OEM Design Definition Issues - JTEG...3 of 24 Misinterpretation of the Blueprint 3D Model of...

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OEM Design Definition Issues ISSC Engineering Team, FRCSW Code 43353 Presented 28 April 2014 Rick Mendoza 1 of 24 NAVAIR public release SPR-2014-342 Distribution A -- Approved for public release distribution is unlimited

Transcript of OEM Design Definition Issues - JTEG...3 of 24 Misinterpretation of the Blueprint 3D Model of...

Page 1: OEM Design Definition Issues - JTEG...3 of 24 Misinterpretation of the Blueprint 3D Model of Structural Former – Translated from 2D Blueprint NAVAIR Public Release SPR-2014-341 Obstacles

OEM Design Definition Issues

ISSC Engineering Team, FRCSW Code 43353 Presented 28 April 2014 Rick Mendoza

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NAVAIR public release SPR-2014-342 Distribution A -- Approved for public release

distribution is unlimited

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Page 2: OEM Design Definition Issues - JTEG...3 of 24 Misinterpretation of the Blueprint 3D Model of Structural Former – Translated from 2D Blueprint NAVAIR Public Release SPR-2014-341 Obstacles

Synopsis • Existing Manufacturing Process Requires

3D Solid Model for CAM Software. – 2D, Blueprint Defined Engineering Data

• 2D-3D translation subject to Human error. • OEM Blueprint can incorrectly define Part.

– MBD Data • Can have quality issues • Can incorrectly define part

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Misinterpretation of the Blueprint

3D Model of Structural Former – Translated from

2D Blueprint

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Presenter
Presentation Notes
Obstacles to Creating Accurate 3-D Solid Models: Misinterpretations of the Blueprints Narrowing in Y419 Solid model (Click for next slide)
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Misinterpretation of the Blueprints

Actual Fuselage ML Theoretical

Fuselage ML

Location of Moldline discrepancy

View Looking AFT

View Looking FWD

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Obstacles to Creating Accurate 3-D Solid Models: Misinterpretations of the Blueprints Reasons/Location for the error Theoretical Fuselage Moldline – before addition of the Diverter Actual fuselage Moldline – current configuration of the F/A-18 A thru D (Click for next slide)
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Misinterpretation of the Blueprints

After correcting solid model

Prior to correcting solid model

Point cloud data

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Presentation Notes
Obstacles to Creating Accurate 3-D Solid Models: Misinterpretations of the Blueprints Narrowing in Y419 Solid model Images of the Solid models before and after corrections were made to the solid model. Comparison between the point cloud data (taken by scanning the original part) and the solid model Reiterate the importance of EQUIVALENCE (Click for next slide)
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Structural Former

Blueprint Errors – Missing information

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Obstacles to Creating Accurate 3-D Solid Model: Errors in the Blueprint – Missing information Intro slide with Y442.00 Duct former as background Address 2 types of errors missing information and extra or erroneous information (Click next slide)
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Blueprint Errors – Missing information

Nacelle Moldline

Duct Moldline

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Presentation Notes
Obstacles to Creating Accurate 3-D Solid Model: Errors in the Blueprint – Missing information Loft Data illustrations Cut away of the Nacelle and Duct Moldline at location Y442 Brief explanation of the loft data and how it is used to create the solid model (click for next slide)
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Trace Nacelle ML

Trace Duct ML

Trace Duct ML

Trace Diverter ML

Actual ML

Blueprint Errors – Missing information

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Obstacles to Creating Accurate 3-D Solid Models: Errors in the Blueprint – Missing information ML TRACE as called out Reference the look of the blueprint (click next) Show how the contours do not match (click next) ML TRACE as needed We need more information to produce the geometry needed. (Click for next slide)
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Example of incorrect call-out on a blueprint

Missile Fairing ML Fin Dent ML (Correct)

Blueprint Errors – Wrong Information

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Blueprint Showed former Approx. 0.190” lower

