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Microturbines
2005-04-21Rolf Gabrielsson, Volvo Aero Corporation
Section 3
Microturbine lecture, section 3, 2005-04-21, Rolf Gabrielsson
Microturbines, section 3
10111 Utg. 1
MEMS Gas Turbine Engines
• Micro-Electro-Mechanical-Systems (MEMS) or Ultra-microturbines.Ref.: Alan H. Epstein, ASME GT-2003-38866
• Microturbines 25 – 500 kW
• Small microturbines 1 – 10 kW Example: IHI remote application
• MEMS 10 - 100 W
Microturbine lecture, section 3, 2005-04-21, Rolf Gabrielsson
Microturbines, section 3
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MEMS Characteristics
• MEMS based on manufacturing technologies developed by the semiconductor industry
• Diameters of millimetres rather than meters with airfoil dimensions in microns rather than millimetres
• Shirt-button-sized gas turbine
Microturbine lecture, section 3, 2005-04-21, Rolf Gabrielsson
Microturbines, section 3
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User Pull - Market interest
• Small portable electronics - computers, GPS receivers, etc require compact energy supplies
• Mobile systems such as robots,air vehicles require increasingly compact power and propulsion
• Hydrocarbon fuels burned in air have 20-30 times the energy density of the best current lithium chemistry-bases batteries Modest system efficiency to compete with batteries
• Development started mid 1990´s
• Main player: MIT,USA
Microturbine lecture, section 3, 2005-04-21, Rolf Gabrielsson
Microturbines, section 3
10111 Utg. 1
Thermodynamic scaling• Air intake diameter:100 MW 1 meter100 W 1 mmHowever reduced pressure ratio (2:1 - 4:1), TIT and increases losses means reduced specific power
• Fluid viscous forces - IncreaseSurface area-to volume - IncreaseHowever, usable strength of material - Increase
• Manufacturing constraints means:- Reduced cycle efficiency Increased specific fuel consumption- But better thrust – to weight ratio. ”The cube-square law”
Microturbine lecture, section 3, 2005-04-21, Rolf Gabrielsson
Microturbines, section 3
10111 Utg. 1
Thermodynamic scaling
Ref.: Gong, Sirakov, Epstein, Tan “Aerothermodynamics of Micro-turbomachinery”, GT2004-53877, ASME Turbo Expo 2004, Vienna
Microturbine lecture, section 3, 2005-04-21, Rolf Gabrielsson
Microturbines, section 3
10111 Utg. 1
Mechanical scaling• Viscous forces larger
film heat transfer coefficient increases Temperature gradients in the structure reduced Helpful reducing stress but makes thermal insulation challenging
• Possibility to use ceramic materials due to size dependent fault-possibility
• Single-crystal semiconductor materials. Usable strength increase with reduced size
• Thermal shock resistance improvedRef: Epstein, ASME GT-2003-38866
Microturbine lecture, section 3, 2005-04-21, Rolf Gabrielsson
Microturbines, section 3
10111 Utg. 1
MEMS Gas turbine design for demo-MEMS
• Microturbine technology applies to Silicon, Si• Si loses strength above 950K• Fuel: H2
• Shaft power: 17 W• Design characteristics:Π = 2:1TIT = 950KDcompressor = 8 mmDturbine = 6 mmRotor speed = 1.2 Mrpm
Ref: Epstein, ASME GT-2003-38866
Microturbine lecture, section 3, 2005-04-21, Rolf Gabrielsson
Microturbines, section 3
10111 Utg. 1
MEMS Manufacturing
• Old-school designer ”Don´t let the manufacturing people tell you what you can´t do”MEMS design philosophy: ”Design for manufacturing”
• Primary fabrication processes:- Etching of photolithographically planar geometries- Bonding of multiple wafers
• Electronics, motors and sensors- Embedded sensors- Alternating insulation and conducting layers- Vapour deposition or sputtering approaches
Microturbine lecture, section 3, 2005-04-21, Rolf Gabrielsson
Microturbines, section 3
10111 Utg. 1
Manufacturing / complete stack
Ref: Epstein, ASME GT-2003-38866
Microturbine lecture, section 3, 2005-04-21, Rolf Gabrielsson
Microturbines, section 3
10111 Utg. 1
Turbine design
• Si prototype turbine TIT < 950 K- (MIT has designed for 1600 K)
• Possible turbine performance- Π = 4:1- Tip speed = 500 m/s- Efficiency, total-to static = 50-60%
(compare Microturbine turbine efficiency approx = 85%)
Microturbine lecture, section 3, 2005-04-21, Rolf Gabrielsson
Microturbines, section 3
10111 Utg. 1
MEMS combustor
Ref: Epstein, ASME GT-2003-38866
• Fuel : H2 (methane, propane)
• Reaction rate- H2 = 90%- Methane = 60%- Compare large Gt: 99.9%
Microturbine lecture, section 3, 2005-04-21, Rolf Gabrielsson
Microturbines, section 3
10111 Utg. 1
Bearings and rotor dynamics
• Electromagnetic and air bearings have been considered
• Electromagnetic bearings up to now not promising
• Gas bearings have advantages such as - No temperature limits- High load- Relatively simple manufacturing
• Gas bearings used in ”microturbines”in the range 30 – 70 kW and turbochargers. Also in gyroscopic instruments
Microturbine lecture, section 3, 2005-04-21, Rolf Gabrielsson
Microturbines, section 3
10111 Utg. 1
Examples of hydrodynamic and hydrostatic air bearings
Ref: Epstein, ASME GT-2003-38866
Microturbine lecture, section 3, 2005-04-21, Rolf Gabrielsson
Microturbines, section 3
10111 Utg. 1
MEMS materials
Si SiC
Max temperature 950 K 1500 KCost 1 100
Microturbine lecture, section 3, 2005-04-21, Rolf Gabrielsson
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MEMS GeneratorPermanent magnetic high speed generator
Ref: Epstein, ASME GT-2003-38866
Microturbine lecture, section 3, 2005-04-21, Rolf Gabrielsson
Microturbines, section 3
10111 Utg. 1
Ongoing technical development
• No reported MEMS operations up to date
• Demonstration of component technology at MIT
• Possible improvements as recuperated cycles with heat exchangers
• MEMS performance:
Ref: Epstein, ASME GT-2003-38866
Microturbine lecture, section 3, 2005-04-21, Rolf Gabrielsson
Microturbines, section 3
10111 Utg. 1
Economics and the future• What is required to make millimetre-scale turbines real?
Answer: - Technical feasibility - Must fulfil societal needs
• Power production in short term is aimed at portable applications due to:- Very much larger energy density of hydrocarbon fuel compared to lithium batteries
• In short term, 5 – 10% overall system efficiency is sufficient
Ref: Epstein, ASME GT-2003-38866