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EMR’13LilleSept. 2013
Summer School EMR’13“Energetic Macroscopic Representation”
«EMR of helicopter electrical power system for its management
in different operating modes»
Dr. Nathalie DEVILLERS, Pr. Marie-Cécile PERA, Dr. Frédéric Gustin
FEMTO-ST, University of Franche-Comté[email protected]
EMR’13, Lille, Sept. 20132
« EMR of helicopter Electrical Power System (EPS)»
Research program - supported by the Direction Générale de l’Armement
(French government defense agency)
- in partnership with : Eurocopter (an EADS company)
Cirtem (expert on power converters)
- Context -
Study of Electrical Power System in a More Electrical Aircraft (helicopter)
Helicopter Electrical Power System = System for electrical production, conversion, distribution and storage aboard the aircraft
Aims : - study a new electrical architecture- evaluate an energy management strategy- develop and test a full-scale prototype
EMR’13, Lille, Sept. 20133
« EMR of helicopter Electrical Power System (EPS)»
- Outline -
1. Helicopter electrical architecture • Classic / more electrical architecture• Aims of more electrical architecture• Different operating modes• EMR : tool for model organization
2. Energetic Macroscopic Representation of an helicopter EPS• Devices : S/G, BAT, SCAP, DC buses• EMR of the whole EPS
3. Maximal Control Structure of an helicopter EPS• Devices : S/G, BAT, SCAP, DC buses• MCS of the whole EPS• Energy management of EPS
4. Simulation of helicopter EPS modelling with Matlab® Simulink
EMR’13LilleSept. 2013
Summer School EMR’13“Energetic Macroscopic Representation”
« Helicopter electrical architecture»
EMR’13, Lille, Sept. 20135
« EMR of helicopter Electrical Power System (EPS)»
- Classic Electrical Power System -
Classic AC architecture as helicopter EPS :
- AC bus : three-phase network
- DC bus connected to AC bus with Transformer Rectifier Unit (TRU)
- Independent starting system
- One energy source per bus (no source in parallel)
- Unidirectional power flows (sources and loads)
G
AC Bus
DC Bus
Load1
=~
Load2
S Gearbox
Engine
Source2
D. Bienaimé, «Modeling and energy management of an electrical power system for aeronautic auxiliary supply », Ph.D. thesis of University of Franche-Comté, Belfort,December 19th 2012.
EMR’13, Lille, Sept. 20136
« EMR of helicopter Electrical Power System (EPS)»
- More Electrical Power System -
More electrical architecture as helicopter EPS :
- Two DC buses connected with a bidirectional chopper
- Starter/Generator system- S/G1 = APU- S/G2 = main S/G
- Generators and Energy Storage Systems (ESS) connected to the DC bus1 with converters
- Bidirectional power flows
S/G1
=~
S/G2
=~
SCAP
==
Source2
DC Bus 1
DC Bus 2
Load1
==
Load2
ACC
==
Gearbox Engine ESS
D. Bienaimé, «Modeling and energy management of an electrical power system for aeronautic auxiliary supply », Ph.D. thesis of University of Franche-Comté, Belfort, December 19th 2012.
J. Asensio-Sauto, M.C. Péra, F. Gustin, N. Devillers, M.L. Grojo, «Scalable modeling approach for assessing helicopter DC electrical power system performances», European Conference on Electrical Power and Applications (EPE), Lille, France, September 2013.
