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AERODAYS 2011
LTCC: A packaging technology p g g gysuitable for high density integration and high temperature applicationsg p pp
AERODAYS 2011
1
AERODAYS 2011Madrid, March the 31st 2011
CREAM Project AAT.2008.4.2.4-234119
Conor Slater, EPFLPaul Vassy, Sagem
AGENDAAGENDA
INTRODUCTION: CREAM context and objectivesP l V S CREAM C di tPaul Vassy, Sagem, CREAM Coordinator
LTCC Packaging technology presentationg g gy pConor Slater, EPFL, PhD
2AERODAYS 2011Madrid, March the 31st 2011 CREAM Project AAT.2008.4.2.4-234119
INTRODUCTIONINTRODUCTION
CREAM CONTEXT AND OBJECTIVES
Compact and Reliable Electronics for Actuators and Motorspwww.creamproject.eu
AcknowledgementThe research leading to these results has received funding from the European Union Seventh Framework Programme (FP7/2007-2013)
3AERODAYS 2011Madrid, March the 31st 2011 CREAM Project AAT.2008.4.2.4-234119
European Union Seventh Framework Programme (FP7/2007 2013) under grant agreement AAT.2008.4.2.4-234119 CREAM"
INTRODUCTION
CREAM: FP7 Program with 14 PartnersSept 2009 – Sept 2012
4AERODAYS 2011Madrid, March the 31st 2011 CREAM Project AAT.2008.4.2.4-234119
INTRODUCTION
CONTEXT
ACARE 2020: Environment, lifecycle cost More Electrical Aircraft Replace hydraulics actuation by electrical actuation Several subsystems concerned: Flight control systems landing gear Several subsystems concerned: Flight control systems, landing gear
systems, fuel pumps for motor regulation, cabin pressurisation… Several architectures under study on research programs
• Power buses (HVDC or AC)• Power buses (HVDC or AC)• Control buses (control loops management)• Energy regeneration issues• Share of the control loops between equipments• Electronics in cabinets shared between several actuators / integrated EMA in harsh
environment
CREAM bj ti i t lid t t h l i bli th i t ti fCREAM objective is to validate technologies enabling the integration of a compact, reliable “all in one” actuator in harsh environment. The
demonstration is performed on a primary flight control actuator
5AERODAYS 2011Madrid, March the 31st 2011 CREAM Project AAT.2008.4.2.4-234119
INTRODUCTIONInnovative Actuator Mechanism with high integration of motor, bearings and roller screw developed by Sagem
Control electronics Power drive electronics
Control electronic technologies :• high temp substrate (LTCC,HTCC)• LT process nanoscale joining• high temp protections• SOI and asic integration
2.3
• SOI and asic integration
Power electronic technologies :• high temp substrate• LT process nanoscale joining• high temp integrated curent sensor
2.2
St t f th t G ti 2• Sic Power part State of the art Generation 2 Aileron actuator (2010)
Weight /vol : 12.5 kg/ 6 l , Reliability 40000h, Temp 85°C
TRL6 Fli ht A320 fl i t t b h
Compact control and
High temperature Reliability evaluation program research
2.4
TRL6: Flight proven on A320 flying test bench
3
Motor mass & volume reduction and temp increase
• higher density magnetic material• Motor power optimization• New motor concept (Variable reluctance)
Electronic motor and mechanism integration conceptFuture CREAM EMA technology
Power drive electronic MCPM
2.1
6AERODAYS 2011Madrid, March the 31st 2011 CREAM Project AAT.2008.4.2.4-234119
Electronic, motor and mechanism integration conceptfuture aileron actuator Target weight/vol : 9 kg/ 4 l , reliability >50000h, Temp > 150°C
LTCC Technologygy Description of Control Module Description of Control Module Properties of LTCC LTCC manufacturing Process Design Rules Design Rules Packaging Technologies Conclusion
Conor Slater, EPFL
7AERODAYS 2011Madrid, March the 31st 2011 CREAM Project AAT.2008.4.2.4-234119
PhD
LTCC Technology
Description of Control Module
Control Module to Survive in Ambient Conditions (-65°C to 200°C)• Operational Lifetime of 100,000 hours
Substrate will need to mount a high number of components (500+) but the total power dissipation will be less than 10W
• Packaging technology will be required for:
● Passive components
● Mounting Silicon dies● Physical attachment● Thermal conduction● Electrical InterconnectsElectrical Interconnects
● Mounting Substrate to Baseplate
8AERODAYS 2011Madrid, March the 31st 2011 CREAM Project AAT.2008.4.2.4-234119
LTCC Technology
Properties of LTCC
Good electrical characteristics• Low Dielectric Loss at high frequency
and high breakdown voltage
Good Thermal stability (450°C+)
Multilayer Technology• Possible to integrate Resistors,
Capacitors and Inductors
3-Dimensional Structures• Cavities and Channels, by means of unfilled cuts and sacrificial layers
Compatible with “Classic” Thick Film Technology (firing temperature <900°C)• Allows use of Pt, Au, Ag, Pd, Metallisations and Thick Film Resistors
9AERODAYS 2011Madrid, March the 31st 2011 CREAM Project AAT.2008.4.2.4-234119
Allows use of Pt, Au, Ag, Pd, Metallisations and Thick Film Resistors
LTCC Technology
LTCC Manufacturing Process
10AERODAYS 2011Madrid, March the 31st 2011 CREAM Project AAT.2008.4.2.4-234119
LTCC Technology
Design Rules
Variety of Thicknesses (…, 50 µm, 114 µm, 254 µm, …)
Dimensions of Thick Film Conductors and Resistors defined by Screen Dimensions of Thick Film Conductors and Resistors defined by Screen Printing Process
• Track width 200 µm
• Clearance 200 to 250 µm● Depending whether tracks are printed
simultaneously or in separate stepsy p p
• Via Diameter 300 µm
• Minimum Resistor Size 500x800 µmMinimum Resistor Size 500x800 µm
11AERODAYS 2011Madrid, March the 31st 2011 CREAM Project AAT.2008.4.2.4-234119
LTCC Technology
Integrated Passives
LTCC allows passive components such as Resistors to be integrated into the substrate.
