Standard Airbus Sisteme Axa

3D-DMU A340-500/-600 12.11.
22
Presented by
Rolf Becker
Agreement for 3D-DMU-A3456
R. Becker H/esgl/esgl4/A3456DMU/Struktur Bibel, Index A

• Confirmation of ATA53 manual
Field Department Date Name Signature
Methods EODKG Hubert Moenter
ATA53 Responsible Rolf Becker
Projectmanagement P3 Stefan Siegler

© AIRBUS DEUTSCHLAND GmbH. Alle Rechte vorbehalten. Vertrauliches und geschütztes Dokument.
• History
 Release only for Project 3D_DMU_A3456 at ……
R. Becker H/esgl/esgl4/A3456DMU/Struktur Bibel, Index A 12.11.22 Seite 2

3D-Models to be created (Level of Detail: 100%)
• Stringers
• Frames
• Frame couplings
• Cross beams
• Longitudinal beams
• Seat rails
• Screwed brackets
• Brackets
• Y- support
• MVK beam
• Door upperdeck (as SPL)

• Door beam (as SPL)
• Floor panels
• Hardpoints

Following parts do not have to be created as 3D-model:
• Clips (with exceptions)

• Skins
• Skin Doublers
• Shear webs (with exceptions)
• Cargo door
• Stringer couplings (with exceptions)
• Wedge
• Crackstopper
• Shim
• Sealant
• Reinforcment
• Doubler
• Tape
• Adhesive

• Layer
 According to the Method Guidline
• Axis Model Method

 According to the AMXXXX-> Creation of CATIA V5 Parts based on drawings
 Brackets for tubes
 Y – support
 MVK beam
 Crackstopper
 Modelling Rules
 AM2118 - SKETCHER
 AM2263 - Sheet Metal Part Modelling for CATIA V5
• Naming & Numbering

 According to the Method Guidline
AM2119 - PART DESIGN
 AM2259 - 3D Modelling Rules for CATIA V5
 AM2252 - CATIA V5 MULTI MODEL LINK
 AM2117 - WIREFRAME & SURFACES
 According to the method guidline
• Holes from ATA 539 see page 8

• Every Sheet metal Part has to be designed with SMD.
Here some examples:

• If the SMD part creation is not possible, these parts has to
be designed with “Part Design” or with “Generative Shape
Design”.
• Every Catia V5 Sheet metal Part must be designed
according to the AM2263 (Sheet Metal Part Modelling for
CATIA V5)
• It`s not allowed to use any Part Design Features, like holes
and pads, in SMD- Parts.

. Holes belonging to ATA 539 (srew holes, RIS) will be
represented as CPPs only.
To see the finished part in Catia V5 you have to load the
structure part itself (ATA 532/534) and all relevant CPPs
Siehe auch in AM xxxxx

zero appears at the beginning of a section.
Stringer X-vektor along the intersection curve stringer surface –inner skin contrary tangency to flieght
direction of the first frame level before stringer plane.
Z-vektor along the intersection line stringer plane –frame level
Y-vektor appears tangential to the intersection curve frame level-inner skin surface
Z X
X
Z
Y
X
X=0
Frame surface
exeption
li ng
em
as s
and
ling
m ode
id
val
FLB like P26(plane) only for modeling No t
and assemling
P26
zero point
Stringer surface

Crossbeam Y
Z
for C54-C80
The zero of a crossbeam appears 1.6mm

In front of the beam in the intersection point
of the frame system and FLB.
For C18-C38

Skin
Z
Z
flight direction
X
Y
zero appears in section zero (0,0,0).

X-vector: intersection AD / FD and contrary to flight direction
Z
flight direction
AD (Y=0)
Y
X P P‘
FD-line (Z=0)
X-Station

Frame X-Station
frame level
AD- line
zero near by X=0, Y=0, Z=0

X-vector contrary to flight direction.
Z
Z-vector upwards AD-loft-frame level.
Y-vector results
Z=0
X
Inner frame strap shows to

Sec.13-14 contrary to flight direction.
Z
Flight directon Y
Sec 16-19 in flight direction
Blatt 2 X

Z
Frame coupling X
Converted parts should be created by ASL tool

(Aerospace Sheetmetal)
Holes should only be created by ‚cutout‘ tool.
zero is intersection point stringer surface –frame profile

X- vector contrary (tangency) to flight direction and on stringer line
Z-vector along the intersection line stringer plane –frame level Inner frame strap shows to
Y –vector results. Sec.13-14 contrary to flight
y direction.
z Sec 16-19 in flight direction.
Internal loft line Frame level

External loft line / frame level
Stringerl line
Stringer surface
Z
X
X
X=0
External loft line