EMR’13, Lille, Sept. 20137
« EMR of helicopter Electrical Power System (EPS)»
- Aims of a more electrical aircraft -
Objectives :
- Reduce the embedded weight
Methods :
- Control of bus voltages through the different sources in all operation modes
- Meet the growing energetic requirements of the aircraft
- Optimize the global energetic efficiency
- Warranty network stability and quality and the energy availability
- Management of the energy flows by balancing the energetic requirements of the loads between the different sources according to their characteristics (energy or power source, Energy Storage System or Starter/Generators, …)
- Reduction of the filters- Addition of Energy Storage
Systems
EMR’13, Lille, Sept. 20138
« EMR of helicopter Electrical Power System (EPS)»
- Energy management in different operating modes -
Starting modes : Degraded operation modes :
EMR’13, Lille, Sept. 20139
« EMR of helicopter Electrical Power System (EPS)»
- EMR : tool for modeling organization -
No source is always connected to the network⇒ No source can set its voltage to the remaining system
⇒ All the sources must be considered as a current source
Vbus1
Vbus1
Vbus1
Vbus1
Vbus1
Vbus1
Ibus_BAT
Ibus_SCAP
Ibus_sm1
Iload1
Ibus_sm2
Idc1
SE
SE
SE
SE
SE
SE
S/G1
S/G2
Go to bus2
BAT
SCAP
load1
Vbus1Ic
DC bus1
EMR’13, Lille, Sept. 201310
« EMR of helicopter Electrical Power System (EPS)»
« Energetic Macroscopic Representation of an helicopter
Electrical Power System»
EMR’13, Lille, Sept. 201311
« EMR of helicopter Electrical Power System (EPS)»
- EMR of a Starter/Generator and its converter -Starter/Generator and its converter:
Tsm1
Ism1
Esm1Ωshaft1
Tgear1
Ωturb1
Tturb1
Vconv1
Ibus_sm1
Tsm1 Ism1
Esm1
SM
Ism1
Ωshaft1
Tgear1
Ωturb1
Tturb1 Ωshaft1
Vconv1 Vbus1
Ibus_sm1
Vbus1
mconv1
where :
turbine gear box synchronous machine AC/DC converterD. Bienaimé, N. Devillers, M.C. Péra, F. Gustin, A. Berthon et M. Hopdjanian, «Energetic Macroscopic Representation of an electric network embedded in an aircraft», IEEE Vehicle Power and Propulsion Conference (VPPC),Chicago, USA, September 2011.
EMR’13, Lille, Sept. 201312
« EMR of helicopter Electrical Power System (EPS)»
- EMR of the battery and its converter -Battery and its converter :
VBAT
IBAT
Vchop1
Ibus_BAT
chopper 1 battery
Vbus1
VBATIBAT
Vchop1
Ibus_BAT
Vbus1 IBAT
SE
mchop1
where model parameters are dependent on SOC and temperature
D. Bienaimé, N. Devillers, M.C. Péra,F. Gustin, A. Berthon, M.L. Grojo,«Energetic Macroscopic Representationas an efficient tool for energymanagement in a hybrid electricalsystem embedded in a helicopter»,Conference on Electrical Systems forAircraft, Railway and Ship propulsion(ESARS), Bologna, Italy, October 2012.
N. Devillers, «Characterization and modeling of storage components», Ph.D. thesis of University of Franche-Comté, Belfort, France, November 29th 2012.
EMR’13, Lille, Sept. 201313
« EMR of helicopter Electrical Power System (EPS)»
- EMR of the supercapacitor pack and its converter -Supercapacitor pack and its converter :
Vbus1
where model parameters are dependent on voltage and temperature
VSCAPVchop2
Ibus_SCAP
ISCAP
chopper 2 supercapacitors
VSCAPISCAP
Vchop2
Ibus_SCAP
Vbus1 ISCAP
SE
mchop2
D. Bienaimé, N. Devillers, M.C. Péra,F. Gustin, A. Berthon, M.L. Grojo,«Energetic Macroscopic Representationas an efficient tool for energymanagement in a hybrid electricalsystem embedded in a helicopter»,Conference on Electrical Systems forAircraft, Railway and Ship propulsion(ESARS), Bologna, Italy, October 2012.
N. Devillers, S. Jemei, M.C. Péra, D. Bienaimé, F. Gustin, «Review of characterization methods for supercapacitor modelling», Journal of Power Sources 246 (2014)596-608.
