Back-Tension Drawing Process

Back-tension drawing, a novel drawing process and a manufacturing method capable of producing precise complex structural shapes, was successfully demonstrated. Rough extrusions of AISI 4340 steel were drawn to precise T sections with a web thickness of 40 mils. In Phase 1, a special hydraulic drawbe...

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Hauptverfasser: Kosinski, E J, Pickett, J J, Loewenstein, Paul
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Pickett, J J
Loewenstein, Paul
description Back-tension drawing, a novel drawing process and a manufacturing method capable of producing precise complex structural shapes, was successfully demonstrated. Rough extrusions of AISI 4340 steel were drawn to precise T sections with a web thickness of 40 mils. In Phase 1, a special hydraulic drawbench capable of independently exerting up to 25 tons of back-tension (back pull) force to a workpiece was designed, constructed, and operated. In Phase 2, comprehensive tests using AISI 1010 and AISI 4340 round steel bars were conducted to establish the relationship between the principal back-tension drawing variables. It was clearly demonstrated that back-tension is capable of greatly reducing the die stresses. In Phase 3, more than 200 drawing operations were performed on extruded AISI 4340 steel T sections. Steel T's having a height of 1 inch, a width of 2 inches, and section thicknesses varying between 0.080 and 0.090 inch were successfully drawn to 0.040 plus or minus .001 inch thickness. The as-drawn T's were straight with negligible bow, twist, or camber. In Phase 4, preliminary attempts were made to apply the process to 1-inch by 2-inch by 0.10-inch T shapes of the alloy Ti-6Al-4V. Back-tension stress levels of 70 to 80 percent of the material yield strength were required to control bow, twist, and camber in drawn sections. (Author) Errata sheet inserted.
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Rough extrusions of AISI 4340 steel were drawn to precise T sections with a web thickness of 40 mils. In Phase 1, a special hydraulic drawbench capable of independently exerting up to 25 tons of back-tension (back pull) force to a workpiece was designed, constructed, and operated. In Phase 2, comprehensive tests using AISI 1010 and AISI 4340 round steel bars were conducted to establish the relationship between the principal back-tension drawing variables. It was clearly demonstrated that back-tension is capable of greatly reducing the die stresses. In Phase 3, more than 200 drawing operations were performed on extruded AISI 4340 steel T sections. Steel T's having a height of 1 inch, a width of 2 inches, and section thicknesses varying between 0.080 and 0.090 inch were successfully drawn to 0.040 plus or minus .001 inch thickness. The as-drawn T's were straight with negligible bow, twist, or camber. In Phase 4, preliminary attempts were made to apply the process to 1-inch by 2-inch by 0.10-inch T shapes of the alloy Ti-6Al-4V. Back-tension stress levels of 70 to 80 percent of the material yield strength were required to control bow, twist, and camber in drawn sections. 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In Phase 4, preliminary attempts were made to apply the process to 1-inch by 2-inch by 0.10-inch T shapes of the alloy Ti-6Al-4V. Back-tension stress levels of 70 to 80 percent of the material yield strength were required to control bow, twist, and camber in drawn sections. (Author) Errata sheet inserted.</abstract><oa>free_for_read</oa></addata></record>
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source DTIC Technical Reports
subjects Aircraft
AIRFRAMES
ALUMINUM ALLOYS
BACK TENSION DRAWING
DIES
DRAWING(FORMING)
Fabrication Metallurgy
INDUSTRIAL EQUIPMENT
LUBRICANTS
MACHINE TOOLS
MANUFACTURING
STEEL
STEEL 1010
STEEL 4340
STRUCTURAL COMPONENTS
Structural Engineering and Building Technology
TITANIUM ALLOY 6AL 4V
TITANIUM ALLOYS
VANADIUM ALLOYS
title Back-Tension Drawing Process
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