US3187544A - Method for effecting a metal working process - Google Patents
Method for effecting a metal working process Download PDFInfo
- Publication number
- US3187544A US3187544A US214464A US21446462A US3187544A US 3187544 A US3187544 A US 3187544A US 214464 A US214464 A US 214464A US 21446462 A US21446462 A US 21446462A US 3187544 A US3187544 A US 3187544A
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- blank
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F3/00—Changing the physical structure of non-ferrous metals or alloys by special physical methods, e.g. treatment with neutrons
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S72/00—Metal deforming
- Y10S72/70—Deforming specified alloys or uncommon metal or bimetallic work
Definitions
- Another object is to disclose a method of forming sheet metal parts from metal sheets in which the elapsed time occurring between a heating and a forming operation thereon is minimized.
- Another object is to disclose a method of forming sheet metal parts from metal sheets in which oxidation thereof is minimized.
- FIGURE 1 is a graph showing the temperature losses encountered by an oven heated titanium alloy sheet in transferring the sheet from an oven to a forming area.
- FIG. 2 is a graph showing of the heating and cool- "ice ing of a titanium alloy sheet heated by radiation as disclosed herein, the radiantly heated sheet being of the same size and thickness and otherwise having the same characteristics as the oven heated sheet referred to in the description of FIGURE 1.
- This invention utilizes a radiant heat source (not shown) for the heating of titanium, magnesium and like sheet metal blanks which subsequently are to be formed into sheet metal parts.
- the blank sheets are first coated with a high temperature drawing compound so that they will absorb heat more readily.
- the blanks are then positioned in their exact forming attitude in a forming facility (not shown).
- the aforementioned radiant heat source comprises a plurality of quartz tube radiant heaters mounted in a suitable reflector, the number of heater tubes depending upon the size of the blanks to be heated.
- the reflector and heater tubes are new juxtapositioned above the blank so that the rays from the heater tubes are directed on the subject blank.
- the heater tubes are now energized and remain energized until such time as the temperature of the subject blank reaches a predetermined temperature.
- the reflector and heater tubes are then withdrawn from their juxtapositioned position above the blank allowing the forming operation to be effected without delay and with a minimum temperature loss.
- the curve in FIGURE 1 graphically illustrates the temperature loss which is experienced in an oven heated blank in moving the blank from the oven to a forming area. For example, if a blank is heated to 1000 F. in an oven and 15 seconds is required to move the blank from the oven to a forming facility it is seen that the temperature of the blank will drop approximately 250 F. during the transfer. Thus a high percentage of the ductility of the metal is lost during the transfer operation.
- the curve of FIGURE 2 graphically illustrates the heating and cooling of a sheet metal blank heated by radiant heaters as disclosed herein.
- This method of heating is fast and efiicient, the temperature of the blank raisin-g from 70 to 1125 F. in approximately 80 seconds.
- the time required to remove the radiant heaters requires approximately 4-5 seconds. During this time delay the temperature of the blank does not change appreciably, it is posible to form the sheet at approximately 7 or slightly less than its maximum temperature and accordingly the blank is formed while its ductility is high.
- the method of minimizing heat loss while fabricating parts from titanium sheet material which can only be effectively worked at elevated temperatures comprising the following steps: positioning a blank sheet of titanium in its forming position in a forming facility while each is at normal room temperatures; positioning a radiant heat source in a juxtaposed position with respect to one of the major sides of said blank sheet; said radiant heat source constituting a bank of quartz tubes adapted to transmit heat to said sheet solely by radiation maintaining said heat source in said juxtaposed position until the temperature of said blank sheet is elevated to a predetermined temperature exceeding 800 F.; removing said heat source from said juxtaposed position to a position ing position and the temperature thereof is near said predetermined temperature.
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- Chemical & Material Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Shaping Metal By Deep-Drawing, Or The Like (AREA)
Description
June 8, 1965 R. A. BRIDWELL 3,187,544
METHOD FOR EFFECTING A METAL WORKING PROCESS Original Filed Dec. 9, 1958 770w [Alma/e9) 0 :0 z0 1a 4a :0 to 7010 120 771m! firm/Ida) United States Patent 3,187,544 METHOD FGR EFFECTTNG A METAL WEIRKENG IRGCESS Robert A. Bridwell, Lynwood, (Iaiih, assignor to Northrop Corporation, a corporation of California tliriginal application Dec. 9, 1953, Ser. No. 779,243. Divided and this application July 31, 1962, Ser. No. 214,454
1 Claim. ((Il. 72-364) This invention pertains to a metal working process and more particularly to a method of heating material to a desired temperature while placed in a specific position and subsequently forming the material at or near the desired temperature without repositioning the material. This application constitutes a division of our copending application, 779,243, filed December 9, 1958, now US. Patent 3,073,172.