EMR’13, Lille, Sept. 201314
« EMR of helicopter Electrical Power System (EPS)»
- EMR of the DC buses and DC/DC converter -DC buses and the DC/DC converter :
Vsource2 Ibus2
Idc2
Vdc2
Idc1
Vbus2
Isource2
Iload2
source 2 load 2 DC bus 2 DC/DC converter
Iload1Ic
DC bus 1 load1
Vbus1
SE
Vsource2
SE
Idc2
Ibus2
Isource2
Idc2
Vdc2 Vbus1
Idc1Vbus2
Vbus2
Vbus2
Vbus2
Isource2
Iload2
mdcdc
Ic
SE
Vbus1 Iload1
Vbus1
D. Bienaimé, «Modeling and energy management of an electrical power system for aeronautic auxiliary supply », Ph.D. thesis of University of Franche-Comté, Belfort, December 19th 2012.
EMR’13, Lille, Sept. 201315
« EMR of helicopter Electrical Power System (EPS)»
- Helicopter Electrical Power System -
Tsm1
Ism1
Esm1Ωshaft1
Tgear1
Ωturb1
Tturb1
Vconv1
Tsm2
Ism2
Esm2Ωshaft2
Tgear2
Ωturb2
Tturb2
Vconv2
Vsource2 Ibus2
Idc2
Vdc2
VBAT
IBAT
Vchop1
Ibus_BAT
VSCAPVchop2
Ibus_SCAP
ISCAP
Vbus1
Ibus_sm1
Iload1
Ibus_sm2
Idc1
Vbus2
Isource2
Iload2
Ic
turbine gear box synchronous machine AC/DC converter DC bus 1 load1
chopper 1 battery
chopper 2 supercapacitorssource 2 load 2 DC bus 2DC/DC
converter
D. Bienaimé, «Modeling and energy management of an electrical power system for aeronautic auxiliary supply », Ph.D. thesis of University of Franche-Comté, Belfort, December 19th 2012.
EMR’13, Lille, Sept. 201316
« EMR of helicopter Electrical Power System (EPS)»
- EMR of the helicopter Electrical Power System -
Tsm1 Ism1
Esm1
SM
Ism1
Ωshaft1
Tgear1
Ωturb1
Tturb1 Ωshaft1
Vconv1
Tsm2 Ism2
Esm2
SM
Ism2
Ωshaft2
Tgear2
Ωturb2
Tturb2 Ωshaft2
Vconv2
SE
Vsource2
SE
Idc2
Ibus2
Isource2
Idc2
Vdc2
VBATIBAT
Vchop1
Ibus_BAT
Vbus1 IBAT
SE
VSCAPISCAP
Vchop2
Ibus_SCAP
Vbus1 ISCAP
SE
SE
Vbus1
Ibus_sm1 Vbus1 Iload1
Vbus1
Ibus_sm2
Vbus1
Idc1Vbus2
Vbus2
Vbus2
Vbus2
Isource2
Iload2
mdcdc
Vbus1Ic
mconv2
mconv1 mchop1
mchop2
EMR of the helicopter EPS:
5 converters => 5 control parameters
D. Bienaimé, «Modeling and energy management of an electrical power system for aeronautic auxiliary supply », Ph.D. thesis of University of Franche-Comté, Belfort, December 19th 2012.
EMR’13, Lille, Sept. 201317
« EMR of helicopter Electrical Power System (EPS)»
« Maximal Control Structure of an helicopter Electrical Power System»
EMR’13, Lille, Sept. 201318
« EMR of helicopter Electrical Power System (EPS)»
- Maximal Control Structure of the helicopter EPS -MCS of Starter/Generators:
Tsm1Ism1
Esm1
SM
Ism1
Ωshaft1
Tgear1
Ωturb1
Tturb1 Ωshaft1
Ωshaft1_ref Tsm1_ref Ism1_ref
Vconv1
Vconv1_ref
Tsm2Ism2
Esm2
SM
Ism2
Ωshaft2
Tgear2
Ωturb2
Tturb2 Ωshaft2
Ism2_ref
Vconv2
Vconv1_ref
Ibus_sm2_ref
Vbus1
Ibus_sm1
Vbus1
Ibus_sm2
mconv2
mconv1
Starter mode :speed control
Generator mode :current control
D. Bienaimé, N. Devillers, M.C. Péra, F. Gustin, A. Berthon, M.L. Grojo, «Energetic Macroscopic Representation as an efficient tool for energy management in a hybridelectrical system embedded in a helicopter», Conference on Electrical Systems for Aircraft, Railway and Ship propulsion (ESARS), Bologna, Italy, October 2012.
