aeronet 2 - workshop “measurement technology” - cluster lect vienne 19/20 sept. 2001 - technical...
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AERONET 2 - workshop “Measurement Technology” - cluster LECT Vienne 19/20 Sept. 2001 - Technical Univ. O. Penanhoat - Snecma
Page 1
ENSMA - Optical measurements / LES-4-LPP « ORACLES rig »
Digitization
Long exposure time40 10-3 sSymmetrical shape
Short exposure time (2 10-3 s)Symmetrical shape
LIF on OHvery short exposuretime : (100 10-9 s)
Pulsating behavior
AERONET 2 - workshop “Measurement Technology” - cluster LECT Vienne 19/20 Sept. 2001 - Technical Univ. O. Penanhoat - Snecma
Page 2
QinetiQ - Fuel Injector Measurements / LowNox III
Measurement techniques and technology demonstrated:
• Internal gas species, smoke and temperature profile mapping
• Combustor wall heat flux and smoke measurements
• Combustion instability detection using high frequency response transducers
• Enhanced convective cooling tiles on combustor walls provided effective wall cooling
ASC combustor
AERONET 2 - workshop “Measurement Technology” - cluster LECT Vienne 19/20 Sept. 2001 - Technical Univ. O. Penanhoat - Snecma
Page 3
High Pressure Fuel Injector Test Rig
Main features:
• 16 bar operating pressure
• Mean air flow velocity >100m/s
• Steady state operation
• Liquid can be kerosene or water
•Can study swirling and non-swirling flows
• Support high speed photography, laser light sheet and PDA techniques
Air in
Settling chamber
Fuelinjector
Workingsection with
optical windows
Exhaustchamber
Airmeter
QinetiQ - Fuel Injector Measurements / LowNox III
AERONET 2 - workshop “Measurement Technology” - cluster LECT Vienne 19/20 Sept. 2001 - Technical Univ. O. Penanhoat - Snecma
Page 4
QinetiQ - Fuel Injector Measurements / LowNox III
PDA instrument and atomiser rig
0
20
40
60
80
100
120
-40 -30 -20 -10 0 10 20 30 40
X Position (mm)
Sa
ute
r M
ea
n D
iam
ete
r (
mm
)
Idle
Take off
Climb out
Cruise
Descent
Approach
-40
-20
0
20
40
60
80
100
120
-40 -30 -20 -10 0 10 20 30 40
X Position (mm)
U V
elo
city (
m/s
)
Idle
Take off
Climb out
Cruise
Descent
Approach
Generic fuel injector study in LOWNOXIII Programme
Laser light sheet flow
visualisation
Axial velocity of jet
Sauter mean diameter of
droplets
AERONET 2 - workshop “Measurement Technology” - cluster LECT Vienne 19/20 Sept. 2001 - Technical Univ. O. Penanhoat - Snecma
Page 5
piezoelectricceramic
Vd
30µm < Dd < 400µm
2 < C0 = Sd / Dd < 7
Meteringghole
0
Liquid
Seal ringtorique
+-
Electricenergizer
~
Thermocouple
Onera - PDA on a stream of monosized droplets / LowNox III
Combustion chamber
« Parametric Study of Autoignition »
AERONET 2 - workshop “Measurement Technology” - cluster LECT Vienne 19/20 Sept. 2001 - Technical Univ. O. Penanhoat - Snecma
Page 6
P=5 bar T=300K
0.3
0.4
0.5
0.6
0.7
0.8
0.9
1.0
0 0.5 1 1.5
Normalized droplets lifetime t/D02 (s/mm2)
(D10
/ D
0 )2
5 bar
10 bar
15 bar
20 bar
Série5
Linéaire(Série5)Slope -K
FLAME LENGTH VERSUS PRESSURE( Tair = 300 K ; Vair = 0.175 m/s )
FL (mm) = 430. P (bar) -0.67
R2 = 0.9957
0
20
40
60
80
100
120
140
160
0 5 10 15 20 25
Pressure (bar)
Fla
me
Len
gth
(m
m)
Onera - PDA on a stream of monosized droplets / LowNox III « Parametric Study of Autoignition »
AERONET 2 - workshop “Measurement Technology” - cluster LECT Vienne 19/20 Sept. 2001 - Technical Univ. O. Penanhoat - Snecma
Page 7
Onera - Optical analysis of premixed injection systems / LowNox III « Autoignition & Flashback»
Performed : PDA, LDV, photoelectric cells
AERONET 2 - workshop “Measurement Technology” - cluster LECT Vienne 19/20 Sept. 2001 - Technical Univ. O. Penanhoat - Snecma
Page 8
ITS Karlsruhe - IR extinction for fuel spray experiments / LowNox III
Development of a measurement technique • design of optical setup• development of a tomographic deconvolution algorithm for circular cross-sections
deconvolution
optical density vapour concentration profile
y r
AERONET 2 - workshop “Measurement Technology” - cluster LECT Vienne 19/20 Sept. 2001 - Technical Univ. O. Penanhoat - Snecma
Page 9
ITS Karlsruhe - IR extinction for fuel spray experiments / LowNox III
local concentrations of gaseous kerosene in a premix-duct :• influence of temperature on fuel evaporation• Influence of fuel type on local air fuel ratio