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Corporate Research Centre Germany Ottobrunn. Total Revenues: 34 M€ Fixed Assets: 38 M€ (orig. costs) Office Space: 2.800 m² Laboratories: 8.200 m² Employees: ~260 (permanent, temporary, graduate and thesis students). 2 0 0 1. Surface and Chemical - PowerPoint PPT Presentation
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Page 1 01.07.03, LG-SC, Werner Zimmermann
Thermal Analysis of High Temperature Materials- for Aerospace Applications -
2 0
0 1
Total Revenues: 34 M€Fixed Assets: 38 M€ (orig. costs)
Office Space: 2.800 m²
Laboratories: 8.200 m²
Employees: ~260 (permanent, temporary, graduate and thesis students)
Corporate Research Centre GermanyCorporate Research Centre GermanyOttobrunnOttobrunn
Corporate Research Centre GermanyCorporate Research Centre GermanyOttobrunnOttobrunn
Page 2 01.07.03, LG-SC, Werner Zimmermann
Thermal Analysis of High Temperature Materials- for Aerospace Applications -
LG-SO/Dr.Schnaut
Topography (AFM)Tribological PropertiesThermal/IR BehaviourElectrical Properties
Metallic/Ceramic/OrganicCoatingsStructured SurfacesMech./Thermal Treatment
Chemical/ElectrochemicalPVD, PACVD andPlasma ProcessesThermal Spraying
Process IntegrationEnvironmental ImpactCost EvaluationSupplementary Methods
Coating Characterizationand Assessment Process Evaluation
and External Contacts
New Processes andProcess Development
Close
26
141
256 nm
0 5.05 10.1 µm
28
164.5
301 nm
0 5.05 10.1 µm
35
148
261 nm
0 5.05 10.1 µm
OTN12/9
Surface and Chemical Engineering
Surface and Chemical Engineering
New Coatings andSurface Modifications
Page 3 01.07.03, LG-SC, Werner Zimmermann
Thermal Analysis of High Temperature Materials- for Aerospace Applications -
Motivation:
Materials for re-entry vehicles
rocket engines
turbines
supersonic systems
.................
Page 4 01.07.03, LG-SC, Werner Zimmermann
Thermal Analysis of High Temperature Materials- for Aerospace Applications -
Collaborationwith internal and external
partners
Microwave Signature Analysis
Measurement Activities:Absorptivity
•Transmissivity•Reflectivity•Magnetic and•Dielectric Loss Factors•Electric Conductivity•Free and Guided Wave
Propagation
Thermal Management & ControlMeasurement Activities
• Emittance• Absorbance• Transmittance• Thermal
transport:-
Conduction-
Radiation-
Convection
Material-, System- and Process Development
Customerneeds
Dept.:Surface and Chemical Engineering, Signature Analysis
Page 5 01.07.03, LG-SC, Werner Zimmermann
Thermal Analysis of High Temperature Materials- for Aerospace Applications -
Research for new Solutions:High temperature structure materials
high strength at high temperature low cost low weight
High Temperature shielding materials &High Temperature thermal control
low thermal conductancelow emittance
high thermal conductancehigh emittance
High temperature Coatings
oxidation resistant
chemical compatibility
diffusion barrier
high/low emittance
...........
Page 6 01.07.03, LG-SC, Werner Zimmermann
Thermal Analysis of High Temperature Materials- for Aerospace Applications -
Thermal material properties (Focus):
• thermal transport mechanisms, heat capacity
• thermo optical properties, spectral absorption, transmittance,
reflectance
• high temperature chemical properties oxidation resistance
chemical compatibility
Page 7 01.07.03, LG-SC, Werner Zimmermann
Thermal Analysis of High Temperature Materials- for Aerospace Applications -
Improved knowledge of material properties asa function of temperature needed:
Thermal transport mechanismsthermal conductance
Heat capacity
IR-optical properties (spectral emissivity,...
as a function of temperatureBecause Materials will be treated close to their limitations
Page 8 01.07.03, LG-SC, Werner Zimmermann
Thermal Analysis of High Temperature Materials- for Aerospace Applications -
High Temperature Functional Materials for
Thermal Isolation
low thermal conductanceradiation shielding
Cooling by radiationby mass transportby heat conduction
Oxidation resistance
structures with high mechanical strength
Page 9 01.07.03, LG-SC, Werner Zimmermann
Thermal Analysis of High Temperature Materials- for Aerospace Applications -
Measurement Techniques at CRC/LG:
• Spectral emissivity measurements using an FTIR
• Thermal conductance
• Heat capacity
• Thermo Graphimetrical Analysislight pipe
sample
inductor
Page 10 01.07.03, LG-SC, Werner Zimmermann
Thermal Analysis of High Temperature Materials- for Aerospace Applications -
Spectral Radiation of a Black Body at 800 °C up to 1550°C
radi
atio
n in
tens
ity
7800.0 7000 6000 5000 4000 3000 2000 1500 1000 370.00.00
0.2
0.4
0.6
0.8
1.0
1.2
1.4
1.6
1.8
2.0
2.2
2.4
2.6
2.8
3.0
3.2
3.36
cm-1
wave number
1550 °C
Spectral Radiation Measurements
Page 11 01.07.03, LG-SC, Werner Zimmermann