• At high temperatures the values of the resistors drift due diffusion of contact material by oxidation
● A barrier layer on the contacts can prevent diffusion allowing stability at 200°C1
● Embedding the resistors between LTCC layers● Embedding the resistors between LTCC layers or under an overglaze protects from oxidation and improves the stability of the Resistor2
● Thin film resistors have greater stability at high
[1] R Johannessen, F Oldervoll, F Strisland, and P Ohlckers. Performance of thin and thick film resistors exposed to high temperature and high pressure (200°C @ 1000 bar). In HITEN 2007, Oxford, UK, pages 678–682, 2007.[2] A Dziedzic L Golonka M Hrovat J Kita M Kosec and D Belavi Some remarks about relations between processing conditions and
temperature but are more expensive
12AERODAYS 2011Madrid, March the 31st 2011 CREAM Project AAT.2008.4.2.4-234119
[2] A Dziedzic, L Golonka, M Hrovat, J Kita, M Kosec, and D Belavi. Some remarks about relations between processing conditions and microstructural, electrical as well as stability properties of ltcc resistors. In European Microelectronics and Packaging Symposium, Prague, Czech Republic, 2004.
LTCC Technology
Compatible Component Attach Methods (1)
Solders• CREAM > High Lead Solder (225 – 300°C)• Variety of Metallisations can be used with LTCC
Transient Liquid Phase (Diffusion Soldering)• Can be used with LTCC due to liquid phase
E hibit l lif ti t hi h t t 3• Exhibits long lifetime at high temperatures3
Silver Filled GlassDi tl tibl ith LTCC b t t• Directly compatible with LTCC substrate
• High Thermal Conductivity and strength4
[3] H.A. Mustain, W.D. Brown, and S.S. Ang. Transient liquid phase die attach for high-temperature silicon carbide power devices. Components
13AERODAYS 2011Madrid, March the 31st 2011 CREAM Project AAT.2008.4.2.4-234119
g gand Packaging Technologies, IEEE Transactions on DOI - 10.1109/TCAPT.2010.2046901, 33(3):563–570, 2010.[4] R. Kisiel and Z. Szczepanski. Die-attachment solutions for sic power devices. Microelectronics Reliability, 49(6):627–629, 2009.
LTCC Technology
Compatible Component Attach Methods (2)
Polymers
• Polymers such as epoxies and silicones adhere well to LTCC
● Silicones and Epoxies stable in the 200-250°C range
● Polymers allow flexibility in CTE mismatch between the substrate and the baseplatey y p
14AERODAYS 2011Madrid, March the 31st 2011 CREAM Project AAT.2008.4.2.4-234119
LTCC Technology
Wirebonds
Gold wire bonds work well on LTCC due to matching Metallisation
Aluminium wires more common Aluminium wires more common• Aluminium metallisations on LTCC problematic due to oxidation during firing
Aluminium to Silver results in Aluminium to Silver results in oxidation of intermetallic5
A li ti f Thi fil b i Application of Thin film barrier layer shows good performance6
[5] R. Kisiel and M. Guziewicz. High temperature applications of al wire connection to sic structures. In 31st International Spring Seminar on Electronics Technology, pages 264–268–, Warsaw Univ Technol, Inst Microelect & Optoelect, Warsaw, Poland, 2008.
15AERODAYS 2011Madrid, March the 31st 2011 CREAM Project AAT.2008.4.2.4-234119
gy p g p[6] R. Johannessen, F. Oldervoll, and F. Strisland. High temperature reliability of aluminium wire-bonds to thin film, thick film and low temperature co-fired ceramic (ltcc) substrate metallization. Microelectronics Reliability, 48(10):1711–1719, 2008.
LTCC Technology
Conclusions
LTCC • Stable at temperature range for CREAM-EMA• High density of interconnects and routing possible• Integrated resistors show good stability at high temperature
Extensive range of packaging technologies compatible with LTCC• Allowing a variety of component configurations to be packaged
LTCC’s suitability for the control module is based on its flexibility• Easily structurable• Wide range of compatible materials
16AERODAYS 2011Madrid, March the 31st 2011 CREAM Project AAT.2008.4.2.4-234119
INTRODUCTION
THANK YOU FOR YOUR ATTENTION
QUESTIONSQUESTIONS
17AERODAYS 2011Madrid, March the 31st 2011 CREAM Project AAT.2008.4.2.4-234119