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Title: A Brief Course in Electrochemical Energy Storage


1
A Brief Course in Electrochemical Energy Storage
  • Bob Nuckolls
  • Sr. Engineer/SME
  • Raytheon Aircraft Company
  • Rev -B- 27 July 2004

2
Copies of this Power Point presentation may be
downloaded fromaeroelectric.com/ppt/Battery_Pre
sentation_D

3
A little history . . .
  • 1800 Volta demonstrates to Napoleon the Volta
    pile, a primary, non rechargeable battery.
  • 1854 Sinstede uses the first time lead plates in
    sulfuric acid to store i.e. accumulate,
    electricity.
  • 1859 Planté improves the capacity of the lead
    acid batteries with a technique still in use
    today.
  • 1881 Faure discovers the pasted plate which
    yields a major breakthrough in capacity. A lead
    antimony alloy is used the first time to give
    strength.
  • 1882 Gladstone and Tribe describe the so called
    double-sulfate theory i.e. the basis of operation
    of the lead acid battery. Tudor operates a lead
    acid battery factory in Luxembourg.
  • 1899 Jungner invents nickel cadmium rechargeable
    battery. Expensive and limited in useage. New
    electrodes developed 1930s. 1940s brought a
    sealed nickel cadmium battery that recombines
    internal gases produced during charge.
    Improvements have been made every decade since.

4
A little history . . .
  • 1907 A lead calcium alloy is patented.
  • 1910 The iron-clad or tubular plate construction
    is introduced
  • 1915 Willard introduces rubber separators.
  • 1918 Shimazu describes the ball mill oxide.
  • 1951 Lead calcium alloys are used in telephone
    exchange stationary lead acid batteries.
  • 1958 Jache describes the gel valve-regulated,
    sealed lead-acid battery.
  • 1965 Polypropylene sealed lead-acid battery cases
    start to be used.
  • 1968 The maintenance free sealed lead-acid
    battery is developed by Gates.
  • 1980 Stationary valve-regulated, sealed lead-acid
    batteries based on AGM technology are developed

5
A little history . . .
  • Primary Cells
  • One shot energy sources . . . Chemistry is not
    reversible
  • Typical products Carbon-Zinc, Zinc-Air,
    Manganese-Dioxide (alkaline)

6
A little history . . .
  • Carbon-Zinc Evolved from Leclanchés 1866
    patent on a wet cell design using a liquid,
    ammonium chloride electrolyte. A dry cell version
    of the Leclanché cell was developed and perfected
    in the 1880s. The carbon zinc dry cell remains
    much the same to this day.

7
A little history . . .
  • Duracell pioneered the Alkaline Manganese Dioxide
    electrochemical system nearly 40 years ago.
  • Alkaline cells have higher energy output than
    zinc-carbon predecessors.
  • Other significant advantages are
  • Longer shelf life
  • Better leakage resistance
  • Superior low temperature performance.

8
A little history . . .
  • Secondary Cells
  • Chemistry can be reversed by forcing energy back
    into the cell via external power supply
    (charger).
  • Typical products Lead-Acid, Ni-Cad, Ni-Mh,
    Lithium Ion

9
A little history . . .
  • Lead-Acid A very successful technology with over
    120 years of commercial service.

10
A little history . . .
  • Ni-Cad Nearly as mature as the Lead-Acid
    battery, Ni-Cads were the first to offer
    drip-free, sealed energy storage technology.

11
A little history . . .
  • Nickel Metal Hydride Chemically, one of the best
    cathode materials for battery cells would be
    hydrogen. Discoveries in late 1960s showed that
    some metal alloys had the ability to store atomic
    hydrogen 1000 times their own volume.
  • NiMh technology is rapidly replacing
    Nickel-Cadmium as the portable power
    cell-of-choice.

