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Equipment
Reliability Institute
ERI News - your reliability newsletter
February, 2002
- volume 6
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Are
you a test engineer? Are you involved in shock and vibration testing
and measurement? I think you'll be benefit from hearing about the
new fifth edition of the famed Shock & Vibration
Handbook. I'm reviewing it in this issue.
Do you measure static or dynamic deformations
(changes in dimension - strain)? Quite likely you bond strain gages
to the structures you investigate. Larry Shull
warns readers about some of the ways to get wrong data.
The reader's question: How
do I test a shelf item? We invite our readers to keep on sending
their questions. One of our specialists or Wayne
will respond to them.
Best wishes,
Wayne
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Reliable
Strain Gage Installation
by Larry Shull
During the heyday (1960-1973) of the Saturn/Apollo
Program there was a term used and understood by all involved, FIVE
NINE RELIABILITY. Interpretation: each and every part on any component
of the entire Saturn assembly was proven to be 99.999% reliable
under full scale loading conditions. This, in effect, means that
99,999 times out of 100,000 tests each part had functioned as designed.
Of course, every part was not tested that many times, but its performance
was proven to meet these standards. This proven reliability was
the major reason for the superb performance of the entire Apollo
program. Quality control was about hardware, not about paper work
as it is today.
Five nine reliability is a thing of the
past, based on material and equipment available on today's markets.
Automobiles must be worked on before they can be driven off the
show room floor; new toasters, out of the box, fail to perform when
plugged in for the first time; buy five shirts off the rack, when
opened at home four have defects, some serious enough to return
the shirt. This holds true for almost anything on the market, mechanical,
electronic, material, and so on. We have generations of younger
people who accept this as the "norm", never having experienced anything
better. Poor performance is expected from almost any endeavor. This
attitude is carried to the test beds of mechanical items. Failure
of sensors used to determine performance is shrugged off as "nothing
unusual!" If a strain gage, or other type transducer fails to provide
the expected answer the sensor is assumed "bad".
Until the introduction of the computer into
the mechanical test world, the strain gage was considered the most
precise component in any measurement system. The manufacture of
these tiny sensors was tightly controlled and installation on a
test item was a thing of great pride for the technicians involved.
Strain gages have performed flawlessly in many different environments,
static, dynamic, deep cryogenic temperatures, outer space, and so
on infinitum. The secret of this success has always been the great
care taken in selecting the proper gage, adhesive, protective coatings,
solder, wiring, and most important, installation techniques. Properly
installed strain gages will survive almost any environment short
of catastrophic hardware failure directly beneath the gage itself.
We
will not go into the quality control during the manufacturing of
strain gages. It will suffice to say that inspection is 100% visual,
and a resistance check. Other parameters are determined statistically,
under tight control. Every strain gage sold is guaranteed out of
the package. What happens to it during or after installation is
the user's responsibility.
Reliability of the strain gage is directly
related to techniques used to install each gage. There are no short
cuts. Certain rules apply to each individual gage as it is removed
from the package, prepared for bonding, positioned, clamped and
cured.
Preparation of the surface where the gage
is to be bonded must meet certain standards to assure a good bond.
It must be smooth, free of any scratches, nicks, other disfiguration,
and almost medicinally sterile. The adhesive to be used must be
fresh, properly mixed and settled. It should be applied to both
the bond side of the gage, as well as the position where the gage
is to be located. Air dry criteria must be met before the gage is
placed in position. If a strip of tape is used to handle each gage
it must be of a certain quality; any old tape will not do. There
are other similar rules that must be observed if the gage system
is to perform as expected. Violations, even minor things, can lead
to disastrous results.
As an example, at one time a very good technician
decided he would concoct his own solder flux, and did so with out
telling anyone. Things went well as long as his gages were used
within a short time after installation. Came the time the gaged
part was put in storage for about six months, waiting for test equipment
to be fabricated. Eventually all was ready, the test item was on
the test pad, strain gages and other sensors connected and checked.
At the time of installation all gages, approximately 300, had checked
out at the normal 350 Ohms. Now these values varied from zero to
infinity, and anything in between. This is a classic example of
what corrosive flux does to electrical circuits over time.
Hundreds of similar examples could be cited,
extending over the past 30 years or so. Inexperienced and untrained
personnel, trying to install gages have accounted for a good number
of such instances. Excellent technicians have also contributed,
as in the example, trying short cuts, not paying attention, and
using chemicals on new materials, without first checking for compatibility.
