SBIR-STTR Award

Fatigue Life Improvement with Surface Treatments other than Shot Peening
Award last edited on: 10/26/2018

Sponsored Program
SBIR
Awarding Agency
DOD : Navy
Total Award Amount
$898,164
Award Phase
2
Solicitation Topic Code
N06-047
Principal Investigator
Brian L Garrison

Company Information

Lambda Technologies Inc (AKA: Lambda Research~Surface Enhancement Technologies)

3929 Virginia Avenue
Cincinnati, OH 45227
   (513) 561-0883
   info@lambdatechs.com
   www.lambdatechs.com
Location: Multiple
Congr. District: 02
County: Hamilton

Phase I

Contract Number: N68335-06-C-0201
Start Date: 4/6/2006    Completed: 8/15/2007
Phase I year
2006
Phase I Amount
$149,960
Risk of fatigue failure is the primary limitation on performance and life of rotorcraft and increases the cost of ownership by increasing maintenance and inspection costs. Shot peening is currently used to enhance fatigue life. However, shot peening does not produce a compressive layer deep enough to arrest a fatigue crack detectable with NDI methods. Laser shocking provides the necessary depth, but is expensive and introduces logistical problems. Low plasticity burnishing (LPB) has already been demonstrated to provide the required depth of compression to arrest detectable fatigue cracks. LPB is a practical shop floor technology currently in commercial production. The Phase I effort would demonstrate arrest of existing flaws and restoration of fatigue life in test coupons using robotic LPB processing. Phase II extends the effort to actual rotocraft dynamic components using roller tool designs to access fatigue critical features with robotic tool positioning. LPB processing of fatigue critical dynamic components will increase life and performance of rotorcraft, reduce the required inspection time costs, and improve aircraft safety and reliability

Benefit:
The primary benefit to NAVAIR of introducing LPB technology will be extended life and reduced cost of manufacturing fatigue critical rotorcraft components, improved time on wing and reducing maintenance and inspection costs and requirements, first for the V-22 program and then extending to other aircraft. Potential applications and commercial opportunities for low plasticity burnishing (LPB) as a means of improving the fatigue performance of aircraft dynamic components are vast. LPB is already approved by NAVAIR for application to the F404 engine LPC1 vanes and blades used on the AV-8 B Harrier to enhance fatigue performance and is in production mitigating fretting fatigue in titanium alloy hip implants. The anticipated market for LPB in aircraft structural and dynamic components is anticipated to approach $100M during the next decade.

Keywords:
Rotorcraft, Rotorcraft, high cycle fatigue (HCF), stress corrosion cracking (SCC), Low Plasticity Burnishing (LPB), foreign object damage (FOD), Fatigue

Phase II

Contract Number: N68335-07-C-0355
Start Date: 6/26/2007    Completed: 6/26/2009
Phase II year
2007
Phase II Amount
$748,204
Risk of fatigue failure is the primary limitation on the performance and life of rotorcraft components, and increases the cost of ownership by increasing maintenance and inspection costs. Low Plasticity Burnishing (LPB) has already been demonstrated to provide the required depth of compression to arrest detectable fatigue cracks and is a practical shop floor technology currently in commercial production. The Phase I effort demonstrated arrest of existing flaws and restoration of fatigue life in test coupons using robotic LPB processing. In Phase II, LPB will be applied to and tested on actual rotorcraft dynamic components using roller and ball tool designs to access fatigue critical components. The application of LPB will increase life and performance of rotorcraft, reduce the required inspection time costs, and improve aircraft safety and reliability.

Benefit:
The primary benefit to NAVAIR of introducing LPB technology will be extended life and reduced cost of manufacturing fatigue critical rotorcraft components, improved time on wing and reducing maintenance and inspection costs and requirements, first for the V-22 program and then extending to other aircraft. Potential applications and commercial opportunities for low plasticity burnishing (LPB) as a means of improving the fatigue performance of aircraft dynamic components are vast. LPB is already approved by NAVAIR for application to the F404 engine LPC1 vanes and blades used on the AV-8 B Harrier to enhance fatigue performance and is in production mitigating fretting fatigue in titanium alloy hip implants. The anticipated market for LPB in aircraft structural and dynamic components is anticipated to approach $100M during the next decade.

Keywords:
stress corrosion cracking (SCC), Low Plasticity Burnishing (LPB), foreign object damage (FOD), Rotorcraft, Fatigue , high cycle fatigue (HCF)