| This article was prepared by staff writers in collaboration with outside contributors. |
The U.S. armed forces rely on
the H-60 to carry troops, cargo, even electronic-jamming equipment. Variations
of the helicopter include Black Hawks, Pave Hawks, and Seahawks. The manufacturer,
Sikorsky Aircraft Corp., says more than 2,500 H-60s are in service with
the U.S. Army, Navy, Coast Guard, Air Force, and Marine Corps.
The Navy and Army have begun to equip the aircraft with sensors that will
monitor key moving parts to make the H-60 more reliable, and to get the
most out of each machine. Now, to make the system even smarter, the Navy
has enlisted a couple of engineering firms in upstate New York to create
intelligent software that one day may tell pilots in the air how much
longer their craft will fly.
Accelerometers can monitor gearboxes and drivetrains so that technical
teams on the ground can use the information to base maintenance decisions
on need rather than timetables. This program is called the Health and
Usage Monitoring System, or HUMS, an almost lighthearted acronym for military-speak
when you consider that it involves sensing vibration.
HUMS tells technicians "so far, so good" or "needs
fixing," as the case may be. But if a computer can reference incoming
information against predictive models, it can make a prognosis of a part's
remaining usefulness in terms of hours.
 |
| A predictive maintenance program
for the H-60 helicopter includes a model of a transmission gear. Highlight
colors show areas of maximum stress. |
According to the lead engineer on the modeling project, Greg Kacprzynski
of Impact Technologies LLC in Rochester, N.Y., "From day one, in
the absence of strong vibration, the system predicts life expectancy.
If vibration increases, the model calculates based on the new information."
According to Tony Ingraffea, a Cornell University professor who has been
brought in as a consultant, in the best-case scenario, computers on the
helicopters will give real-time feedback to pilots.
The engineers are modeling the spiral-bevel pinion gear in the helicopter's
intermediate gearbox, one of three transmissions that step down the thousands-per-minute
spin of the turbine to hundreds of rpm for the rotor.
William Hardman, diagnostic engineer at the Naval Air Systems Command
in Patuxent River, Md., assembled data from two sample gears, which he
had run to failure on test stands. In each test, a gear tooth was notched
to hasten crack initiation.
One gearbox was subjected to various loads "to capture what you
see in service," he said. A second started at 2,340 ft.-lbs. of
torque and continued to 2,000 (3,173 newton-meters easing to 2,711) after
damage became serious.
Gleason Corp.
of Rochester, N.Y., provided gear data and a model of three consecutive
teeth to cover the complete load cycle for any tooth. The model was translated
into an Ansys file, according to Avinash Sarlashkar, director of technology
at Impact. This software, from Ansys Inc. of Canonsburg, Pa., calculated
physical values and generated the finite-element mesh for analysis.
According to Sarlashkar, who with Brad Lamirand did much of the Ansys
work, simulations of crack propagation were done by Fracture Analysis
Consultants Inc., Ingraffea's consulting firm in Ithaca, N.Y. Ingraffea,
an ASME member, used a program called Franc-3D, developed by his research
group at the university, the Cornell Fracture Group.
So far, the researchers have deemed their models accurate in calculating
a crack length of about a half-inch, or 2 cm. Beyond that point, they
say, load-sharing factors that were not modeled may have come into play.
According to Sarlashkar, the project is in its second phase under a Small
Business Innovative Research grant, and the model is being adjusted to
match the test data more closely.
A crack in a gear tooth, whether it is accidental or intentional, will
produce vibration, Sarlashkar said. The challenge is to get the complex
events of gear failure to fit into a computer.
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