Wright Dialogue with Industry

July 20-21, 2011
Hope Hotel & Conference Center
Wright-Patterson Air Force Base, Dayton, Ohio

LSP Technologies is proud to attend again this year to discuss it’s laser peening process and services as well as it’s laser bond inspection process.

The following is taken from their website:
The Dayton Area Defense Contractors Association (DaytonDefense) will sponsor the fifth “Wright Dialogue with Industry” conference on July 20-21, 2011 at the Hope Hotel and Conference Center, Wright-Patterson AFB, OH.

The purpose of this conference is to help promote economic development activity among local defense contractors and Wright-Patterson Air Force Base. Please plan to attend this year’s Wright Dialogue with Industry to hear first-hand from key leaders of the Air Force Research Laboratory (AFRL) organization as they discuss both current and future business opportunities.  There will be opportunities throughout the day for more detailed breakout sessions where you can pose your particular questions to the Laboratory representatives. Throughout the course of the event, there will be time to network and discuss opportunities to do business in greater detail with AFRL.


3rd Int’l Conference on Laser Peening

Dr. Jeff Dulaney and Dr. Allen Clauer of LSP Technologies will attend the 3rd International Conference on Laser Peening & Related Phenomena on October 11-14, 2011 in Grand Cube Osaka, Japan.  Dr. Dulaney has joined the conference committee.

Dr. Dulaney will present on the topic Future Shock: Accelerating Technology, here is the abstract for his presentation.

It takes an enormous effort to take technology from a laboratory research environment to commercial use.  Laser Shock Processing (LSP) of the 1970s evolved into the commercial success known today as laser peening.  There are several variants of laser peening in use today, and others yet to be discovered, developed, and integrated into commercial use.  The study of the laser-generated shock waves, so critical to laser peening, will find commercial applicability beyond imparting compressive residual stress in metals.  Computer models, currently being used to support commercial applications development, will continue to improve and lead the way to new applications and uses.  Overlay materials will evolve to enhance the effectiveness of laser peening through the use of special materials and techniques.  In situ process controls and diagnostics will continue to be developed to provide real-time feedback for process control and continuous quality assurance as critical parts are being processed.  Advancement of laser peening systems will enable new and unexpected applications.

Dr. Clauer will present a paper he co-authored with Peter Gaydos entitled, “The Effect of Surface Treatments on Fatigue of Carburized X2M Steel.”   Here is the abstract for his paper.

“Carburized X2M specimens were tested in 3-point bending fatigue after having their surface treated with four different treatments both individually and in combination. The bend specimens were 102 mm x 34 x 8.5 mm, with the longitudinal edges of the tensile surface tapered. The surface treatments were Isotropic Surface Finishing (ISF), Low Stress Grinding (LSG), Shot Peening (SP) and Laser Shock Peening (LSP). The first three were also applied in combination with a follow-up LSP treatment, and also a combined ISF/SP/LSP treatment.
The results show that the fatigue strength increased with the type of surface treatment in the order of ISF, LSG, SP, LSP. The combination treatments produced fatigue strength equivalent to or slightly better than the LSP treatment alone.

These results will be discussed in the context of residual stress profiles and scanning electron microscopy of the surfaces and fracture surfaces. The observed modifications of the surfaces and comprehensive residual stresses lead to observable changes in crack initiation behavior.”

Other committee members from Ohio include:

Ramana V. Grandhi: Wright State University, USA

Kristina Langer: Wright-Patterson AFB, USA

S. R. Mannava: University of Cincinnati, USA

Visit the conference website to learn more.

11th International Conference on Shot Peening

South Bend, Indiana

September 12-15, 2011
Booth #111

LSP Technologies happily returns to the the International Conference on Shot Peening in 2011.  David Lahrman and Steve Dykes will be attending the conference and will be available to discuss and explain the laser peening process.  Stop by and visit with them in our booth (#111).  We hope you will stop to learn more about laser peening and how it can improve the fatigue properties of the parts you manufacture or maintain.

