fee payment

Year of fee payment: 14