EP2016279A2 - Method and apparatus for hot forming elongated metallic bars - Google Patents
Method and apparatus for hot forming elongated metallic barsInfo
- Publication number
- EP2016279A2 EP2016279A2 EP07794657A EP07794657A EP2016279A2 EP 2016279 A2 EP2016279 A2 EP 2016279A2 EP 07794657 A EP07794657 A EP 07794657A EP 07794657 A EP07794657 A EP 07794657A EP 2016279 A2 EP2016279 A2 EP 2016279A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- die
- metal form
- metal
- wrapping
- insulative material
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Withdrawn
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D11/00—Bending not restricted to forms of material mentioned in only one of groups B21D5/00, B21D7/00, B21D9/00; Bending not provided for in groups B21D5/00 - B21D9/00; Twisting
- B21D11/02—Bending by stretching or pulling over a die
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D37/00—Tools as parts of machines covered by this subclass
- B21D37/16—Heating or cooling
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
- B21J13/00—Details of machines for forging, pressing, or hammering
- B21J13/08—Accessories for handling work or tools
Definitions
- the present invention relates to hot stretch-wrap forming of metal parts, most particularly elongated metal bars. More particularly, the invention relates to hot stretch-wrap forming of titanium, titanium alloys and similar metals which are typically difficult to stretch-wrap form. In particular, the invention relates to hot stretch-wrap forming of a metal form using a die having a thermally and electrically insulated work surface.
- the present invention relates to the hot stretch-wrap forming of elongated metallic parts which are formed at high temperatures, and in particular parts made of titanium alloys which are manufactured by extrusion, forging, rolling, machining or a combination of these processes.
- Titanium alloys have been widely used as aerospace materials due to their excellent mechanical and corrosion properties in combination with being comparatively light weight.
- titanium alloys are difficult to form in general and require heating to a substantial temperature in order to properly form such parts.
- Titanium alloys are highly desirable for use in contoured structural members of an aircraft, but the formation of such structural members has been very limited due to the lack of a suitable and economically feasible method of forming such contoured members.
- the demand for such parts has increased with the desire for lightweight and high strength structural components such as chords in advanced airplanes.
- bump forming One process currently available for forming elongated titanium parts is known as "bump forming". This process involves the heating of an elongated part in the furnace to a predetermined temperature at which time the part is removed from the furnace and placed on forming blocks of a forming press. The press applies a bending force which results in a localized deformation of the part. The temperature of the part quickly decreases during formation and the resistance to forming thus significantly increases. Thus, bump forming requires repeated heating cycles to complete the forming process, which is time consuming and costly. In addition, the bending moment that results from bump forming causes tensile stresses in the section of the part above the neutral axis and compressive stresses below the neutral axis which lead respectively to cracks and wrinkles in the part.
- the present invention provides an apparatus comprising a die having a work surface which is formed of at least one of a thermally insulative material and an electrically insulative material; wherein the work surface is adapted for wrapping a metal form there around during hot stretch wrap forming of the metal form; a set of first and second spaced jaws adapted for gripping the metal form; wherein the jaws are movable away from one another whereby the jaws are adapted to apply a stretching force to the metal form; and wherein at least one of the set and the die is movable relative to the other of the set and die between a pre-wrapping configuration and a post-wrapping configuration whereby the relative movement between the set and die is adapted to wrap the metal form around the work surface of the die.
- the present invention further provides a method comprising the steps of heating a metal form; applying a stretching force to the heated metal form; and wrapping the heated metal form around a working surface which is formed of at least one of a thermally insulative material and an electrically insulative material.
- Fig. 1 is a diagrammatic top plan view of the hot stretch-wrap forming apparatus of the present invention showing thermally and electrically insulative material within the die cavity and a metal bar prior to wrapping around the die.
- Fig. 2 is a sectional view taken on line 2-2 of Fig. 1 showing two layers of insulative material within the die cavity.
- Fig. 3 is a sectional view similar to Fig. 2 showing the metal bar inserted into the die cavity with the insulative material separating the metal die and metal bar.
- Fig. 4 is similar to Fig. 1 and shows the jaws having moved from the starting position of Fig. 1 to the completed position of Fig.4 to wrap the elongated bar around the work surface of the die.
- Fig. 5 is a diagrammatic side elevational view of one of the jaws of the present invention.
- Fig. 6 is similar to Fig. 3 and shows a single layer of insulation instead of a double layer of insulation.