Thermal Analysis of High Temperature Materials- for Aerospace Applications -
7800.0 7000 6000 5000 4000 3000 2000 1500 1000 370.0
-0.003
0.05
0.10
0.15
0.20
0.25
0.30
0.35
0.40
0.45
0.50
0.55
0.60
0.637
cm-1
Egy
7800.0 7000 6000 5000 4000 3000 2000 1500 1000 370.0
-0.003
0.05
0.10
0.15
0.20
0.25
0.30
0.35
0.40
0.45
0.50
0.55
0.60
0.637
cm-1
Egy
Rad
iatio
n in
tens
ity
Normal spectral Intensity of PtIr30 at 800 °C up to 1500 °C, steps of 50 °Cwave number
1500 °C
Spectral Radiation Measurements
Page 12 01.07.03, LG-SC, Werner Zimmermann
Thermal Analysis of High Temperature Materials- for Aerospace Applications -
Normal Spectral Emissivity of PtIr30 at 900 °C up to 1450°C
1.28 2.0 4.0 6.0 8.0 10.0 12.0 14.0 15.000.0
10
20
30
40
50
60
70
80
90
100.0
wave length [µm]
Nor
mal
Spe
ctra
l Em
issi
vity
[%]
Calculations of the Spectral Emittance
Page 13 01.07.03, LG-SC, Werner Zimmermann
Thermal Analysis of High Temperature Materials- for Aerospace Applications -
Induction Heating
Pyrometer
PID-Temperature-adjust
PC
Stepper motorcontroller(OVIS)
Stub Tuner
micro wave-generator
AMRData-Logger
RS232/RS422
Detector
Detectors
Stepper MotorsTemp
A/DA/DA/DRS232
D/A
RS 232
ADAM
ACCUFIBER
Sampleroom
Pyrometer (Raytek od. Accufiber)
(Maurer)
Sensor
Control UnitInductionHeating andMicro waveGenerator
D/A
P818
12
3
4
6
7 8
9 1011
Inductor
Block / Functional Diagram of the Measurement System withInduction Heating (6kW) and Micro Wave Heating (2kW)
to FTIR
Measurement System
Page 14 01.07.03, LG-SC, Werner Zimmermann
Thermal Analysis of High Temperature Materials- for Aerospace Applications -
High Temperature Spectral Emissivity Measurements
Inductive andmicrowaveheating furnacewith FTIR-spectrum-analyser,range: 0,6-25 µm
Measurement System
Page 15 01.07.03, LG-SC, Werner Zimmermann
Thermal Analysis of High Temperature Materials- for Aerospace Applications -
TGA von MoSi2, Pt, Rh und PtRh30 up to 1600 °C in Standard-Atmosphere
Thermo Graphimetrical Analysis
Page 16 01.07.03, LG-SC, Werner Zimmermann
Thermal Analysis of High Temperature Materials- for Aerospace Applications -
pyrometer
data-logger
°K,mA,V,
IR-Camera3-5 M
video-/IR-Camera
VIS<1,0µm
Laptop
intra-/internet
serialinterfaces
frame-grabber
telemetrictransceiver
telemetrictransceiver
videotransceiver
videotransceiver
455MHz
2,4GHz
Thermal Management & ControlMoveable measurement System
intra-/Internet
LAN
othersensors
Page 17 01.07.03, LG-SC, Werner Zimmermann
Thermal Analysis of High Temperature Materials- for Aerospace Applications -
Thermal Management & ControlFlow and Temperature Measurements in Motor Compartments
Position of flow sensors and thermal sensors
0.00.1
0.2
1.7
6
Strömungsgeschwindigkeit unter wechselnden Einsatzbedingungen, 26.10.01, 7h55-10h27
0
0,5
1
1,5
2
2,5
3
3,5
4
4,5
Uhrzeit
Str
öm
un
gsg
esc
hw
ing
dig
ke
it [
m/s
]
0 -
1 -
2 -
3 -
4 -
1. Testfahrt 2. TestfahrtRast RastWerk WerkWerk
Page 18 01.07.03, LG-SC, Werner Zimmermann
Thermal Analysis of High Temperature Materials- for Aerospace Applications -
Bionic Solutions for Temperature Control
Swakobmund Beetle
Page 19 01.07.03, LG-SC, Werner Zimmermann
Thermal Analysis of High Temperature Materials- for Aerospace Applications -
Bionic Solutions for Temperature Control
0 ,67 0 ,8 1 ,0 1 ,2 1 ,4 1 ,6 1 ,8 2 ,0 2 ,2 2 ,4 2 ,6 2 ,8 3 ,0 3 ,2 3 ,4 3 ,70
0 ,8
2
3
4
5
6
7
8
9
10
11
12,0
µm
%R
Vergleich der Reflexionsgrade von Lacken und des Swakopmund-K äfers
Laquer Coatings
Swakopmund Beetle
Normal Spectral Reflectivity of the Swakobmund Beetle versus Laquer Coatings
Page 20 01.07.03, LG-SC, Werner Zimmermann
Thermal Analysis of High Temperature Materials- for Aerospace Applications -
Bionic Solutions for Temperature Control
Spectral reflectanceMeasurement of theAbdomen
Page 21 01.07.03, LG-SC, Werner Zimmermann
Thermal Analysis of High Temperature Materials- for Aerospace Applications -
Bionic Solutions for Temperature Control
EDX of the Abdomen of the Swakopmund-Beetle
Page 22 01.07.03, LG-SC, Werner Zimmermann
Thermal Analysis of High Temperature Materials- for Aerospace Applications -
Expectations from Evitherm:
National Laboratories and research centres closer to industry
Validated improved measurement techniques
Validated Reference Materials needed
Catalogues with extended description of material properties
Discussion Forum
Online testing of materials, controlled bythe customer via Internet, assisted by the staff ?
Page 23 01.07.03, LG-SC, Werner Zimmermann
Thermal Analysis of High Temperature Materials- for Aerospace Applications -
Great Thanks to the Evitherm Committee and toDr. Joachim Fischer for the Invitationand to Dr.Neuer who gave me the start up support to work on this field of material sciences.
W. ZimmermannEADS, CRC/LG-DC81663 München/OttobrunnGermany