
Oil & Natural Gas Projects
Exploration and Production Technologies
Laser Peening to Improve Fatigue and Corrosion Resistance of Drilling Equipment
FEW 0118
Program
This project was funded through DOE's Natural Gas and Oil Technology Partnership
Program. The program establishes alliances that combine the resources and experience
of the Nation's petroleum industry with the capabilities of the National Laboratories
to expedite research, development, and demonstration of advanced technologies
for improved natural gas and oil recovery.
Project Goal
The project goal was to apply laser peening to oil and gas drilling hardware
and equipment, evaluate specific areas where cracking initiates, and treat and
test sample material and actual hardware.
Performers
Lawrence Livermore National Laboratory (LLNL)
Livermore, CA
University of California
Davis, CA
ExxonMobil Corp.
Irving, TX
Project Results
The first major project goal was to determine the achievable life improvement
of laser-peened welded four-point bend fatigue coupons compared with unpeened
coupons. It appears that laser peening could be used to induce compressive stresses
at selected regions inside and outside of the welded pipes.
Benefits
The laser-peened treated pipes in both welded and unwelded sections demonstrated
roughly four- to five-fold superiority over conventional methods.
Background
Laser peening is bursting on the scene as a process that treats the surface
of metal components to significantly reduce fatigue and stress corrosion cracking.
A commercially viable laser and process technology was transferred to industry
by LLNL in May 2002. This new technology immediately has been shown to bring
enormous benefit to the airline industry with respect to eliminating crack growth
in key jet engine components. It has solved a severe cracking problem that no
other technology was able to do. Since initial deployment, the laser process
has impacted over $25 billion worth of commercial jet aircraft by providing
longer life spans for expensive jet engine fan blades. The process extends the
useful lifetime of a $0.7 million set of fan blades by a factor of up to 20
times and converts a $500,000 engine teardown and rebuild every two months into
a once-per-two-year requirement. The benefit/cost ratio for aircraft components
is about 1000 to 1. The process now is expanding to solve an even broader group
of problems. This project looks at the application to oilfield hardware and
its potential for extending tool life.
Project Summary
The project tasks break out as:
Year 1, evaluation and sample treatment.
-Task 1, evaluation of gas and oil drilling mechanical failures. With experts
from the drilling industry, LLNL is to identify equipment mechanical failures
related to fatigue failure and stress corrosion and the materials and geometries
involved and propose approaches to reduce those failures by laser peening.
-Task 2, treatment of sample materials. Researchers are to treat sample materials
and complete fatigue and stress corrosion cracking tests to demonstrate the
value of laser peening.
-Task 3, estimate benefit/cost ratio. With improved sample lifetime by laser
peening, the lab can estimate value to the industry.
Year 2, treatment and testing of field components.
-Task 1, evaluation of actual components. LLNL is to evaluate how to treat
actual hardware and design appropriate tooling for handling the large, heavy
components.
-Task 2, treatment of actual components. Researchers are to build hardware
to handle field components and treat a representative number for field testing.
-Task 3, evaluation of treatment. Work is to proceed with drilling contractors
to test treated and untreated components to evaluate lifetime improvement
and benefit/cost ratio.
Year 3, commercial deployment.
-Task 1, transfer to commercial production. LLNL is responsible for transferring
treatment of components for initial commercial production treatment.
-Task 2, field testing. The project is to support field testing of commercially
treated components.
-Task 3, upgrades, final review, and final reporting. Researchers are to
upgrade any deficiencies resulting from field testing and complete final review
and testing of a commercialized process.
The first major project goal was to determine the achievable life improvement
of laser-peened welded four-point bend fatigue coupons compared with unpeened
coupons. ExxonMobil, using a coupon geometry defined by LLNL and the University
of California at Davis, CA (UCD), fabricated welded and base-metal coupons
from ASTM A656 Grade 1 steel. Initial testing of the welded coupons was completed.
Treating fatigue coupons with laser peening allows for an increase in applied
stress of more than 20 ksi, while maintaining the same fatigue life-an order-of-magnitude
increase in life at a particular test stress.
UCD has completed residual test models with matching geometries and planned
complementary residual stress measurement for small cylindrical geometries.
It appears that laser peening could be used to induce compressive stresses
at selected regions inside and outside of the welded pipes.
The next step laid out in the project plan was the application of laser peening
to cylindrical geometries. LLNL started with small, unwelded pipe sections
with laser peening and residual stress measurements, followed by axial fatigue
testing of small-diameter welded pipes, both laser peened and unpeened. The
final goal is laser peening and fatigue testing large diameter (on the order
of 18-inch) welded pipes. To date, ExxonMobil has provided several small-diameter
pieces of both welded and unwelded pipe, which LLNL laser peened using a helical
pattern. The laser-peened treated pipes in both welded and unwelded sections
demonstrate roughly a four- to five-fold increase in fatigue life.
Current Status (November 2005)
LLNL is to upgrade any deficiencies resulting from field testing and complete
final review and testing of a commercialized process in the final year of
the project.
Project Start: April 8, 2004
Project End: April 7, 2006
Anticipated DOE Contribution: $192,000
Performer Contribution: $0
Contact Information
NETL - Rhonda Jacobs (rhonda.jacobs@netl.doe.gov or 918-699-2037)
LLNL - Lloyd Hackel (hackel1@llnl.gov or 925-422-9009)
|