- Fig. 7 is similar to Fig. 6 and shows a metal form and die cavity having a different configuration.
- the hot stretch-wrap forming apparatus of the present invention is indicated generally at 10 in Fig. 1.
- Apparatus 10 includes a die 12 and a pair of spaced jaws 14 which are configured to clamp a metal form shown as an elongated metal bar 16 adjacent respective ends thereof in order to stretch metal bar 16 when heated and wrap it around die 12.
- Apparatus 10 is particularly useful for hot stretch-wrap forming of bars made of titanium alloys.
- Jaws 14 are attached to respective swing arms which are not shown but are well known in the art.
- Each of jaws 14 is in communication with an electrical power source 18 via conductors or wires 20 to form an electrical circuit for resistively heating metal bar 16.
- the exemplary embodiment of apparatus 10 shows die 12 in electrical communication with power source 18 via wires 22 to form an electrical circuit by which die 12 may be resistively heated if desired.
- a plurality of heating elements 24 may be inserted into die 12 for the heating thereof.
- Die 12 includes a body having a die face or cavity- bounding surface 26 which defines a T-shaped die cavity 28 (Fig. 2).
- Surface 26 and cavity 28 have an arcuate configuration which extends from a first end 30 of die 12 to a second end 32 of die 12.
- First or inner and second or outer layers 34 and 36 of insulation serve as a die face cover which is positionable between die face 26 and metal bar 16 during the hot stretch-wrap process.
- Layers 34 and 36 are shown disposed within cavity 28 with first layer 34 abutting surface 26 of die 12 in a substantially continuous manner from first end 30 to second end 32 of die 12.
- Second layer 36 likewise abuts first layer 34 in a substantially continuous manner from first end 30 to second end 32.
- Layers 34 and 36 conform to surface 26 and thus are of a generally T-shaped configuration.
- Second layer 36 defines a working surface 38 which abuts metal bar 16 during the wrapping process.
- metal bar 16 has a T-shaped cross section which is of a mating configuration with the T-shaped cavity 28 and working surface 38.
- Work surface 38 defines a T-shaped working space 40 in which bar 16 is disposed during the stretch-wrap process.
- each of first and second layers 34 and 36 is most preferably formed of a thermally and electrically insulative material.
- one of layers 34 and 36 may be formed of a thermally insulative material and the other may be formed of an electrically insulated material if desired. While it is preferred to provide thermal and electrical insulation between die 12 and bar 16, it is contemplated that only a layer of thermal insulation or only a layer of electrical insulation may be used depending on the circumstances.
- Jaw 14 includes first and second spaced arms 42 and 44, first and second insulation members 46 and 48 respectively connected to arms 42 and 44 and disposed therebetween, and first and second gripping members 50 and 52 respectively connected to insulation members 46 and 48 and disposed therebetween.
- First insulation member 46 thus prevents electrical communication between first arm 42 and first gripping member 50
- second insulation member 48 likewise prevents electrical communication between second arm 44 and second gripping member 52.
- First gripping member 50 is in electrical communication with wire 20 and with metal bar 16 when clamping bar 16 so that first gripping member 50 is part of the electrical circuit previously discussed for providing the resistive heating of metal bar 16. The electrical scheme shown in Fig.
- layers 34 and 36 are formed of a flexible refractory material. This allows layers 34 and 36 to easily conform to the shape of the die cavity.
- the use of such flexible layers allows for versatility in positioning the layers prior to the wrapping process. For example, prior to insertion of the metal bar into the die cavity, the layers may be disposed within the die cavity (as shown), wrapped around a portion or all of the metal bar, or simply suspended between the cavity and the metal bar so that insertion of the metal bar into the cavity presses the insulation material into the desired shape.
- Layers 34 and 36 are typically refractory ceramic blankets.
- Ceramic blankets typically provide both the thermal and electrical insulative properties previously described and are formed of woven ceramic fabric or fibers. These flexible blankets are also easily removed from the die cavity or the metal bar when degraded to a degree such that they are no longer useful for the present purpose. While such ceramic blankets are one form of a desirable insulative material, other suitable materials may be utilized which provide the thermal and/or electrical insulative properties needed for the present invention and which are capable of withstanding the heat and pressure utilized during the wrapping process.