EMR’13, Lille, Sept. 201319
« EMR of helicopter Electrical Power System (EPS)»
- Maximal Control Structure of the helicopter EPS -MCS of Energy Storage Systems:
Battery:current control
Supercapacitor pack:current control
VBATIBAT
Vchop1
Ibus_BAT
Vbus1 IBAT
SE
Ibus_BAT_ref
IBAT_ref
Vchop1_ref
VSCAPISCAP
Vchop2
Ibus_SCAP
Vbus1 ISCAP
SE
Ibus_SCAP_ref
ISCAP_ref
Vchop2_ref
mchop1
mchop2
D. Bienaimé, N. Devillers, M.C. Péra, F. Gustin, A. Berthon, M.L. Grojo, «Energetic Macroscopic Representation as an efficient tool for energy management in a hybridelectrical system embedded in a helicopter», Conference on Electrical Systems for Aircraft, Railway and Ship propulsion (ESARS), Bologna, Italy, October 2012.
EMR’13, Lille, Sept. 201320
« EMR of helicopter Electrical Power System (EPS)»
- Maximal Control Structure of the helicopter EPS -MCS of buses:
SE
Vsource2
SE
Idc2
Ibus2
Isource2
Idc2
Vdc2
SEVbus1 Iload1
Vbus1
Idc1Vbus2
Vbus2
Vbus2
Vbus2
Isource2
Iload2
Vbus2_ref Idc2_ref Vdc2_ref
mdcdc
Vbus1_ref
Vbus1
Ic
Ic
Ic_ref Ibus_SCAP_ref
Ibus_BAT
Ibus_sm2
Ibus_sm1Idc1
Iload1
Bus 1: voltage control and association with current control loop of supercapacitor pack (source with the fastest time response)
D. Bienaimé, «Modeling and energy management of an electrical power system for aeronautic auxiliary supply », Ph.D. thesis of University of Franche-Comté, Belfort,December 19th 2012.
Bus 2:voltage control and association with a current control loop
EMR’13, Lille, Sept. 201321
« EMR of helicopter Electrical Power System (EPS)»
- Maximal Control Structure of the helicopter EPS -MCS of helicopter EPS:
D. Bienaimé, «Modeling and energy management of an electrical power system for aeronautic auxiliary supply », Ph.D. thesis of University of Franche-Comté, Belfort, December 19th 2012.
EMR’13, Lille, Sept. 201322
« EMR of helicopter Electrical Power System (EPS)»
- Energy management of the helicopter EPS -Energy management of helicopter EPS:
D. Bienaimé, «Modeling and energy management of an electrical power system for aeronautic auxiliary supply », Ph.D. thesis of University of Franche-Comté, Belfort, December 19th 2012.