Some nstallation Procedures are absolutely wrong, but must be adhered
to because that is what Quality Assurance uses to certify the situation.
There is another situation that arises from
the instrumentation used to condition and record the information
from a strain gage. A properly installed gage will respond, almost
to the molecular motion of the atoms, to anything that occurs in
the surface immediately beneath the gage grid, integrating the motion
over the grid length. No motion outside this area will be monitored.
The gage will respond to any strain, be it axial, bending, torsion,
temperature effects in the gage, thermocouple effects in the solder
joints, magnetic effects on gage and wiring, and so on. All of these
things cause changes of resistance in the gage, which has no way
of knowing what, where, when, why, and who caused the change. Methods
have been devised to sort things out, canceling unwanted information,
while enhancing wanted information. To do this type compensation
requires considerable knowledge of, not only the gage behavior,
but how the part will behave under given loads, what temperatures
are expected, and any other effects mentioned. A thorough and complete
understanding of the Wheatstone bridge is necessary. Thus, strain
gage systems can be designed and installed that will produce valid
information required by Engineering, while eliminating unwanted
signals. This, as a rule, requires four (4) gages to make one measurement.
Such methods were used successfully for
years, with excellent results. With the introduction of the computer
into the mechanical test world, engineers wrongly decided that arithmetic
will provide all the right answers without "wasting" the extra gages.
Computing bridge circuits are rarely used today, especially in stress
analysis where they are badly needed. The problem, as mentioned
above, is that the gage responds to any and all environmental changes.
Some of these can be sorted out by using sum and difference methods
as would be the case for axial and bending loads applied to a part
having at least three gages located around the part at a particular
station. However, if the test item is a cylindrical vessel, loaded
in compression, and gages are located only on the outside, or only
the inside, bending strains can directly cancel compression strains
under the gage. Another situation is caused by strain gage temperature
changes during mechanical loading of the item. Strain gages are
excellent temperature sensors, and unless this is considered during
data reduction, serious errors can occur.
The point of this short dissertation is
that strain gages, properly installed, are five nine reliable in
any situation short of catastrophic failure of the test item immediately
beneath the gage grid. Poor installations result in inexact data
and failed gages. Not understanding gage behavior in all environments
can result in improper data interpretation. Not accounting for temperature,
or other extraneous effects, can also lead to misinterpretation.
The strain gage itself is rarely at fault.
Larry Shull is the president of Strain
Gage Advice, Inc. and also one of ERI's specialists. Please click here to access his bio. Also, Larry provides
a short course in Engineering Applications of Strain Gages.
Click here to see the course outline.
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Fifth Edition
- Harris' Shock And Vibration Handbook
by Wayne Tustin
This fifth edition supersedes the previous four editions,
the first having appeared in 1961 and subsequent editions in 1976,
1988 and 1996. Gaps between editions have been 15, 12, 8 and now
6 years; one might infer that changes in dynamics are occurring
more frequently as the decades pass. This edition is coauthored
and edited by Allan G. Piersol of Woodland Hills, California.
My
purpose in writing this review is to honor the editors/organizers/compilers
(as well as the authors). What a monumental task, to coordinate
the work of 53 authors! Pages are only numbered within sections.
They add up to 1416 pages, including a 231-page index.
Chapters 1 through 9 deal with basic theory and have
only minor editorial changes, additional references and/or revised
references. At least minor changes were made in all other Chapters.
Major changes to individual Chapters are indicated in the Chapter
listing which follows. Some of the Chapters by deceased authors
were revised and updated by the editors, retaining author credits
in recognition of the authors' significant contributions to shock
and vibration technology.