- power source 18 is operated to cause an electrical current to flow through metal bar 16 to resistively heat metal bar 16 to a desired predetermined temperature. Once this temperature is reached, jaws 14 apply an outward stretching force as indicated at Arrows A, that is, a longitudinal tensile force or strain. Meanwhile, die 12 may or may not be heated depending on the particular circumstances. If die 12 is to be heated, power source 18 may be operated to resistively heat die 12 via wires 22 and/or heating elements 24 may be heated to heat die 12. Whether or not die 12 is heated, jaws 14 are then moved toward die 12 to move bar 16 into working space 40 as indicated at Arrows B in Figs. 3 and 4.
- die 12 may be moved to facilitate the relative movement between die 12 and jaws 14. Jaws 14 are then moved as indicated at Arrows C in Fig. 4 to force bar 16 against work surface 38 of layer 36 to wrap bar 16 around die 12 to form the arcuate configuration of the formed part as shown in Fig.4. The longitudinal stretching force continues to be applied to metal bar 16 during the wrapping of the bar around die 12. Thus, jaws 14 move from the pre-wrapping configuration of apparatus 10 shown in Fig. 1 to the post-wrapping configuration shown in Fig. 4. The electrically insulative property of layer 34 and/or 36 prevents the electrical shunting between bar 16 and die 12 which was discussed in the Background section of the present invention.
- thermal insulative property of layer 34 and/or 36 minimizes or eliminates the creation of hot spots in bar 16 which might otherwise be caused by die 12 when it is heated, and especially if not uniformly heated.
- the thermal insulative property also allows for the use of die 12 either without heating die 12 or heating die 12 at a substantially reduced level compared to known prior art configurations.
- apparatus 10 provides a configuration for resistively heating metal bar 16 without creating shunting problems or hot spots during the wrapping operation.
- resistive heating of metal bar 16 provides for uniform heating throughout the metal bar.
- metal bar 16 is heated to a particular temperature range, is stretched at a relatively low strain rate and is held at the temperature range throughout the process and for a holding period after the wrapping process in order to allow formation of the metal bar in its final form substantially without springing back and substantially without undesirable tensile or compressive stresses within the formed part. Longitudinal stretching may continue during the holding period if desired.
- the uniform temperature of bar 16 is preferably maintained throughout the stretching and wrapping process and during any holding period, even if die 12 is not independently heated or is heated to a temperature substantially below the forming temperature of bar 16.
- Insulation layers 34 and/or 36 greatly facilitate the ability to maintain this uniform temperature due to the corresponding reduction in heat loss from bar 16 and prevention of the hot spots previously discussed. Apparatus and methods for several preferred aspects of the invention are described in greater detail in the copending patent application entitled Method And Apparatus For Creep Forming Of And Relieving Stress In An Elongated Metal Bar, which is filed concurrently herewith and incorporated by reference herein.
- Fig. 6 shows an alternate embodiment in which only layer 34 of insulation is used, thus eliminating a layer 36.
- layer 34 may have thermal and/or electrical insulation properties depending on the specific circumstances although typically both thermal and electrical insulative properties are desired.
- Fig. 7 shows an alternate die 54 defining a U-shaped cavity for use with a generally U-shaped metal bar 56.
- First and second layers 58 and 60 are used in a manner analogous to layers 34 and 36 and conform to the U-shaped configuration of the cavity of die 54.
- Fig. 7 thus represents that the process can be used with metal bars of a wide variety of cross sectional shapes.
- Other shapes may have an outwardly-facing recess, such as a U-shaped configuration which is inverted relative to bar 56.
- These recesses may be filled with an elongated flexible structure to maintain the proper configuration during hot-stretch formation, for instance, to prevent the legs of the inverted U-shape bar from deforming toward one another.
