CYBERNET SYSTEMS CORPORATION — Department of Defense SBIR Phase I: AF161-117

Description

ABSTRACT: Metallic high pressure compressor (HPC) blades are a critical component in all jet engines and can incur erosional and impact damage during normal operations. During an engine maintenance, repair, and overhaul (MRO) cycle, these blades are routinely removed from the engine, cleaned, inspected, and either repaired or replaced based on the type of damage and the repair capability available. A common repair technique is the use of high speed grinding to carefully blend out surface damage such as gouges, nicks, scratches, etc. primarily located on the leading and trailing edges of the blade. This is a time consuming and labor intensive process and is highly reliant on the skill level of the individual maintainer. There is a need for an improved process that can more quickly, reliably, accurately, and repeatably inspect and repair these blades. Cybernet specializes in improving such processes through the targeted application of automation. In the proposed effort, we will design and develop an automated workcell that can identify and categorize surface defects on HPC blades and then perform high speed grinding/blend repairs on these blades based on defect size and location.; BENEFIT: The proposed technology will create an automated system for inspecting and repair surface defects on high pressure compressor blades. This technology will support maintenance, repair, and overhaul of turbine engines for both military and commercial entities. It will lead to a significant increase in the quality and repeatability of the repair process while increasing the speed at which repairs can be conducted.