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Machinability of AF 1410 and AerMet 100 High Strength Steel

Award Information
Agency: Department of Defense
Branch: Navy
Contract: N/A
Agency Tracking Number: 26576
Amount: $726,818.00
Phase: Phase II
Program: SBIR
Solicitation Topic Code: N/A
Solicitation Number: N/A
Timeline
Solicitation Year: N/A
Award Year: 1996
Award Start Date (Proposal Award Date): N/A
Award End Date (Contract End Date): N/A
Small Business Information
7785 Foundation Drive, Suite One
Florence, KY 41042
United States
DUNS: N/A
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 John D. Christopher
 (606) 342-8215
Business Contact
Phone: () -
Research Institution
N/A
Abstract

The ultra-high strength steels, AF 1410 and AerMet 100, have improved fracture toughness and stress corrosion cracking resistance, desirable mechanical properties for naval aircraft landing gears. However, the absence of accurate machining information on the various operations necessary to manufacture these and other parts has limited the use of these alloys. Significant potential improvements of in-service life of aircraft components are not being realized, along with the resulting cost savings, because of the inability to forcast machining costs and productivity levels. Comprehensive, accurate machining data, when accompanied by a simple, easy-to-use cost analysis enables the potential contractor to competitively bid on manufacturing aircraft components, based on his equipment, scheduling, and personnel limitations. Current efficient techniques for machinability and grindability tests provide the maximum statistically validated results with a minimum investment of testing time. The combined relationship of cutting speed and feed on tool life or grinding wheel wear can usually be expressed as an equation which can support computer integrated manufacturing (CIM) systems. The author of this proposal has been producing machining and grinding information for various U.S. Government agencies and private industry since 1963.

* Information listed above is at the time of submission. *

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