| 1. |
Introduction to the Handbook, by Cyril M. Harris,
27 pp
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| 2. |
Basic Vibration Theory, by
Ralph E. Blake, 32 pp |
| 3. |
Vibration of a Resiliently Supported Rigid Body,
by Harry Himelblau and Sheldon Rubin, 56 pp
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| 4. |
Nonlinear Vibration, by Fredric
Ehrich and H. Norman Abramson, 45 pp |
| 5. |
Self-Excited Vibration, by
Fredric Ehrich, 25 pp |
| 6. |
Dynamic Vibration Absorbers
and Auxiliary Mass Dampers, by F. Everett Reed, 42 pp |
| 7. |
Vibration of Systems having Distributed Mass
and Elasticity, by William F. Stokey, 50 pp
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| 8. |
Transient Response to Step
and Pulse Functions, by Robert S. Ayre, 59 pp |
| 9. |
Effect of Impact on Structures,
by William H. Hoppman II, 13 pp |
| 10. |
Mechanical Impedance, by
Elmer L. Hixson, 14 pp, major revisions by Hixson |
| 11. |
Statistical Methods for Analyzing
Vibrating Systems, by Richard G. DeJong, 32 pp |
| 12. |
Vibration Transducers, by Anthony S. Chu, 41
pp
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| 13. |
Vibration Measurement Instrumentation,
by Robert B. Randall, 17 pp |
| 14. |
Vibration Analyzers and Their
Use, by Robert B. Randall, 42 pp |
| 15. |
Measurement Techniques, by
Cyril M. Harris, 23 pp |
| 16. |
Condition Monitoring of Machinery,
by Joelle Courrech and Ronald L. Eshleman, 25 pp, major revisions
by Courrech and Eshleman |
| 17. |
Strain-Gage Instrumentation, by Earl J. Wilson,
15 pp
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| 18. |
Calibration of Pickups, by
M. Roman Serbyn and Jeffrey Dosch, 28 pp |
| 19. |
Shock and Vibration Standards,
by David J. Evans and Henry C. Pusey, 8 pp, completely rewritten
with new authors |
| 20. |
Test Criteria and Specifications,
by Allan G. Piersol, 20 pp |
| 21. |
Experimental Modal Analysis,
by Randall J. Allemang and Daviod L. Brown, 72 pp |
| 22. |
Concepts in Vibration Data Analysis, by Allan
G. Piersol, 28 pp, completely rewritten with new author
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| 23. |
Concepts in Shock Data Analysis,
by Sheldon Rubin, 26 pp, major revisions by Rubin of obsolete
or redundant material |
| 24. |
Vibration of Structures Induced
by Ground Motion, by William J. Hall, 22 pp |
| 25. |
Vibration Testing Machines,
by David O. Smallwood, 22 pp |
| 26. |
Part I, Shock Testing Machines,
by Richard H. Chalmers, 14 pp 26. Part II, Pyroshock Testing,
by Neil T. Davie and Vesta I. Bateman, 18 pp |
| 27. |
Application of Digital Computers, by Marcos A.
Underwood, 36 pp, completely rewritten with new author
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| 28. |
Part I, Matrix Methods of
Analysis, by Stephen H. Crandall and Robert B. McCalley, Jr.,
27 pp 28. Part II, Finite Element Models, by Robert N. Coppolino,
24 pp, completely rewritten with new author |
| 29. |
Part I, Vibration of Structures
Induced by Fluid Flow, by Robert D. Blevins, 20 pp 29. Part
II, Vibration of Structures Induced by Wind, by Alan G. Davenport
and Milos Novak, 25 pp 29. Part III, Vibration of Structures
Induced by Sound, by John F. Wilby, 20 pp, new material, not
in previous edition |
| 30. |
Theory of Vibration Isolation,
by Charles E. Crede and Jerome E. Ruzicka, 43 pp, major deletions
of obsolete or redundant material |
| 31. |
Theory of Shock Isolation,
by R. E. Newton, 37 pp |
| 32. |
Shock and Vibration Isolators and Isolation Systems,
by Romulus H. Racca and Cyril M. Harris, 41 pp
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| 33. |
Mechanical Properties of
Rubber, by Ronald J. Schaefer, 18 pp |
| 34. |
Engineering Properties of
Metals, by James E. Stallmeyer, 22 pp |
| 35. |
Engineering Properties of
Composites, by Keith T. Kedward, 31 pp, new material, not in
previous edition |
| 36. |
Material Damping and Slip
Damping, by Lawrence E. Goodman, 30 pp |
| 37. |
Applied Damping Treatments, by David I. G. Jones,
22 pp
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| 38. |
Torsional Vibration in Reciprocating
and Rotating Machines, by Ronald J. Eshleman, 33 pp, major deletions
of obsolete or redundant material |
| 39. |
Part I, Balancing of Rotating
Machinery, by Douglas G. Stadelbauer, 35 pp |
| 39. |
Part II, Shaft Misalignment
of Rotating Machinery, by John D. Pietrowski, 4 pp |
| 40. |
Machine-Tool Vibration, by
Eugene I. Rivin, 22 pp |
| 41. |
Equipment Design, by Karl
A. Sweitzer, Charles A. Hull and Allan G. Piersol, 28 pp, completely
rewritten with new authors. This chapter replaces Chapters 42
and 43 of the previous edition. Chapter 41 in the previous edition
("Package Engineering") has been deleted. |
| 42. |
Effects of Shock and Vibration
on Humans, by Henning E. von Gierke and Anthony J. Brammer,
61 pp, major revisions by von Gierke and Brammer |
I'm sure your favorite engineering bookstore can obtain
the Handbook for you. Or send an e-mail to customer.service@mcgraw-hill.com.