.190” The change in height also affects the position of the flange

Blueprint Errors – Wrong Information

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Blueprint Errors – Wrong Information Discovered after Aircraft Fuselage already spliced together Protrusion of Former prevented MLG Door from closing Required Cut and Splice repair after former installation

Former Cut Area

Repair Piece with Correct Mold Line

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Blueprint Errors – Wrong Information Complete Splice Repair Installation

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Blueprint Errors – Conflicting information

Hinge Half Assembly

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Obstacles to Creating Accurate 3-D Solid Models: Errors in the Blueprint – Conflicting information Intro title page w/ photo of inboard, aileron support Point out how this is a wing part and not the fuselage. The problems are not isolated. (Click for next slide)
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Blueprint Errors – Conflicting information

-B-

WING LWR OML

WING REF PLANE

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Obstacles to Creating Accurate 3-D Solid Models: Errors in the Blueprint – Conflicting information Blueprint Point out how the side walls are explicitly defined by dimensions from datum –B-, angle measurements, ml measurements as well as locations of radii. (Click for next slide)
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Blueprint Errors – Conflicting information

Reproduction of Section View F-F After Correction

WING LWR OML

WING REF PLANE

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Presentation Notes
Obstacles to Creating Accurate 3-D Solid Models: Errors in the Blueprint – Conflicting information Blueprint recreation Point out the how the engineer had to make a decision to float the .50 radius in order to maintain surface accuracy. (Click for next slide)
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Part Received from DLA Supply

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Vs.

MBD Quality Issues

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MBD Quality Issues

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Detail

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Lacking Corner Radii

Lacking Fillet Radii

OEM MBD Detail This cannot be Manufactured without a CNC Programmer adjusting the tool-path.

MBD Quality Issues

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Page 20: OEM Design Definition Issues - JTEG...3 of 24 Misinterpretation of the Blueprint 3D Model of Structural Former – Translated from 2D Blueprint NAVAIR Public Release SPR-2014-341 Obstacles

Correct Corner Radii

Correct Fillet Radii

MBD Quality Issues

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Manufacturing Model Management System (3MS)

Original blueprint Created from Model Interrogation

Check 1: Ensure Model is True to Blueprint

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Presenter
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The evolution of the process: Reproduce the Blueprints The modeler would reproduce a copy of the blueprints by taking measurements directly from the model. (Click for next slide)
Page 22: OEM Design Definition Issues - JTEG...3 of 24 Misinterpretation of the Blueprint 3D Model of Structural Former – Translated from 2D Blueprint NAVAIR Public Release SPR-2014-341 Obstacles

Manufacturing Model Management System (3MS)

Check 2: Scan Aircraft Sample and Compare to Model

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Neg Nom Pos Total Pct In Tolerance: 6354 70 6834 13258 41.86 Out of Tolerance: 8258 10154 18412 58.14 Failed Points: Total Points: 14612 70 16988 31670 100.00

DX DY DZ 3D Maximum Deviation: 0.2080 0.1840 0.3230 0.1050 Minimum Deviation: -0.0900 -0.0870 -0.2790 -0.4120 Deviation Range: 0.2980 0.2710 0.6020 0.5170 Average Deviation: 0.0000 0.0000 0.0000 0.0050 RMS Deviation: 0.0080 0.0090 0.0240 0.0270 Standard

Deviation: 0.0080 0.0090 0.0240 0.0260

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Questions?

ISSC Engineering Team, FRCSW Code 43353 Presented 28 April 2014 Rick Mendoza

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FRCSW 2D-3D Translation Control Documents FRCSWINST 4790.4 FRCSWINST 13600.2

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Presenter
Presentation Notes
Introduction: Hello my name is _________ of the Advanced Design Team at NADEP North Island. A little background into what we, the Advanced Design Team does for the Depot. The Depot mission statement is, “…to provide top quality products and services at the best value in the fastest time.” (The Advanced Design Team provides engineering support to the Depot by providing repair design solutions for complex repair needs.) The title of the presentations…Why is it important to overcome the pitfalls of 2-D blueprints? Next Slide