sirris_am in aviation and aerospace_airbus

15
This document and its content is the property of Astrium [Ltd/SAS/GmbH] and is strictly confidential. It shall not be communicated to any third party without the written consent of Astrium [Ltd/SAS/GmbH]. Christian Désagulier, Materials & Processes Expert An ALM Qualification Logic Proposal for Space Equipments SIRRIS, Liege Science Park, Rue Bois Saint Jean 12, 4102 Seraing 2014, May the 13th Current applications, trends and future developments of metal Additive Manufacturing / 3DPrinting for space and aviation

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Sirris Workshop - Additive manufacturing in aviation and aerospace 13/05/2014

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Page 1: Sirris_am in aviation and aerospace_airbus

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Christian Désagulier, Materials & Processes Expert

An ALM Qualification Logic Proposal for Space Equipments

SIRRIS, Liege Science Park, Rue Bois Saint Jean 12, 4102 Seraing 2014, May the 13th

Current applications, trends and future developments of metal Additive Manufacturing / 3DPrinting for space and aviation

Page 2: Sirris_am in aviation and aerospace_airbus

Confidential

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Introduction : 3 ALM school cases..

Copper foil gilded for DGR telecom reflector antenna

Integral Co-curing for ULR Ku sandwich (1 ply per skin, without adhesive, < 1 kg/m2)

Launchers CFRP composite Tanks

Ti64 brackets EBMed for ULR Ka antenna reflector

Page 3: Sirris_am in aviation and aerospace_airbus

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1st ALM case : Copper foil gilded for DGR antenna

Page 4: Sirris_am in aviation and aerospace_airbus

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- 35 microns Copper foil annealed 1360 x 3500 mm- 0,5 micron gilded- NDI Gold thickness - Sample traveler for adhesion tests

more than 80’s flying since 1995 (i.e. 320 gilded copper foils)

Page 5: Sirris_am in aviation and aerospace_airbus

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2d ALM case : Ultra-Light Reflector Ku antenna

Page 6: Sirris_am in aviation and aerospace_airbus

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- Integral Co-curing : 1 ply per skin, without adhesive, sandwich < 1 kg/m2

- NDI (thermography, US) + curing cycle checking

- Mimic sample traveler (OOP/ Compression tests, micrographs)

100s customized antenna reflectors in flight since 2000..

Page 7: Sirris_am in aviation and aerospace_airbus

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13 May 2014 7

The well known Additive Layer composite Manufacturing machines CFRP based

Filament winding

Tow placement

- Spherical tanks from Ø 0,3 m to 1 m

- Cylindral tanks & structures from Ø 3m up to 5,5m, H up to 12 m

3d ALM case : CFRP Launchers Composite tanks & structures

Page 8: Sirris_am in aviation and aerospace_airbus

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13 May 2014 8

100’s ALM tanks on civil and defence launchers, manufactured since 25 years..

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3d ALM case : Satellite Bi-axial Sun Sensor

Page 10: Sirris_am in aviation and aerospace_airbus

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3d ALM case : Satellite Bi-axial Sun Sensor

Page 11: Sirris_am in aviation and aerospace_airbus

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Sirris, 2014, May the 13h

Telemetry Support (TMTC) + Bi-Axial Sun Sensor (BASS) Ti64 node support- Conventional design for back up need- Quality audit of the manufacturer subcontractor and registration of the qualified EBM process- Manufacturing according to registered process- NDT & traveler samples checking- Mast to CFRP tubes integration with bonding of the knot- Mast to Satellite integration

ATLANTIC BIRD 7, first ALM commercial application in GEO, launched on Tuesday the 27th of September 2011, delivered to the customer on the 23th of October..

3d ALM case : Satellite Bi-axial Sun Sensor

Page 12: Sirris_am in aviation and aerospace_airbus

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ALM - One Technology But Several Processes

Powder Bed Wire feed

Ti64Inconel

Stainless steelsScalmalloy®

Maraging

Electron Beam

LASER

CMTTi64

Stainless steels

INVAR ?

CrCo alloys and High T° alloys

Al-Si-Mg Alloys

HP-Al Alloys(2xxx, 7xxx)

Page 13: Sirris_am in aviation and aerospace_airbus

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General technical status@EADS

General technical status@AIRBUS

AIRBUS

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ASTRIUM Qualification logic

Two possible approaches

Proof load test on each new built part, or on one part per batch

Validation of samples produced with the parts

Traceability

NDI qualification

High level Incoming inspection

“Conventional”The long-term target

“Composite”Interim approach duringALM maturity development

the choice depend on the maturity of processes and considering volume of parts..

Development of a specific qualification logic, in particular on inspection and verification methods, contributing to increase of technical maturity

Impact and sensitivity of process parameters

NDI qualification

Raw material (powder) supply chain qualification

Page 15: Sirris_am in aviation and aerospace_airbus

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