Or FAX: the McGraw-Hill Bookstore Attn: Mail Order Department, 212-512-4105.
Ask for: Harris' Shock & Vibration Handbook 5/e ISBN: 0071370811
$150.00.
On a personal note, I had the honor and pleasure of
knowing Charles E. "Charlie" Crede in New England in the 'fifties
and later in Southern California in the early 'sixties. In 1962,
on Charlie's recommendation, I invested in the three-volume Harris
& Crede Edition 1. Charlie's autograph (in Volume 1) is dated
October 1962. Unfortunately, Charlie died shortly thereafter. Fast
forward 22 years. I carried that Volume 1 to a New York City meeting
with Dr. Cyril M. Harris who, on September 16, 1984, added his autograph.
Now, treasurers of first editions, what am I offered?
Wayne and publisher Eve Mattingley hope to meet many
TEST readers at the Annual Technical Meeting of the Institute of
Environmental Sciences and Technology, April 28 to May 1, 2002,
at Anaheim, California. Wayne will convene a meeting of Working
Group DTE013 on "Vibration and Shock Test Fixturing", Sunday, April
28 at 3 pm, location to be determined. On May 1, Wayne will speak
on "Planning your Vibration/Shock Test Facility". That is part of
chairman Jeff Schutt's session on "Test Facilities". Also on May
1, Wayne will co-chair (with Karl-Friedrich Ziegahn from Germany)
a session on "Test Methods". Details of the IEST meeting may be
found at http://www.iest.org/estech/estech.htm.
Wayne Tustin, ERI's president,
can be reached at tustin@equipment-reliability.com
or at 805/564-1260.
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Questions
our readers have asked...
This section of our newsletter was created
for you, reader! Feel free to send questions or suggestions to the
webmaster.
They will be either responded by Wayne Tustin or forwarded to one
of our specialists.
Here is the question for this issue:
Q: How do I test a shelf item? My product
is never attached in service, as are units that are bolted to aircraft,
to missiles, to ships, to automobiles. My product simply rests on
a desk or a shelf. How will I attach it for a vibration or shock
test?
A: Your only recourse is to clamp your product
onto the vibrating table of a shaker or onto the platform of a shock
test machine. See Figure 1.

Fig 1 - Typical ESS Clamping Fixture
Often the "clamped to" element is an intermediate aluminum
or magnesium flat plate, perhaps an inch thick, which in turn is
bolted to your shaker or shock test machine. Why? Because the existing
mounting points on your shaker or shock test machine are probably
not at the locations you need for your particular DUTs (devices
under test). You will need to drill and tap holes, typically 3/8-24,
at appropriate locations close to where the DUTs will be located.
The vertical members, Figure 1, can be several suitable
lengths of "running thread". Cut these from 3/8-24 or other threaded
rod . Tighten a 3/8-24 nut on each vertical member, atop the lower
horizontal bar (if you use it - see later note) so that the lower
bar and vertical member remain attached to the intermediate plate.
The horizontal members, Figure 1, might be ½ inch thick
x 1 inch wide bar stock. Whereas Figure 1 shows only one overhead
"holdown" bar, larger DUTs might require two overhead bars. If the
bottom surfaces of your DUTs can lay flat on your intermediate plate,
you might not require the lower bars.
Atop the "holdown" bar, tighten 3/8-24 or other nuts,
so that the DUTs don't move while the test is underway.
Wayne Tustin, ERI's president,
can be reached at tustin@equipment-reliability.com
or at 805/564-1260.
(back to the top)
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Last chance
to enroll!
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Wayne's Fundamentals of Vibration and Shock Measurement is happening
next Feb 11-13, in Santa Barbara, California. Registration is still
opened until February 10. Hurry up! Get more details about this
course here or send us an e-mail
with your questions.
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Contaminants
and Moisture can disrupt your electronics
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David Douthit will teach "Contaminants and Moisture can disrupt
your electronics" at Santa Barbara, California, next August 26-28.