12
Electrochemical Energy Storage Basics(Its all
in the cells!)
What is a cell?
13
What is a cell?
Definition of Cell Anode - Source of electron
flow to the outside. Cathode - Sink for electron
flow from the outside. Electrolyte - Media for
the exchange of ions in reduction-oxidation
reactions at anode and cathode.
14
What is a cell?
Every material in the universe has a position on
the ladder of values for Electromotive Force when
compared with other materials . . . Lets explore
the comparative differences between a rudimentary
cell using silver-copper and silver-aluminum
electrodes . . .
15
What is a cell?
16
What is a cell?
17
What is a cell?
18
What is a cell?
19
What is a cell?
20
What is a cell?
21
What is a cell?
22
What is a cell?
23
What is a cell?
Classic classroom electrolysis demonstration . .
. The Lemon Cell.
24
What is a cell?
Construction typical of all flooded and gelled
lead-acid cells. A battery is a array of
series connected cells (higher voltage) or
parallel connected cells (higher capacity /
current)
25
What is a cell?
An array of cells assembles into a battery . . .
26
What is a cell?
Cutaway of Gates/Hawker/Enersys jelly roll
cells which introduced recombinant gas, lead-acid
technology to the marketplace in the late 60s.
27
What is a cell?
Gel-Cell Not! Prismatic VRSLA cells followed
closely on the heels of Gates Cyclon series
jelly-roll cells. The vent regulated, sealed
lead-acid (VRSLA), recombinant-gas (RG), absorbed
glass mat (AGM) products proliferated. Prismatic
cells are available in sizes from 0.5 to 1200
a.h. These are manufactured in the millions for
emergency lighting, portable power,
un-interruptible power supplies, etc. etc
Cells of these batteries contain so little liquid
that you can drive a nail into them, pull it out,
and they will not leak.
28
What is a cell?
Ni-Cad and Ni-Mh jelly-roll construction.
29
Lead-AcidElectrochemical Energy Storage Basics
Lead-Acid How it works . . .
30
Lead Acid how it works . . .
31
Lead Acid how it works . . .
The chemical reaction during normal lead-acid use
is Pb PbO2 lt-----gt 2PbSO4 H2O 2
electrons Fortunately the reaction proceeds
readily in either direction without much heat.
The chemistry usually is written as two half cell
reactions which makes it a little more clear just
what is happening at each plate At the anode
PbO2 4H 2 electrons---gt PbSO4
2H2O At the cathode Pb(metal) ---gt PbSO4 2
electrons (Equations above are not balanced) As
the battery discharges more water is produced
which forces specific gravity of electrolyte
lower.
32
Lead Acid how it works . . .
During cell over-charge there is no more
lead-sulfate left on the plates to be oxidized
and reduced. Current forced through a solution
must produce a reaction at both electrodes. Since
all materials used to store electrical energy has
been completely oxidized or reduced (charged)
something else happens. Further, its not good
for the battery and could generate a hazardous
condition. The net reaction in the battery
during overcharge is 2H2O 4 electrons ----gt
2H2 O2
33
Lead Acid how it works . . .
  • There are two basic cell types flooded-vented
    and starved-sealed.
  • Flooded cell batteries require vents to
    atmosphere so that loose hydrogen and oxygen
    gases generated during charging are vented from
    the cell.
  • Recombinant gas or immobilized electrolyte cells
    keep a grip on evolved gasses Oxygen generated
    from the positive electrode during charging
    diffuses to the negative electrode where it
    recombines to form water
  • The recombination reaction suppresses hydrogen
    evolution at the negative electrode so that the
    cell may be sealed to atmosphere.
  • In practice, the recombination efficiency is not
    100. Therefore, a pressure relief valve limits
    internal pressure to a relatively low value on
    the order of 2 psig.
  • Sealed lead-acid cells may be called
    valve-regulated lead-acid (VRLA) cells.