The excerpt below from the 11th International Conference on Shot Peening website highlights shot peening alternative or supplemental processes.

“Related mechanical surface treatments, such as deep rolling, laser peening, ultrasonic peening, combined processes and other cold work processes including compressive surface residual stresses, are within the scope of the conference, especially when compared to shot peening.”  To read more, visit the conference website:


The conference is hosted by Electronics, Inc. and The Shot Peener Magazine.  You can also visit the conference host’s websites for more information about them:




11th International Conference on Shot Peening

LSP Technologies will be a presenter.

September 12-15, 2011
South Bend, Indiana

ICSP-11 will be the 11th International Conference on Shot Peening. Related mechanical surface treatments – such as deep rolling, laser peening, ultrasonic peening, combined processes and other cold work processes inducing compressive surface residual stresses – are within the scope of the conference, especially when compared to shot peening. Shot Peening and related mechanical surface treatments have proved to be powerful instruments in enhancing the resistance of components to various kinds of stress-induced damage, particularly with respect to fatigue and corrosion damage. The service lives of a wide variety of structural components, irrespective of shape and dimensions, can be improved dramatically by shot peening. The commercial benefits of applying mechanical surface treatments are increasingly recognized, especially in the automotive and aerospace industries.


Pilger Dies – New Applications for Laser Peening

Exciting new applications continue to be found for LSP Technologies‘ LaserPeen® process! Pilger dies are used in the manufacture of high quality tubing for aerospace and nuclear applications. Pilgering is a cold forming process in which tubes are reduced in cross section by a combination of wall thinning and diameter reduction. Pilger die life is a major factor in the economics of the pilgering process.

Laser peening has been used to increase the life of pilger dies made of A2 tool steel by imparting compressive residual stresses to failure-prone areas of the dies.  Deep, high-magnitude compressive residual stresses were generated by LSP Technologies’ Laser Peening process, and the treated dies showed a significant increase in service life.

Click on the link below to download an article on laser peening of pilger dies.

Laser Peening of Pilger Dies

Laser Peening Proves to be the Solution for the B-1B Lancer’s Engine Failures

Beginning in 1991, the B-1B Lancer’s F101 engine began experiencing failures of titanium turbine blades due to foreign object damage (FOD) caused by ice and hard objects ingested into the engine. Chunks of blades that broke loose, in some cases, did irreparable damage to the rest of the engine. To avoid grounding the B-1 fleet, the Air Force required a manual inspection of all the fan blades before each flight. The time-consuming leading edge inspections involved rubbing the leading edge with cotton balls, cotton gloves and even dental floss. If a single snag was detected, the blade was replaced prior to the next flight. In 1994, over one million man-hours at a cost of $10 million per year were required to complete the engine inspections and keep the B-1 flying.

General Electric Aircraft Engines (GEAE) investigated an innovative technology, called Laser Shock Peening (or laser peening), as a potential solution to increase the durability of titanium fan blades and decrease the sensitivity to FOD. Laser peening uses a high energy laser pulse to create an intense shock wave into the surface of metal parts. The shock wave imparts deep compressive residual stresses, which greatly improve the blade’s fatigue properties and toughness.

The high cycle fatigue performance of laser peened blades is remarkable. Damage to an F101 blade can reduce the fatigue strength from about 75 ksi to less than 20 ksi, which is less than half of the design requirement. However, when laser peened blades are comparably damaged, they retain a fatigue strength of 75-100 ksi. Thus, laser peening restores the structural integrity of damaged fan blades! Sensitivity to FOD defects up to 1/4 of an inch in F101 blades was virtually eliminated.

In 1995, the USAF authorized the production development of laser peening, bringing this technology out of the lab and into a production environment. Jeff Dulaney founded LSP Technologies, Inc. (LSPT) in 1995 to provide laser peening equipment and services to industry and the U.S. military. By 1997, GEAE had proven the beneficial effects of laser peening and began production application to F101 blades, using four laser peening systems designed and built by LSPT.