It is a prerequisite of certain types of material that they must be heated prior to their fabrication. This is particularly true of titanium and magnesium sheets, etc., and alloys thereof if they are to be effectively fabricated into sheet metal parts by stamping, pressing, drawing, and like operations. These blanks must be worked at elevated temperatures to render them sufliciently ductile to eliminate the occurrence of cracks, tears, and the like which normally occur during the working of these materials at ordinary room temperatures. Elevated temperatures as used throughout the specification refer to temperatures in the 300-1500 F. range.
It is well known in the metal working art that an elongation loss of approximately 66% is experienced in the forming of titanium, magnesium and like sheets should their temperature drop 200 from the maximum allowable temperature of approximately 9001300 F. It, therefore, becomes apparent that sheet material of this type must be worked at a high predetermined temperature, or as near to the predetermined temperature as possible, if optimum results are to be achieved.
To the best of applicants knowledge blank sheet material as described above are at present heated in an oven located in the immediate vicinity. of a forming facility. However, this method is not satisfactory due to the time lag which necessarily occurs between the removal of a blank from an oven and an actual forming operation. A time lag of 12-15 seconds is required to remove the blank from an oven and place it in a forming facility during which time the blank experiences a temperature drop of as much as 250 and a corresponding loss in elongation.
Accordingly it is an object of the present invention to disclose a method of forming titanium, magnesium and like sheets at or near a predetermined elevated temperature without first preheating the sheets to temperatures exceeding the predetermined elevated temperature.
Another object is to disclose a method of forming sheet metal parts from metal sheets in which the elapsed time occurring between a heating and a forming operation thereon is minimized.
Another object is to disclose a method of forming sheet metal parts from metal sheets in which oxidation thereof is minimized.
Although the characteristic features of the present invention are particularly pointed out in the appended claim, the invention itself, also the manner in which it may be carried out, will be better understood by referring to the following description taken in connection with the accompanying drawings forming a part of this application and in which:
FIGURE 1 is a graph showing the temperature losses encountered by an oven heated titanium alloy sheet in transferring the sheet from an oven to a forming area.
2 is a graph showing of the heating and cool- "ice ing of a titanium alloy sheet heated by radiation as disclosed herein, the radiantly heated sheet being of the same size and thickness and otherwise having the same characteristics as the oven heated sheet referred to in the description of FIGURE 1.
This invention utilizes a radiant heat source (not shown) for the heating of titanium, magnesium and like sheet metal blanks which subsequently are to be formed into sheet metal parts. The blank sheets are first coated with a high temperature drawing compound so that they will absorb heat more readily.
The blanks are then positioned in their exact forming attitude in a forming facility (not shown). The aforementioned radiant heat source comprises a plurality of quartz tube radiant heaters mounted in a suitable reflector, the number of heater tubes depending upon the size of the blanks to be heated. The reflector and heater tubes are new juxtapositioned above the blank so that the rays from the heater tubes are directed on the subject blank. The heater tubes are now energized and remain energized until such time as the temperature of the subject blank reaches a predetermined temperature. The reflector and heater tubes are then withdrawn from their juxtapositioned position above the blank allowing the forming operation to be effected without delay and with a minimum temperature loss.
Referring to the drawing, the curve in FIGURE 1 graphically illustrates the temperature loss which is experienced in an oven heated blank in moving the blank from the oven to a forming area. For example, if a blank is heated to 1000 F. in an oven and 15 seconds is required to move the blank from the oven to a forming facility it is seen that the temperature of the blank will drop approximately 250 F. during the transfer. Thus a high percentage of the ductility of the metal is lost during the transfer operation.
The curve of FIGURE 2 graphically illustrates the heating and cooling of a sheet metal blank heated by radiant heaters as disclosed herein. This method of heating is fast and efiicient, the temperature of the blank raisin-g from 70 to 1125 F. in approximately 80 seconds. The time required to remove the radiant heaters requires approximately 4-5 seconds. During this time delay the temperature of the blank does not change appreciably, it is posible to form the sheet at approximately 7 or slightly less than its maximum temperature and accordingly the blank is formed while its ductility is high.