34
Lead-AcidBattery Fabrication
Lead-Acid Battery Fabrication
35
Lead Acid Battery Fabrication
36
Lead Acid Battery Fabrication
37
Lead Acid Battery Fabrication
38
Lead Acid Battery Fabrication
39
Lead Acid Battery Fabrication
Buttered plates are stacked and then cured for
two weeks in a temperature-humidity controlled
environment.
40
Lead Acid Battery Fabrication
41
Lead Acid Battery Fabrication
42
Lead Acid Battery Fabrication
43
Lead Acid Battery Fabrication
44
Lead Acid Battery Fabrication
45
Lead Acid Battery Fabrication
46
Lead Acid Battery Fabrication
47
Lead Acid Battery Fabrication
48
Lead Acid Battery Fabrication
49
Lead Acid Battery Fabrication
50
Lead Acid Battery Fabrication
51
Lead Acid Battery Fabrication
52
Lead Acid Battery Fabrication
53
Lead Acid Battery Fabrication
54
Lead Acid Battery Fabrication
At this point, the capped battery sits overnight
for sealing epoxy to set up. Battery is pressure
tested on a cell-by-cell basis. Any detected
leakage is cause for rejection.
55
Lead Acid Battery Fabrication
56
Lead Acid Battery Fabrication
57
Lead Acid Battery Fabrication
58
Lead Acid Battery Fabrication
59
Lead Acid Battery Fabrication
60
Lead Acid Battery Fabrication
61
Lead Acid Battery Fabrication
  • Cast lead plates (1 calcium reduces water loss)
  • Apply paste positive and negative plates
  • Aged two weeks
  • Insulated and sleeved
  • Soldered into temporary battery array
  • Charge individual plates
  • Group sets of () and (-) plates for assy and
    then group again for weight matching.
  • Molded plastic cases and tops
  • Install sets of plates in battery box.
  • Weld risers onto plate arrays
  • Hand-weld crossovers and terminal straps
  • Epoxy grooves in lid and set battery upside down
    into lid
  • Pressure test. If pressure test fails, battery
    is scrap.
  • 7x Deep cycle charge and capacity tests
  • Pour out excess electrolyte
  • Cap and wash
  • Ip Test
  • Elapse Time 6 weeks!

62
Lead Acid Battery Fabrication
63
Lead Acid Battery Fabrication
Exploded view of a Concord lead-acid aircraft
battery . . .
64
Lead Acid Battery Fabrication
65
Lead Acid Battery Fabrication
66
Lead Acid Battery Fabrication
Concord Labor intensive. 160 employees
fabricate 1000 units a day Lead Calcium Alloy
Plates Cast Plates, cast pockets for active
material An array of plates are weighed on
cell-by-cell basis for capacity matching. Sets of
plates are relatively loose fit in battery box
and placed individually by hand before inter-cell
connections are hand welded.
Enersys (Hawker) Highly automated 560 employees
fabricate 60,000 units a day Pure Lead
Plates Plates punched from long rolls of
chill-cast lead sheet No porous plastic pocket
over plate structure. AGM is only separator. Sets
of plates are hydraulically compressed and pushed
into tight fitting boxes by machine. Inter-cell
connections are spot welded
67
Lead Acid Battery Fabrication
Concord cont. Dry charged cells are flooded and
electrically cycled to insure saturation of
separators. Cells are sealed after excess
electrolyte is poured out at the conclusion of
deep cycle activation and testing. Manufacturing
cycle 6 weeks
Enersys (Hawker) cont. Electrolyte vacuum
injected in precise amounts and cells are
immediately sealed. Battery is activated during
first charge cycle. Manufacturing cycle 5
weeks. Cost approx 2x that of comparable Concord
68
Lead Acid Battery Fabrication
  • Coming over the hill . . .
  • Concord has patented a new process for making
    lighter grid plates.
  • Lead-clad ALUMINUM plates are being perfected.
    Chemically, these perform light lead but offer
    lighter structure, stiffer plates and better
    conductivity.
  • This process promises substantial reductions in
    battery weight by something on the order of 20.
  • Recycling is more difficult . . . Aluminum does
    NOT mix well with lead in a smelting operation.
    These new products will CANNOT utilize the
    current recycle stream for lead-acid batteries.

69
Lead-Acid Battery Operation
70
Lead Acid Battery Operation
  • Batteries in airplanes serve three major
    functions
  • Crank engine(s). This is a relatively high
    power/low energy (perhaps 5 to 15 of batterys
    total charge is needed to get a turbine engine
    started. Even less for a piston engine.
  • Filter / stabilize the operating system. The
    batterys low internal impedance provides the
    best filter for alternator / generator noise.
    Also, some alternators do not run well without a
    battery on line.
  • Standby power in case of engine driven source
    failure. Here the battery must be sized and
    maintained to assure duration of operation of
    equipment essential for descent to landing.