Application of laser peening avoided over $59 million in blade replacement costs, secondary damage engine repair costs, and cost avoidance from airfoil failures. Avoiding catastrophic engine failures over the remaining life of the B-1B/F101 program is estimated to have saved another $40 million.

Due to this success, laser peening was applied to solve similar problems for the F110 engine blades for the F-16 Falcon, and the USAF estimates similar cost savings to the B-1B/F101 program.

LSP Technologies, Inc. has continued to improve LaserPeen® processing equipment and processing methods. With the newest generation of LaserPeen® processing equipment and the RapidCoater™ system for automating the coating overlays used in the process, LSPT has reduced the cost of LaserPeen® processing dramatically making the process affordable for many new applications!

Overall, the potential savings from laser peening are expected to easily approach $1 billion when calculating this impact over all engines in the Air Force fleet!

Laser Peening of Raptor Engine Components

Aerospace applications of laser peening include many gas turbine engine components, such as airfoils and integrally bladed rotors (IBRs) because of the enormous benefits of preventing fatigue failures and improving damage tolerance for these critical parts.


LaserPeen® Processing of Raptor IBRs Production at LSP Technologies, Inc.

Laser peening is a Production Process for the fan blades of GE Aviation’s F110 engine that powers the Falcon and Lancer.

– F110-GE-129 Engine (F-16 C/D Falcon)
– F110-GE-100 Engine (F-16 A/B Falcon)

– F101-GE-102 Engine (B-1B Lancer)

– Joint Strike Fighter

Production use of the laser peening on the fourth stage Integrally Bladed Rotor (IBR) for Pratt & Whitney’s F119-PW-100 engine, which powers the US Air Force’s F/A-22 Raptor, started at LSP Technologies in March 2003.  LaserPeen® processing increases the damage tolerance and enhances the fatigue performance of this IBR.


Applications of Laser Peening to Titanium Alloys

Originally presented at the ASME/JSME 2004 Pressure Vessels and Piping Division Conference, July 25-29, 2004.

Authored by David W. Sokol, Allan H. Clauer, Ravi Ravindranath.

Laser peening has been a commercial surface enhancement process for over six years, and has been gradually expanding the number of applications being laser peened in production ever since. LSP Technologies has been a major developer of the process and new applications for laser peening. It has developed production laser peening systems and innovative laser peening technology to increase throughput and reduce cost. Some of these production and technology developments will be discussed in this paper. Also, an evaluation of applying laser peening to increase the fretting fatigue resistance of titanium alloys, based on Ti-6Al-4V has been made. Included in this evaluation is the use of small spot laser peening to enable the processing of the inside of small, generally inaccessible areas such as the insides of holes and slots. Laser peening with either large or small spots dramatically increased the fretting fatigue life under both R=0.5 and R=0 fatigue conditions with three different contact pad pressures. Fretting fatigue life was increased by at least 25 times. Actual increases in fatigue life and fatigue strength could not be determined because most specimens ran to the runout life of 106 cycles without failure. The laser peening does not appear to affect the fretting behavior, but instead inhibits the initiation of fatigue cracks at the fretting cracks developed from the fretting process. The compressive residual stress from laser peening also would slow the growth rate of any fatigue crack that does eventually initiate at a fretting crack.

LSP Technologies has designed and built two production laser peening systems with the support of the Air Force Materials and Manufacturing Directorate. In 2003 it began production laser peening of an integrally bladed rotor for the F119 engine being built by Pratt & Whitney. To increase throughput and reduce the cost of the process, several technology improvements have also been developed and are being implemented into production. Among these is the RapidCoater™ system, which allows continuous processing of a part. Under a NAVAIR Phase II SBIR, LSP Technologies has investigated the effect of laser peening on fretting and fretting fatigue in dovetail slots. An outcome of this program is a laser peening system that enables the interior of dovetail slots to be accessed by laser peening. Because of the dovetail geometry, small spots (<1 mm in diameter) and underwater laser peening were used to treat the interior of the slots.

To download the entire article as a pdf: Applications of Laser Peening to Titanium Alloys