EMR’13, Lille, Sept. 201323
« EMR of helicopter Electrical Power System (EPS)»
« Simulation of helicopter EPS modelling with Matlab® Simulink»
EMR’13, Lille, Sept. 201324
« EMR of helicopter Electrical Power System (EPS)»
- Energy management of the helicopter EPS -Energy management of helicopter EPS:
0 2000 4000 6000 8000 10000 12000 140000.9995
1
1.0005
time [s]
volta
ge [V
]
Vbus1
0 2000 4000 6000 8000 10000 12000 14000
1
1
1
1
1
time [s]
volta
ge [V
]
Vbus2
0 2000 4000 6000 8000 10000 12000 140000
0.2
0.4
0.6
0.8
1
time [s]
curre
nt [A
]
Iload1Ioad2
0 2000 4000 6000 8000 10000 12000 14000-1
-0.5
0
0.5
time [s]
curre
nt [A
]
Ibus sm1Ibus sm2
0 2000 4000 6000 8000 10000 12000 14000-1
-0.5
0
0.5
time [s]
curre
nt [A
]
Ibus ACCIbus SCAP
0 2000 4000 6000 8000 10000 12000 140000
0.2
0.4
0.6
0.8
1
time [s]
stat
e-of
-cha
rge
[pu]
SOC ACCSOC SCAP
EMR’13, Lille, Sept. 201325
« EMR of helicopter Electrical Power System (EPS)»
- Conclusion and outlooks -
Conclusion and outlooks :
- Characterization and modeling of the EPS devices
- Simulation of the helicopter EPS in different operating modes
- Tests in a full-scale prototype with energy management
- Comparison of model simulation results with experimental results
EMR’13, Lille, Sept. 201326
« EMR of helicopter Electrical Power System (EPS)»
« BIOGRAPHIES AND REFERENCES »
EMR’13, Lille, Sept. 201327
« EMR of helicopter Electrical Power System (EPS)»
- References -
D. Bienaimé, N. Devillers, M.C. Péra, F. Gustin, A. Berthon et M. Hopdjanian, «Energetic MacroscopicRepresentation of an electric network embedded in an aircraft», IEEE Vehicle Power and PropulsionConference (VPPC), Chicago, USA, September 2011.
D. Bienaimé, N. Devillers, M.C. Péra, F. Gustin, A. Berthon, M.L. Grojo, «Energetic MacroscopicRepresentation as an efficient tool for energy management in a hybrid electrical system embedded in ahelicopter», Conference on Electrical Systems for Aircraft, Railway and Ship propulsion (ESARS),Bologna, Italy, October 2012.
J. Asensio-Sauto, M.L. Grojo, M.C. Péra, F. Gustin, «Modeling and simulation of a helicopter embeddeddirect current electrical power distribution network», Conference on More Electrical Aircraft (MEA),Bordeaux, France, November 2012.
J. Asensio-Sauto, M.C. Péra, F. Gustin, N. Devillers, M.L. Grojo, «Scalable modeling approach forassessing helicopter DC electrical power system performances», European Conference on ElectricalPower and Applications (EPE), Lille, France, September 2013.
N. Devillers, S. Jemei, M.C. Péra, D. Bienaimé, F. Gustin, «Review of characterization methods forsupercapacitor modelling», Journal of Power Sources 246 (2014) 596-608.
N. Devillers, «Characterization and modeling of storage components», Ph.D. thesis of University ofFranche-Comté, Belfort, France, November 29th 2012.
D. Bienaimé, «Modeling and energy management of an electrical power system for aeronautic auxiliarysupply », Ph.D. thesis of University of Franche-Comté, Belfort, December 19th 2012.
EMR’13, Lille, Sept. 201328
« EMR of helicopter Electrical Power System (EPS)»
- Authors -
Pr. Marie-Cécile PERAFEMTO-ST, University of Franche-Comté, FranceFull professor since 2008, Deputy Director of FEMTO-STPhD in Electrical Engineering at the INP of Grenoble (1993)Research topics: EMR, Optimized energy management and diagnosis of electrical systems (Fuel Cells, Storage systems…) for EVs and HEVs
Dr. Nathalie DEVILLERSFEMTO-ST, University of Franche-Comté, FranceResearch Engineer since 2009PhD in Electrical Engineering at University of Franche-Comté (2012)Research topics: Electrical Energy Storage Subsystems
Dr. Frédéric GUSTINFEMTO-ST, University of Franche-Comté, FranceAssitant professor, Director of the Institute of Technology of BelfortPhD in Electrical Engineering at the University of Franche-Comté (2000)Research topics: power electronics, converters and simulation methods