71
Lead Acid Battery Operation
  • Engine Cranking . . .
  • Getting the engine started is certainly a
    high-power event. Currents delivered by the
    battery at the beginning of a turbine start cycle
    is on the order of 700 to 1000 Amps. It tapers to
    about 300 Amps at the end of a 20-30 second start
    cycle.
  • While the current levels are high, total energy
    removed from the battery is a fraction of the
    battery total. The 200,000 watt-second start
    curve illustrated next represents less than 10
    of typical batterys 3,000,000 watt-second
    capacity.
  • Reciprocating engines start in a much shorter
    period of time on the order of 5-10 seconds . . .
    Average current during the start cycle is 200-300
    Amps.
  • A reciprocating engine takes about 40,000
    watt-seconds, about 4 of the batterys capacity.
  • While power levels are high, total energy
    requirements are rather modest.

72
Lead Acid Battery Operation
Beechjet Start Curve Piecemeal Integration
Shows 200Kw/Sec Start Cycle
73
Lead Acid Battery Operation
The importance of controlling internal and
external impedance . . .
74
Lead Acid Battery Operation
75
Lead Acid Battery Operation
Each cell can be visualized as many hundreds of
individual cells-sites in parallel . . . Each one
contributing a small energy storage
capability and a moderately high source
impedance. E.g. A cell of 1000 cell-sites having
individual source impedance of 1 ohm combine to
make a single cell with a source impedance of
1 milliohm. When half of the cell sites die,
capacity drops by half and source impedance
doubles.
76
Lead Acid Battery Operation
Effects of internal impedance become apparent
when we consider energy delivered to the external
world at various discharge rates. Here are
typical discharge curves at 25C for a 24 Volt,
37 Ah VSLA aircraft battery.
77
Lead Acid Battery Operation
  • Standby Power. . .
  • This is the batterys toughest task . . . Most
    production aircraft with a standby power storage
    requirement call for 30 minutes of operation sans
    engine driven power sources.
  • Unlike engine cranking, emergency operations are
    all but guaranteed to tax the batterys capacity
    to the limit.
  • Unfortunately, battery capacity cannot be gauged
    from outside the battery without doing an actual
    capacity test.

78
Lead Acid Battery Operation
Portable capacity tester/chargers do exist but
theyre not the kind of thing you find in the
average mechanics tool box!
79
Lead Acid Battery Operation
Ideal charging voltage for a battery is
temperature dependent. Unfortunately, the only
known temperature compensated regulators for
aircraft applications are available only to the
owner-built and maintained (OBAM) aircraft
community.
80
Lead Acid Battery Operation
Lacking the elegant solution regulator, the
best compromise is to make maintenance
adjustments of bus voltage depending on current
climatic operating conditions. The following
recommendations come from Concords user guide on
lead-acid battery application.
81
Lead Acid Battery Operation
The ideal battery charging philosophy maintains
voltage commensurate with present battery
temperature until recharge rate drops to less
than 1A at the whereupon voltage should be
stepped down to something on the order of 13.5
(27.0) volts.
A stepped down maintenance voltage would be just
high enough to prevent loading the battery but
too low to put any significant charge on the
battery. This charging philosophy would promise
nearly ideal battery service life by offering
fastest practical recharge while protecting the
battery from overcharging.
82
Care and Feeding of Lead-Acid Batteries
83
Care and Feeding of Lead Acid Batteries . . .
  • A comprehensive study was recently conducted at
    RAC to determine why we were suffering large
    warranty losses on batteries installed in
    customer aircraft.
  • The study looked at end-to-end battery handling
    issues from the time a cell plate is fabricated
    until a battery is no longer suited for service.
  • A major fraction of the costs were traced to
    poor warranty policy . . . RAC warranty was set
    to a value much greater than the battery
    manufacturers warranty. Most of the cash bleed
    was fixed with a more realistic battery warranty
    policy.
  • The study identified a number of areas where
    battery handling can be improved.
  • Take advantage of just-in-time deliveries
    offered by battery manufacturers to reduce number
    of batteries in inventory -AND- time that
    batteries sit on the shelf.
  • Concentrate battery delivery and storage in
    smaller area. A survey of SAP showed that we had
    batteries in storage in dozens of different
    places on the square mile.

84
Care and Feeding of Lead Acid Batteries . . .
  • Reduce numbers of folk who need to touch
    batteries. Individuals who dont handle
    batteries dont need to be trained or provided
    with tools and work-orders to accommodate a
    batterys special needs. Cost of ownership and
    risks go down.
  • Vast majority of handling induced battery
    failures on square mile occur either on
    experimental flight test aircraft or batteries
    neglected in storage.
  • Most production lines already use tool
    batteries . New policies and procedures have
    been developed to store customer batteries in
    racks at the end of assembly lines.
  • Tool batteries will be used until aircraft is
    ready for delivery to flight test.
  • Number of storage locations for batteries on the
    square mile reduced to a tiny fraction of the
    current condition.
  • Few opportunities for improvement were
    identified after the customer battery was
    installed on the aircraft Battery failure rates
    from time-of-installation to time-of-delivery was
    quite low . . .