The course provides details about the root causes of many poorly
understood electronic failures. The chemistry encountered in many
end-use environments (and in some manufacturing environments) will
be covered at length. We will discuss sources of contamination and
the effects of that contamination on electronic systems. This understanding
will enable participants to create more complete and accurate testing
protocols and better estimating long-term reliability of new electronic
designs, materials and processes. This understanding will also help
organizations to troubleshoot production problems and field problems
with existing electronic designs, materials and processes. Click here to get more information about this course.
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New date for Optimizing Electronic Circuit Card course
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John Starr, a specialist from ERI, will teach "Electronic Circuit
Cards - Applied Vibration" in August 19-21, 2002. Click
here to register for the course. |
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Vibration and Shock courses coming up
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Wayne Tustin will teach the following short courses
in vibration and shock measurement, analysis, calibration, testing,
HALT, ESS and HASS:
Santa Barbara, California, February 11-13, 2002
Huntsville, Alabama,
April 2-4, 2002
Livonia, Michigan,
April 10-12, 2002
Baltimore, Maryland,
April 15-17, 2002
Newport, Rhode Island, May 22-24, 2002
Santa Barbara, California,
August 12-14, 2002
Additional courses:
Montreal, Quebec, Canada,
September 25-27, 2002
Billerica (Boston), Massachusetts,
October 7-9, 2002
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New web
sites coming up
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ERI's web sites are being
redesigned to offer better and faster information for you. We are
also creating new features that will provide more services to our
readers and, for the first time, the opportunity to advertise on
both sites and at ERI News - your reliability newsletter. Stay tuned!
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Message
Board
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One of the new features the site Vibration and Shock will provide
soon is a message board. You will be able to post your message at
the board and someone who shares your interest will answer it. Have
you a new idea? Did it come to you while you were conducting a test?
Have you observed something you feel is interesting - and will you
share it with others? Do you wish to "try out" a conclusion on another
person? Or do you just want to share some information? There will
be many ways to explore the up coming message board. Stay tuned!
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Announcements
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Fixture group to meet
The IEST (Institute of Environmental Sciences & Technology)
Working Group DTE013 will meet at the Disneyland Hotel from 3:00-4:00
pm on Sunday, April 28, 2002. Readers involved with vibration and/or
shock testing, attending the IEST annual technical meeting at Anaheim,
CA, are invited.
The 20th Aerospace Testing
Seminar
Don't miss this seminar next March 26-28, at the Manhattan Beach
Marriott, Manhattan Beach, California. Our specialists Chuck Wright
and Lee Smith will be presenting, respectvely, "Update on the Test
Effectiveness of Systems Level Thermal Vacuum Testing" and "Optimization
of End-to-End Pyrotechnic Data Processing at the Boeing Space &
Defense System Laboratories". If you want to know more about
our specialists, click here. If you want to read more about their
papers, click
here, then click on abstracts and go to sessions 2 and 5 (you
will need Acrobat Reader to see the pdf document).
Wayne's COTS presentation
If you did not have the chance to be at the COTS San Diego event
or if you were there and would like to have access to Wayne's presentation,
go to ERI's
web site to see it.
Fuel Cell Technology
Do any of our readers know of someone who can
teach a beginner-level short course in fuel cell technology, particularly
(but not exclusively) for automotive applications? Please send
us the person's name, address, phone, e-mail address, etc. Thanks!
Seeking teacher
Someone once told me that the number of pressure sensors sold is
10X the number of accelerometers sold. Whatever the ratio, it is
certainly greater than 1:1. ERI is seeking someone to teach short
courses about dynamic and static pressure measurements and calibration.
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Think about |
Don't Let Your Career Depend Upon Your Employer
Do you need some specialized, career-advancing training? And been
told by your boss that "There's no money in our training budget."?
Your career and your lifetime earnings are too valuable to let that
deter you. Tell (don't ask) your boss that you will be away from ____
to ____, participating in that training, at your own expense. THAT
will get his attention + the attention of higher management. |
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Check
our Glossary |
Check our Vibration
and Shock Glossary. We have just added new words and their definitions.
This list evolved from Wayne's 50 years of work experience and it
is constantly updated. |
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Contact
information
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ERI - Equipment Reliability Institute
1520 Santa Rosa Av.
Santa Barbara - CA - 93109
Tel/Fax: (805) 564-1260
Wayne Tustin tustin@equipment-
reliability.com
Webmaster webmaster@equipment
- reliability.com
Web sites
http://www.equipment-
reliability.com
http://vibrationand
shock.com
Copyright © 2000-2001 Equipment Reliability Institute.
All rights reserved.
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