While in .order to comply with the statute, the invention has been described in language more or less specific as to structural features, it is to be understood that the invention is not limited to the specific features shown, but that the means and construction herein disclosed comprises a preferred form of putting the invention into effect, and the invention is therefore claimed in any of its forms or modifications within the legitimate and valid scope of the appended claim.
What is claimed is:
The method of minimizing heat loss while fabricating parts from titanium sheet material which can only be effectively worked at elevated temperatures comprising the following steps: positioning a blank sheet of titanium in its forming position in a forming facility while each is at normal room temperatures; positioning a radiant heat source in a juxtaposed position with respect to one of the major sides of said blank sheet; said radiant heat source constituting a bank of quartz tubes adapted to transmit heat to said sheet solely by radiation maintaining said heat source in said juxtaposed position until the temperature of said blank sheet is elevated to a predetermined temperature exceeding 800 F.; removing said heat source from said juxtaposed position to a position ing position and the temperature thereof is near said predetermined temperature.
References Cited by the Examiner UNITED STATES PATENTS 2,055,535 9/36 Hopkins.
1/ 6'2 Bridwel-l 29-552.2 X 3/62 Haerr 29552.2 X
OTHER REFERENCES 5 Forming of Hi Temperature Metals, A.S.M.E., Mar.
,Plastic Working of Magnesium Alloy Sheet, The Iron Age, Mar. 18, 1943, pp. 45-50.
10 WHITMORE A. WILTZ, Primary Examiner.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US214464A US3187544A (en) | 1958-12-09 | 1962-07-31 | Method for effecting a metal working process |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US779243A US3073172A (en) | 1958-12-09 | 1958-12-09 | Movement for heat exchange assembly |
US214464A US3187544A (en) | 1958-12-09 | 1962-07-31 | Method for effecting a metal working process |
Publications (1)
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US3187544A true US3187544A (en) | 1965-06-08 |
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US214464A Expired - Lifetime US3187544A (en) | 1958-12-09 | 1962-07-31 | Method for effecting a metal working process |
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Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3469433A (en) * | 1965-06-04 | 1969-09-30 | Eugene E Fresch | Metal-working process |
US3503240A (en) * | 1966-08-01 | 1970-03-31 | James R Lawler | Heat treating method and apparatus |
US4181000A (en) * | 1977-10-04 | 1980-01-01 | Rockwell International Corporation | Method for superplastic forming |
EP0026032A1 (en) * | 1979-07-24 | 1981-04-01 | SAMUEL STRAPPING SYSTEMS (a division of SAMUEL MANU-TECH INC.) | Heat treatment process and apparatus |
US4362578A (en) * | 1980-10-16 | 1982-12-07 | Teledyne Industries, Inc. | Method of hot working metal with induction reheating |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2055535A (en) * | 1934-06-20 | 1936-09-29 | Kellogg M W Co | Method for corrugating conduits |
US3015292A (en) * | 1957-05-13 | 1962-01-02 | Northrop Corp | Heated draw die |
US3025905A (en) * | 1957-02-07 | 1962-03-20 | North American Aviation Inc | Method for precision forming |
-
1962
- 1962-07-31 US US214464A patent/US3187544A/en not_active Expired - Lifetime
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2055535A (en) * | 1934-06-20 | 1936-09-29 | Kellogg M W Co | Method for corrugating conduits |
US3025905A (en) * | 1957-02-07 | 1962-03-20 | North American Aviation Inc | Method for precision forming |
US3015292A (en) * | 1957-05-13 | 1962-01-02 | Northrop Corp | Heated draw die |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3469433A (en) * | 1965-06-04 | 1969-09-30 | Eugene E Fresch | Metal-working process |
US3503240A (en) * | 1966-08-01 | 1970-03-31 | James R Lawler | Heat treating method and apparatus |
US4181000A (en) * | 1977-10-04 | 1980-01-01 | Rockwell International Corporation | Method for superplastic forming |
EP0026032A1 (en) * | 1979-07-24 | 1981-04-01 | SAMUEL STRAPPING SYSTEMS (a division of SAMUEL MANU-TECH INC.) | Heat treatment process and apparatus |
US4362578A (en) * | 1980-10-16 | 1982-12-07 | Teledyne Industries, Inc. | Method of hot working metal with induction reheating |
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