85
Care and Feeding of Lead Acid Batteries . . .
  • Opportunities for improvement
  • Work with field service organizations to avoid
    handling damage on replacement batteries.
  • New policies and procedures for ordering stock
    warehousing.
  • Develop first-in-first-out handling procedures.
  • Develop monitoring techniques for ALL
    life-limited parts including batteries.
  • Acquire tools and conduct training for battery
    maintenance where there is a demonstrable return
    on investment.
  • Conduct training for folks who handle batteries
    to improve awareness of the fragile nature of
    stored batteries.
  • Work with manufacturers to improve data
    gathering on field failures. This same data
    offers a fall-out opportunity to improve battery
    performance based on real-life numbers on how
    aircraft batteries are used. More on this later.

86
Lead Acid Battery Operation
  • Long Term Battery Storage
  • A number of conditions affect the magnitude of
    leakage current in batteries.
  • Storage temperature
  • Batteries stored in warm climes and un-controlled
    warehouse environments are especially subject to
    increased rates of leakage discharge. Batteries
    stored in Canadian warehouses do very well.
  • Free oxygen dissolved in the electrolyte.
  • When a cell is sealed off from the environment,
    the percentage of dissolved gasses in the
    electrolyte drops to a very low value. This
    simple isolation of the cell environment from
    ambient atmosphere results in markedly low self
    discharge rates.
  • VSLA batteries can be stored at moderate
    temperatures for many months.

87
Lead Acid Battery Operation
  • Long Term Battery Storage (cont)
  • Batteries in warehouses tend to be stored in
    ready-to-ship cartons or crates.
  • This works directly against any efforts to
    monitor or maintain batteries on the shelf.
  • Any stocking operation that intends to keep
    zero-time batteries in long-term storage (6
    months or more) would do well to store them out
    of the crate and connected to some form of
    battery-tending power supply to offset
    self-discharge characteristics inherent in all
    batteries.

88
Lead Acid Battery Operation
Long Term Battery Storage EVERY battery suffers
from some degree of internal self-discharging
leakage. This manifests itself as a low level
load on the battery that will eventually
produce a totally discharged battery.
A Battery Tender type of smart charger will
charge initially at some level that insures a
charge top-off . . . Something on the order of
14.4/28.8 volts. When charge acceptance current
drops below some small value, the output voltage
drops to 13.0/26.0 volts so that the Battery
Tender exactly offsets the leakage currents.
89
Lead Acid Battery Operation
0.75A Battery Tender from Deltron
(www.batterytender.com)
90
Lead Acid Battery Operation
91
Lead Acid Battery Operation
92
Value Assessment of Concord vs..
Enersys(Getting Past the Marketing Hype . . .
Beware of Pink Bunnies)
93
Getting Past the Marketing Hype . . .
94
Getting Past the Marketing Hype . . .
95
Getting Past the Marketing Hype . . .
Performance of various AA cell brands at room temp
96
Getting Past the Marketing Hype . . .
Alkaline vs.. Photo Lithium at Room Temp and -20C
97
Getting Past the Marketing Hype . . .
  • Bottom line of study on AA Alkaline batteries
    Irrespective of intensity and flavor of marketing
    hype, the best isnt a lot better than the
    worst and the lowest cost is not the worst
    yet offers the best value.
  • We know that lead-acid capacity is a function of
    mass of reactants. Lead, lead-oxide, sulfuric
    acid, water, lead-sulfate, and to some lesser
    degree, mini-reactions that affect
    charge/discharge efficiency and water loss. Just
    how bad can a lead-acid battery be?
  • Greater number of thinner, pure lead plates has
    an obvious advantage in terms of lowering
    internal impedance of the cells but since most of
    our customers are obligated to set service life
    based on capacity, is there a cost-of-ownership
    advantage to the higher cost of thin, pure-lead
    plates?
  • A question yet to be answered is whether the
    premium construction of an Enersys (Hawker)
    battery translates directly into additional
    service life commensurate with the increased cost
    of the battery.

