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Performance
of 50 Completed ATP Projects
Status
Report - Number 2
NIST SP 950-2
APPENDIX
B
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Terminated
Projects
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| At
the end of an ATP competition, projects are selected for award and
the winners are announced. Most of these projects proceed through
their multiyear research programs to completion. A few of the projects
that are announced, however, never actually start. A few others start,
but are not carried through to completion. Rather, they are halted
for a variety of reasons. The projects that are announced but do not
start, and those that start but are stopped prior to completion, are
collectively called by the ATP terminated projects. |
During
the time that the 50 projects covered in the body of this report completed
their research agendas, 16 of the 522 projects announced by the ATP through
2000 were terminated short of completion. This appendix examines the reasons
for their termination, and the funding spent on the projects.
In addition,
one of the terminated projects is reviewed in detail. The purpose is to
provide insight about what can go wrong during the complex, challenging
period of research, and also to illustrate that much can be learned despite
project derailment.
Reasons for Termination
Thus far, projects have terminated short of completion for the following
six principal reasons:
Reason
1:
A company leading a project, or one or more companies in a joint venture,
may request their project be stopped due to unexpected, adverse changes.
Shifts in company strategic goals; major reorganizations, mergers, and
changing leadership; changes in market demand and the competitive situation
are among the events that may affect the internal and external business
climate in which companies operate and plan. Any of these developments
may disrupt project plans.
Reason 2:
Financial distress may cause one or more companies providing matching
funds to become unable to meet the resource commitment that is a necessary
condition for ATP funding. Cash-flow difficulties may force a small company
to drop its research activities and pursue short-term survival goals,
or it may go bankrupt. Financial backers may pull back or fail to materialize
as expected, or they may delay. Corporate internal sources of funds may
not be provided as expected.
Reason 3:
Organizations proposing as a joint venture may find last-minute obstacles
to signing their agreement and decide to disband their planned partnership.
Reason 4:
Lack of technical progress can result when bottlenecks arise or technical
problems prove intractable. Technical challenges may be even more difficult
than expected. Personnel or management deficiencies, or unavailability
of prerequisite materials, components, or equipment may also end a project
prematurely.
Reason 5:
Early success can obviate the need for a project to continue. That is,
unexpected events in research can have positive as well as negative effects.
Reason 6:
Downstream changes may move a project out of compliance with ATPs
selection criteria, and cause ATP to stop the project. For example, a
project may attempt to shift away from challenging, enabling research
toward business as usual approaches; or the loss of key members of a team
(without a plan for overcoming the deficiency in a timely way) may threaten
the ability of a project to meet its goals.
Sixteen Terminated
Projects
Figure B-1 shows the distribution of 16 projects terminated during the
time the 50 featured in the body of the report were completed. To date,
terminations are running from five to six percent of total projects selected
and announced. (1)
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Figure
B-1. Distribution of Terminated Projects by Reason for Termination
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Of the 16 terminated
projects, 5 were stopped before they got started. The remaining 11 went
varying distances in their research agenda before they were stopped. Thirty-one
percent of the projects were joint ventures whose members could not reach
final agreement among themselves, and, therefore, never progressed further.
An equal percentage got started, but closed down because the project leader
or joint-venture members wanted the project stopped due to change in strategic
goals, structure, markets, or other factors. Financial distress caused
19 percent of the projects to end prematurely. These were primarily small
companies that encountered cash-flow difficulties.
Terminated Does Not
Equal Total Failure
It is an oversimplification to think of the terminated group simply as
project failuresalthough they clearly did not live up to expectations.
Terminated projects can produce important knowledge gains even when ultimate
goals are not reached. As the following example demonstrates, terminated
projects may yield patents, papers, collaborative relationships, and products.
Even projects that
stop without ever getting off the ground entail a great deal of integrated
planning for research, development, and business activities. They typically
entail substantive cross-disciplinary contact among scientists and other
researchers, cross talk among technical and business staff, and high-level
negotiations among business executives at different companies. Often the
planning period brings together business staff with university researchers,
federal laboratory specialists, and other nonprofit facilities. The ATP
process has been said by many to stretch the thinking and horizons of
participants in the process. There are likely to be extended effects of
this process that may bear fruit in future diverse and difficult-to-capture
ways.