Stringer coupling
stringer linie
P‘
Stringer surface
XYZ Zero appears at bottom corner of the profile
X-vector shows contrary to direction of flight

(tangency) and parallel to stringer linie
Z-vector. Shows to outsite
Y-vector results.
Z
Z
Zero: stringer coupling
Z X
X
X
X=0
Y

Milling bracket
Zero point of similar parts must be ever at the same postion
z (e.g. on hole or at the border).
x
Zerol appears in a hole or at the border.
Z-vector shows upwards in direction AD loft.frame level
Y-vector results.
Z Y

Y-support
The zero is to position

at a wisely place near by AD line.
AD - linie
zero is positioned at the plain side.
y
z
X-vector contrary to flight direction
Z-vector upwards in direction AD loft-frame level.
Y-vector results.
x

Brackets
Converted parts should be created by ASL tool
Holes should only be created by ‚cutout‘ tool.
Zero point of similar parts (L/U-profile) must ever be at the same postion
Z
Z Z
Y
X
X
L-section extruded parts should be created with‘part design‘ tool.
The zero is situated at the border.

Seatrail
Help for installation
from
Y X
Z
FLB
X
Zero is situated in front of the part.

X-vektor at intersection border –floor system contrary to flight direction.
Z-vektor at intersection FLB and 3mm from top side.
Y-vektor in the middle of the profile and the direction results.

Clip
Clips and all converted parts should be modelled by the ASL tool
zero point =
The zero is located at the intersection frame level-stringer plane.

The system lines are applied to split the surface.

Brackets for tubes
Zero is to position at the back side of the part .
Converted parts should be modelled with (Aerospace Sheetmetal) tool.
Holes should only be created by ‚cutout‘tool.
Z
A2-A2
Y
Zero appears at the plain side

Crackstopper
Crackstopper are designed as a 2d plane part and installed as a 3d model.
Zero should be located at the part.
Y
The strap is created by 3d

mastergometrie.

3D-DMU A340-500/-600
Skin, Panel ( Hautblech)
Y Y
A
Don`t model this tooling lug
Z
X
Mögliche Achsenkreuze,
abhängig immer von
Loflinie
A A
X X

MVK- beam
MVK- beam and Y-support assembled
The zero is to postion at a

wisely place near by AD line.

Z-vector upwards in direction AD loft-frame level.
Y-vector results.

Floor - panel
Z
Y X Y -450
Floor- panels are

designed as SPL- Parts
(no corners)
flight direction
Missing dimension have
been taking over of
assembly (CCD).
Y -923
A A Z
SPL- Part
A-A A-A
Z SPL- Part

STA- Beschlag
A-A
y
Y
A
X Z
A
A Z
Z A
y
X

ATA 53 Montage Bibel
Page 27: Rumpf Section and Halfsection

Page 28: Primär Schalen
Page 29: Fussbodengerüst
Page 30: Fußbodenplatten
Page 31: MVK Träger
Page 32: Kleine Assys (Halter +Clip)
Page 33: Optionshalter bei Sec.13 und14 / Sec. 16 und 18
Page 99: Deu Halter (in Deckenträger)
Page 99: Halter Schale
Page 99: Geschraubte Halter

Page 99: Halter Sec. Montage G539-70020-000-0592
Page 99: Halter Fussbodengerüst
Page 99: Halter Querträger
Page 99: Halter Trennstelle
Page 99: ISO Kobihalter F258 70016/ 70017/ 71016/ 71017
Page 99: Rumpf Sec. 13-14 / 16- 18

Section and half Section
Z=0
Z=0 X
Y=0

Schale
Y=0 X
Z=0
Y=0

•Fusssbodengerüst

Floor - panel
Valid for Sec.16-18 Valid for Sec.13-14
Z Z
X X
Y=0 X

Z
X
Am C20 wird montiert

Sec16 and 17, Einbauspant C55

Sec18 Einbauspant C72
Bohrungen (CPP-Parts siehe
Halter Baugrp.) für den
Einbau nutzen

Smal Assemblys
•Wie Halter

Option brackets for Sec. 13-14 Option brackets for Sec. 16-18
Z=0 X
Z=0 X
X-Wert (option)
Options Assemblys werden von C18 bzw. C54 aus positioniert und bekommen
die entsprechenden X, Y, Z Angaben.
Z=0
Y=0

Insulation brackets
Valid for Sec. 13-14, upper deck and lower deck
Z=0 Z=0
X
FD Y=0
Valid for Sec. 16-18 , upper deck and lower deck
Z=0
X

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3D-DMU A340-500/-600 12.11.