98
Getting Past the Marketing Hype . . .
  • Current best recommendation for the Owner Built
    and Maintained Aircraft (OBAM) community is to by
    the least expensive product you can find and
    change it out often . . . Like every annual
    inspection.
  • For light aircraft running dual batteries, this
    means that you can put a new battery in the main
    battery slot every year and rotate the main
    battery into the auxiliary battery slot.
  • For a cost of about 40/year
  • The main battery is less than 1 year old and
    its stand-by capacity is assured.
  • There are no batteries more than 2 years old and
    the auxiliary battery can be depended on for
    backing up a light, ignition load (2A or so) for
    duration of fuel aboard.
  • Two batteries in parallel offer 34 a.h. cranking
    performance for superior engine starting.

99
Getting Past the Marketing Hype . . .
  • The jury is still out on battery brand selection
    philosophy (Concord versus Hawker) based on
    real-number economics and physics.
  • There is consideration for developing a black
    box for aircraft batteries.
  • A small (0.5 x 1.0 x 2.0) module mounted in
    the head-space of the battery would measure and
    record voltage and temperature every 10 seconds
    for two years.
  • When a battery is taken out of service, the
    black box can be easily removed and sent back
    to manufacturer for evaluation. One can easily
    deduce number of flights, number and difficulty
    of engine starts. If, when and for how long a
    battery was deeply discharged and stored in a
    discharged state, etc.
  • A battery taken out of service need not be
    shipped to a remote location for evaluation. The
    maintenance technician needs only to return the
    black box. Battery is recycled locally.

100
Getting Past the Marketing Hype . . .
  • The cost of the black box may well be less than
    cost of shipping a battery.
  • When batteries are pulled for warranty
    adjustment, the manufacturer would have hard data
    on potential abuse of the battery.
  • A parallel program to offer credit on new
    battery by returning the black box would
    encourage field participation data gathering for
    product improvement studies.
  • Same device might include an LED warning light
    that illuminates below 25.0 volts . . . Battery
    in storage can say Charge Me!

101
Getting Past the Marketing Hype . . .
  • There is substantial anecdotal information
    suggesting that a major source of battery-killing
    stress in field is failure to shut of hot-battery
    bus accessories in some models. This will run the
    battery down completely. Batteries stored in this
    condition are VERY difficult to recover. The
    battery black box would record these events.
  • When the battery makes it past the warranty
    period, data gleaned would provide hard data
    feedback on battery performance and battery
    usage. This type of information would be
    invaluable to the manufacturer in making process
    tweaks to design to maximize performance.
  • This data would also cut through the fog of
    marketing hype and permit considered
    recommendations of one brand over another with
    respect to overall battery performance and best
    value for cost-of-ownership issues.
  • At this time Its not clear that capacity based,
    service life of pure-lead, thin-plate Enersys
    products will outperform Concord cast-plate
    products a factor of 21

102
Summation on Batteries . . .
  • Batteries are like houseplants Peak performance
    is achieved with optimized control of deleterious
    and helpful environmental conditions.
  • When a battery is fully discharged and allowed
    to sit, irreversible damage MAY result . . . Not
    all batteries can be recovered from this kind of
    abuse.
  • Service life is strongly influenced by owner,
    pilot and maintenance behavior. A battery
    likes to be moderately challenged often.
    Batteries stored for long periods of time will do
    better with considered attention . . . Like
    Battery Tenders.

103
Missed Opportunities . . .
  • The aviation design community has been aware of
    the temperature dependence of lead-acid batteries
    and temperature criticality of nickel-cadmium
    batteries for a very long time.
  • However, there have been no development
    programs that specify generator and alternator
    control units to extend battery life and reduce
    maintenance costs.
  • Accessories that run from hot-battery busses
    should be fitted with auto-shutoff timers or
    other technology designed to protect batteries
    from accidental total discharge.
  • There may be value for OEM airframe engineers
    and field service personnel to participate in
    promoting and implementing installation and
    recovery of black boxes on aircraft batteries.
  • There is value in crafting and presenting
    familiarization courses and published materials
    to elevate all user awareness of the unique
    characteristics of aircraft batteries.

104
A Brief Course in Electrochemical Energy Storage
The End
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