Would-be joint-venture
partners may regroup to reapply to ATP, or find other ways to cooperate.
Companies may learn about new opportunities. They may apply the integrated
planning techniques to other projects. The companies involved, as well
as others, may learn from the terminated projects, approaches to avoid
or to pursue. In short, terminated projects as a group may yield some
positive effects even as they incur costs.
The mini-case treatment
of a terminated project that follows illustrates the achievements and
failures of a project that went part of the way: the project aimed to
develop composite flywheels for electric vehicles. It lasted nine months
of an anticipated three-year period, and was terminated when the company
requested that it be stopped due to an unanticipated changein this
case, a change in cost targets set by automakers.
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Dow-UT
Composite Products, Inc.
Composite
Flywheels for Electric Vehicles:
A Terminated Project that Produced Partial Results
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| Electric
Vehicles (EVs) are no longer concept cars of the future. Today, they
offer the promise of reduced air pollution and less reliance on imported
crude oil, but technical obstacles impede their widespread acceptance.
They are powered by an energy storage device, from which energy is
converted to either alternating current (AC) or direct current (DC),
to drive electric motors that propel the vehicle. Performance demands
of the vehicle determine the key performance requirements of the energy
storage device: range dictates a minimum energy storage capacity;
acceleration rate is tied to the maximum energy dissipation rate (surge
or peak power) of the storage device. A power source that is both
efficient and light is key to successful commercialization, but thus
far available sources have proven inadequate. |
Battery Alternatives
Traditional lead-acid batteries currently used in EVs cannot meet the performance
requirements of the automobile market. They have a number of drawbacks.
Although they are capable of storing large quantities of energy, they are
inefficient at absorbing high power levels (charging) and at dissipating
the high power levels needed for acceleration (surging). Moreover, lead-acid
batteries are very heavy. Even a small EV such as a converted Geo Metro
requires nearly 700 pounds of lead-acid batteries, (at a cost of some $1,600)
for reasonable performance. This weight requires additional energy and power
to meet performance goals, and creates problems of crash safety and vehicle
handling. A number of alternative chemical battery technologies are under
development, but none is yet recognized as a practical alternative.
Hybrid Electric Vehicles
Problems with conventional EVs have prompted work on hybrid electrical
vehicles. The hybrid EV uses two energy sources: one for mass energy storage
and the second for power storage. A hybrid vehicle might, for example,
employ a lead-acid battery for energy storage and another energy source
to meet peak or surge power needs. Flywheel systems are an important contender
for the latter application.
Flywheels
A flywheel is the mechanical equivalent of a rechargeable battery. It
operates by storing kinetic energy in the rotary motion of a ring or rotor
spinning on an axis. When coupled with an electric generator, its stored
kinetic energy can be rapidly converted to electrical energy. Since this
power conversion is a mechanical process, energy transfer is direct, not
limited by chemical reaction rates as in batteries. The rapid conversion
of kinetic energy to electrical energy makes flywheels suitable for use
as surge power devices for acceleration of hybrid vehicles. They can be
used to complement the steady energy supply from a chemical battery or
a heat engine (e.g., internal combustion engine).
In flywheel systems
under consideration, a flywheel rotor is attached to a central shaft.
To reduce friction and increase speed, the shaft is mounted on magnetic
bearings and is contained within a vacuum chamber. The central shaft is
connected to an electric generator that can absorb or discharge power
as needed. The entire apparatus is inside a protective casing to prevent
damage to surrounding parts if the flywheel becomes unstable or fails.
The Physics of Flywheels
The ability of a flywheel to store energy is dependent on two characteristics:
the weight of the rotor and its rotational speed. The heavier a flywheels
rotor or the faster it spins, the greater the flywheels energy storage
capacity. However, storage capacity increases linearly with weight (in
a ratio of one to one), while it is the square of rotational speed. This
concept favors efforts to increase energy storage without increasing weight
(i.e., energy density). This goal, however, is constrained by limits in
the strength of the rotor itself. Increases in rotational speed generate
increases in centrifugal forces (the forces that push you to the outside
when you are spinning on a merry-go-round). These forces place strain
on the flywheel rotor. The rotor must be able to withstand these forces
without breaking apart.