Agreement for 3D-DMU-A3456

R. Becker H/esgl/esgl4/A3456DMU/Struktur Bibel, Index A

ATA53 Responsible Rolf Becker

Projectmanagement P3 Stefan Siegler

R. Becker H/esgl/esgl4/A3456DMU/Struktur Bibel, Index A 12.11.22 Seite 2

• Door upperdeck (as SPL)

R. Becker H/esgl/esgl4/A3456DMU/Struktur Bibel, Index A 12.11.22 Seite 3

• Clips (with exceptions)

R. Becker H/esgl/esgl4/A3456DMU/Struktur Bibel, Index A 12.11.22 Seite 4

• Axis Model Method

• Naming & Numbering

R. Becker H/esgl/esgl4/A3456DMU/Struktur Bibel, Index A 12.11.22 Seite 5

R. Becker H/esgl/esgl4/A3456DMU/Struktur Bibel, Index A 12.11.22 Seite 6

R. Becker H/esgl/esgl4/A3456DMU/Struktur Bibel, Index A 12.11.22 Seite 7

Siehe auch in AM xxxxx

R. Becker H/esgl/esgl4/A3456DMU/Struktur Bibel, Index A 12.11.22 Seite 8

R. Becker H/esgl/esgl4/A3456DMU/Struktur Bibel, Index A 12.11.22 Seite 9

The zero of a crossbeam appears 1.6mm

R. Becker H/esgl/esgl4/A3456DMU/Struktur Bibel, Index A 12.11.22 Seite 10

zero appears in section zero (0,0,0).

X-vector: intersection AD / FD and contrary to flight direction

R. Becker H/esgl/esgl4/A3456DMU/Struktur Bibel, Index A 12.11.22 Seite 11

zero near by X=0, Y=0, Z=0

Inner frame strap shows to

R. Becker H/esgl/esgl4/A3456DMU/Struktur Bibel, Index A 12.11.22 Seite 12

Converted parts should be created by ASL tool

zero is intersection point stringer surface –frame profile

Internal loft line Frame level

External loft line

R. Becker H/esgl/esgl4/A3456DMU/Struktur Bibel, Index A 12.11.22 Seite 13

X-vector shows contrary to direction of flight

R. Becker H/esgl/esgl4/A3456DMU/Struktur Bibel, Index A 12.11.22 Seite 14

R. Becker H/esgl/esgl4/A3456DMU/Struktur Bibel, Index A 12.11.22 Seite 15

The zero is to position

R. Becker H/esgl/esgl4/A3456DMU/Struktur Bibel, Index A 12.11.22 Seite 16

R. Becker H/esgl/esgl4/A3456DMU/Struktur Bibel, Index A 12.11.22 Seite 17

Zero is situated in front of the part.

R. Becker H/esgl/esgl4/A3456DMU/Struktur Bibel, Index A 12.11.22 Seite 18

The zero is located at the intersection frame level-stringer plane.

R. Becker H/esgl/esgl4/A3456DMU/Struktur Bibel, Index A 12.11.22 Seite 19

Zero appears at the plain side

R. Becker H/esgl/esgl4/A3456DMU/Struktur Bibel, Index A 12.11.22 Seite 20

The strap is created by 3d

R. Becker H/esgl/esgl4/A3456DMU/Struktur Bibel, Index A 12.11.22 Seite 21

Skin, Panel ( Hautblech)

R. Becker H/esgl/esgl4/A3456DMU/Struktur Bibel, Index A 12.11.22 Seite 22

The zero is to postion at a

X-vector contrary to flight direction.

R. Becker H/esgl/esgl4/A3456DMU/Struktur Bibel, Index A 12.11.22 Seite 23

Floor- panels are

R. Becker H/esgl/esgl4/A3456DMU/Struktur Bibel, Index A 12.11.22 Seite 24

R. Becker H/esgl/esgl4/A3456DMU/Struktur Bibel, Index A 12.11.22 Seite 25

Page 27: Rumpf Section and Halfsection

Page 99: Geschraubte Halter

R. Becker H/esgl/esgl4/A3456DMU/Struktur Bibel, Index A 12.11.22 Seite 26

R. Becker H/esgl/esgl4/A3456DMU/Struktur Bibel, Index A 12.11.22 Seite 27

R. Becker H/esgl/esgl4/A3456DMU/Struktur Bibel, Index A 12.11.22 Seite 28

R. Becker H/esgl/esgl4/A3456DMU/Struktur Bibel, Index A 12.11.22 Seite 29

R. Becker H/esgl/esgl4/A3456DMU/Struktur Bibel, Index A 12.11.22 Seite 30