To reduce weight,
composite materials have been employed in the fabrication of rotors. Composite
rotors with the strength to endure the strain imposed by high rotation
speeds have had to be made with all-graphite fibers, which are too expensive
for all but a few aerospace and defense applications. A promising approach,
therefore, was development of new methods for fabricating flywheel rotors
with the requisite strength that could use cheaper composite materials.
Dow-UT Pursuit of
the Resin Transfer Molding Process
In late 1989, Dow Chemical Company and United Technologies Corporation
(UT) formed a joint-venture entity, called Dow-United Technologies Composite
Products, Inc., to exploit the commercial potential of a new process,
known as Resin Transfer Molding (RTM), for fabricating composite parts.
In the subsequent five years, Dow-UT spent $40 million to develop RTM
into a commercially viable process. It demonstrated the commercial viability
of RTM for high-performance aerospace and defense applications. The focus
was on using RTM in the production of high-speed rotating parts, such
as the fan spacers used in the Pratt and Whitney 4084 commercial jet engine.
Dow-UT was also successful in developing RTM for use in the production
of high-volume, lower-cost automotive applications. For example, Chrysler
used Dow-UTs RTM process for the production of specialty automotive
parts for the Dodge Viper.
A Plan for Developing
Strong, Lower Cost Flywheels
In a 1994 focused program competition, ATP announced the Dow-UT project
as an award winner. The planned ATP cost share was $519,000 over a three-year
period. The goal of the project was to develop cost-effective production
methods for strong, lightweight composite flywheel rotors to be used in
hybrid electric vehicles.
For the ATP project,
Dow-UT obtained the commitment of several other companies in subcontractor
roles and several other divisions of UT to contribute essential skills
and resources. Suppliers included Fiberite Specialty Weaving Group, with
experience in a technique known as polar weaving.(2)
Dow Chemical worked on flow modeling and Test Devices engaged
in spin testing. One division of UT provided design and test consulting,
and another division was involved in flywheel commercialization.
Dow-UT saw the technology
as a multi-use technology with broad application through licensing in
the auto industry and beyond. Extensive licensing of a technology tends
to yield greater spillovers for the economy.
An example of a potential
applicationif strong, lightweight composite rotors could be developedis
the use of flywheel systems by utilities in load-leveling devices (LL)
and uninterrupted power supplies (UPS). Load-leveling devices allow utilities
to store power generated during times of low demand so that it is available
in times of high demand. This allows utilities to meet growth in demand
without building expensive new plants. Uninterrupted power supply devices
are important to manufacturers, hospitals, and others who need to guard
against unexpected interruptions in power supply.
The centerpiece of
the Dow-UT project was to combine the techniques of resin transfer molding
(RTM) and polar weaving in the construction of flywheel rotors. Polar
weaving would be used to fabricate material with a continuous woven structure;
the RTM process would be used to create the finished rotor from this material.
Composite flywheel
rotors had previously been fabricated using a process called filament
winding: fibers were woven into flat sheets, treated with epoxy resin,
wrapped together, and compressed to create forms. In contrast, polar weaving
produces a continuous helix of woven fibers, similar in form to a SlinkyTM
toy. This helical weave increases radial tensile strength, that is, the
capacity of the material to resist centrifugal forces pulling it away
from the center. Lack of radial tensile strength had previously constrained
efforts to develop a composite flywheel capable of increased rotational
speed.
Resin transfer molding
(RTM) involves the use of a vacuum mold into which resin is injected under
pressure. The resin permeates the woven structure, which is at the same
time shaped under pressure. The resin gels and cures to create a solid
piece. By achieving the shaping and curing function in the same step,
RTM reduced the cost of the fabrication process. In addition, since RTM
applies pressure through the resin rather than through mechanical means,
the piece is shaped continuously, which eliminates the need for expensive
secondary machining. Production costs are thus considerably reduced.
Achievements
The combination of polar weave and RTM techniques allowed Dow-UT to use
cheaper materials to create equally strong flywheel rotors. Dow-UT used
fibers made from glass mixed with graphite, at a cost of about $1 per
pound, a considerable cost reduction from graphite fibers at $7 per pound.(3)
Although the individual composite (glass and graphite) fibers
are weaker than all-graphite fibers, polar weave and RTM allow for the
creation of rotors or other parts with the requisite strength.
Dow-UT demonstrated
flywheels in the ATP project that were better in four ways. First, they
could spin faster. The new flywheels were tested at speeds of up to 40,000
RPM, a 25 percent improvement over older flywheel technology. Second,
they had improved lifetimes. Fatigue resistance was improved by a factor
of ten compared to older flywheel technology.(4)
Third, production costs per pound were cut in half by the new
fabrication techniques, to less than $20. Fourth, the improved flywheels
were lighter. The reduced weight and faster spinning speed increase the
energy density, that is, the amount of energy stored per unit weight.
Another useful development
from this project was a software package that enabled better computer
design of the composite flywheel rotors. This software allows engineers
to model the performance of flywheel rotors fabricated with different
types of fibers and fiber architectures (the amount of fiber used in hoop
and radial directions). This tool should speed future design and development
work.
Project Stopped Early
After the project had been underway for less than a year, the automakers
revised their cost targets for EV flywheel systems sharply downward. The
revised maximum cost required by the industry was below $600 for a complete
system, which included not only the rotor, but also the motor/generator,
magnetic bearings, vacuum system, housing, and additional elements. This
figure was not much more than the actual cost of the fiber for the rotor
alone. The most advanced system envisioned by the project would cost more
than $1,800. Dow-UT determined that these new cost targets could not be
met with existing technology, and discontinued its work on rotors for
automotive flywheels. The ATP concurred, and by mutual agreement, the
project was stopped after nine months and $99,035 in ATP outlays and $155,072
in company costs.
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Project
Highlights
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PROJECT:
To develop a cost effective means of fabricating strong lightweight
flywheel rotors from composite materials primarily for use in hybrid
electric vehicles, and also potentially for other applications.
Duration: 8/5/1995 8/15/98
ATP Number: 94-02-0041
FUNDING (in
thousands):
| ATP |
$ 99
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39%
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| Company |
155
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61%
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| Total |
$254
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ACCOMPLISHMENTS:
Dow-UT met the originally targeted project goals for cost of production
that were based on estimates from the automakers. During the course
of the project, the automaker revised their cost targets substantially
downward. Based on its progress to date, Dow-UT determined that
the new auto industry cost requirements could not be met and chose
not be met and chose not to continue the project. Consequently,
the project and ATP funding ended after only nine months. The project
nevertheless made substantial accomplishments. A combination of
polar weaving and resin transfer molding (RTM) techniques in the
construction of composite flywheel rotors allowed Dow-UT to cut
the cost producing flywheel rotors in half. Additionally, the many
during an after the award period displayed other accomplishments:
- developed
a software package that enables better computer design of the
composite flywheel rotors;
- contracted
with NASA and the U.S. Air Force to develop a composite flywheel
for aerospace use;
- partnered
with SatCon Corporation, a flywheel assembler, on the development
of uninterrupted power supplies (UPS) for satellites;
- presented
a paper and research results on the 1997 and 1998 NASA/USAF Flywheel
Conferences; and
- received
a patent, "Energy Storage Flywheel Device" (No. 5,590,569:
files 6/7/1995, granted 1/7/1997).
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COMMERCIALIZATION
STATUS:
The automotive industry requires a total flywheel system that costs
below $600, while the most advanced system envisioned by this project
would cost more than $1,800. The upward revision in the cost requirement
by automakers stalled development work on flywheel systems for automotive
applications. Dow-UT determined that these new cost targets would
not be met with the technology under development, and therefore,
asked that the ATP project terminated and discontinued its work
on rotors for automotive flywheels.
OUTLOOK:
Under contract with NASA and the U.S. Air Force, Dow-UT has found
an alternative application in which to use its knowledge gains developed
within the ATP project The company's state-of-the-art materials
an manufacturing processes for flywheel technology have shown promise
in space applications, such as for uninterruptible power supply
(UPS) for satellites, where cost requirements are not as restrictive
as those of the auto industry. The outlook is promising for use
of the technology in aerospace applications. Auto use appears delayed.
COMPANY:
Dow-United Technologies Composite, Inc.
KN Westland Aerospace, Inc.
15 Sterling Drive
Wallingford, CT 06492-1843
Contact:
John Gendreau
Phone: (202) 949-5145
Number of employees: 3 at project start, 14 at the end of
1997
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Remaining Technical
Obstacles to the Commercialization of Automotive Flywheel Systems
In addition to cost barriers, flywheels still face many technical hurdles.
There are the challenges of maintaining rotor integrity over longer lifetimes,
containing the flywheel in case of failure, and dissipating friction in
the bearings. Vacuum containment and magnetic bearing advancements, which
increase lifetimes and reduce friction, will probably be required before
flywheels come into widespread automotive use. The safety question also
hampers flywheel use. For example, the failure of a 1 kWh flywheel (the
size required for automotive applications) would release enough energy
to blow a 2,500-pound car 1,000 feet into the air.(5)
The safety risks associated with fast spinning rotors were pointed
up by an industrial accident during product tests. The accident highlighted
the need to improve containment structures.
Flywheel Technology
for Other Applications
Flywheel technology remains promising for applications other than vehicles.
One promising potential application is power storage for satellites. Space
applications demand extremely low weights since each pound costs more
than $1,000 to send into orbit. Light, all-graphite rotors are ideal for
the expanding space-use market where material costs are less important
than weight factors.
Following the termination
of the ATP project, Dow-UT began a contract with NASA and the U.S. Air
Force to develop a composite flywheel for aerospace use. Dow-UT worked
with SatCon Corporation, a flywheel assembler, on the development of uninterrupted
power supplies (UPS) for satellites. SatCon has aggressively moved into
the space market, creating a new subsidiary, Beacon Corporation, to manufacture
and distribute flywheel energy systems.(6)
This work continued following the acquisition of Dow-UT by GKN
Westland Aerospace in the fall of 1998. Researchers that were formerly
with Dow-UT have been able to apply the combined use of polar weaving
and RTM to the manufacture of rotors from all-graphite fibers for these
aerospace purposes. Thus, although the projects automotive goals
were not met, advances have proved commercially useful in other specialized
applications higher up the cost curve.
Knowledge Spillover
Benefits
Dow-UT received a patent for manufacturing the composite rotor that it
developed during the ATP project.(7)
In the aerospace field, Dow-UT was among the invited industry
guests to present a paper and results at the 1997 and 1998 NASA/USAF Flywheel
Conferences. The combined RTM/polar weaving method developed by the project
has been applied to the fabrication of rotors for flywheel systems used
as uninterrupted power supplies for satellites.
Sidetracked, but Not
Off Track
Dow-UTs effort to develop composite flywheel rotors was guided by
the originally estimated technical and cost requirements of automakers
for flywheel systems to be used in hybrid electric vehicles. Dow-UT was
on track to meet the originally anticipated requirements. When the cost
target was revised sharply lower, however, Dow-UT decided it could not
meet the automakers more demanding requirements with the technology
it was developing. Consequently, it decided to terminate the project early,
with ATPs concurrence. Cost effectiveness of flywheels for automobile
use was not reached.
Process technology
that was developed by Dow-UT researchers in the ATP project has since
found another application: the fabrication of flywheel rotors for flywheel
systems used as uninterrupted power supplies for satellites. In this application,
the cost requirements are less demanding. Further progress in developing
flywheel technology in the aerospace area may later feed back to applications
in the automotive industry.
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1. The
analysis identifies the distribution of terminated project by reason for
termination, while providing anonymity to the companies in order to preserve
their rights regarding proprietary information.
2. After another company bought out Fiberite, Dow-UT
undertook the development of the polar weaving technology in-house.
3. High Performance Composites, March/April 1996, p.
25; Cheaper Composite Flywheels, Mechanical Engineering, June
1996
4. Battery and EV Technology, June 1996, p. 25.
5. High-Performance Composites, March/April 1996, p.25
6. Battery and EV Technology, July 1997.
7. Energy Storage Flywheel Device, patent number
5590569, January 7, 1997.
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Date created: April
2002
Last updated:
April 12, 2005
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