- certain terms have been used for brevity, clearness, and understanding. No unnecessary limitations are to be implied therefrom beyond the requirement of the prior art because such terms are used for descriptive purposes and are intended to be broadly construed.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Heat Treatment Of Strip Materials And Filament Materials (AREA)
- Resistance Heating (AREA)
- Shaping Metal By Deep-Drawing, Or The Like (AREA)
- Extrusion Of Metal (AREA)
- Metal Extraction Processes (AREA)
- Bending Of Plates, Rods, And Pipes (AREA)
Abstract
Description
Claims
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US11/432,045 US20070261461A1 (en) | 2006-05-11 | 2006-05-11 | Method and apparatus for hot forming elongated metallic bars |
| PCT/US2007/011115 WO2007133548A2 (en) | 2006-05-11 | 2007-05-08 | Method and apparatus for hot forming elongated metallic bars |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP2016279A2 true EP2016279A2 (en) | 2009-01-21 |
| EP2016279A4 EP2016279A4 (en) | 2010-06-23 |
Family
ID=38683854
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP07794657A Withdrawn EP2016279A4 (en) | 2006-05-11 | 2007-05-08 | Method and apparatus for hot forming elongated metallic bars |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US20070261461A1 (en) |
| EP (1) | EP2016279A4 (en) |
| JP (1) | JP2009536881A (en) |
| KR (1) | KR20090008383A (en) |
| CN (1) | CN101505888A (en) |
| WO (1) | WO2007133548A2 (en) |
Families Citing this family (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102814368A (en) * | 2012-08-23 | 2012-12-12 | 北京航空航天大学 | Compound molding tool system for hot stretch bending and creep deformation of section bar and application method of compound molding tool system |
| US20180015522A1 (en) * | 2016-06-20 | 2018-01-18 | Imam Khomeini International University | High-speed hot forming and direct quenching |
| CN106825250B (en) * | 2017-04-01 | 2018-12-11 | 京东方科技集团股份有限公司 | A kind of mold |
| CN109954773A (en) * | 2019-04-30 | 2019-07-02 | 长春工业大学 | A kind of metal profile multi-point three-dimensional hot drawing and bending forming equipment |
| CN111644498B (en) * | 2020-06-12 | 2021-09-10 | 中国航空制造技术研究院 | Control method for electrothermal stretch bending process of titanium alloy section and stretch bending forming device |
| CN112157157B (en) * | 2020-09-11 | 2023-03-24 | 中国航空制造技术研究院 | Forming method and correcting device for titanium alloy thin-wall component |
| CN115673117B (en) * | 2022-11-09 | 2025-07-15 | 中国航发沈阳黎明航空发动机有限责任公司 | A local temperature-changing forming device and method for titanium alloy hoop-type component linkage die |
Family Cites Families (29)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2952767A (en) * | 1960-09-13 | Thermo stretch forming of metal | ||
| US2486817A (en) * | 1948-11-24 | 1949-11-01 | Glenn L Martin Co | Apparatus for stretch forming hard metal alloys |
| US3021887A (en) * | 1956-07-19 | 1962-02-20 | Rohr Aircraft Corp | Titanium stretch forming |
| US2905225A (en) * | 1956-09-13 | 1959-09-22 | Romeo A Lalli | Stretch former with replaceable heated die and pivotally mounted draw bar |
| US3169156A (en) * | 1960-12-23 | 1965-02-09 | Gen Dynamics Corp | Apparatus for the forming and aging of titanium alloys |
| US3426589A (en) * | 1966-07-18 | 1969-02-11 | Lebow Associates Inc | Tension transducer |
| US3452573A (en) * | 1967-06-14 | 1969-07-01 | Cyril Bath Co | Stretch wrapping fixture and combination thereof with drawing dies and press |
| US3568490A (en) * | 1968-09-27 | 1971-03-09 | Fairchild Hiller Corp | Method and apparatus for heat forming elongated metal panels |
| US3584487A (en) * | 1969-01-16 | 1971-06-15 | Arne H Carlson | Precision forming of titanium alloys and the like by use of induction heating |
| US3722068A (en) * | 1971-02-22 | 1973-03-27 | Northrop Corp | Method for forming titanium sheets |
| US3934441A (en) * | 1974-07-08 | 1976-01-27 | Rockwell International Corporation | Controlled environment superplastic forming of metals |
| US3933020A (en) * | 1974-07-18 | 1976-01-20 | Tre Corporation | Method for stretch wrapping of panels |
| US3920175A (en) * | 1974-10-03 | 1975-11-18 | Rockwell International Corp | Method for superplastic forming of metals with concurrent diffusion bonding |
| US3974673A (en) * | 1975-04-07 | 1976-08-17 | Rockwell International Corporation | Titanium parts manufacturing |
| US4011429A (en) * | 1975-10-20 | 1977-03-08 | Northrop Corporation | Hot stretch-wrap forming with resistance heating |
| US4188811A (en) * | 1978-07-26 | 1980-02-19 | Chem-Tronics, Inc. | Metal forming methods |
| US4242899A (en) * | 1979-03-05 | 1981-01-06 | The United States Of America As Represented By The Secretary Of The Air Force | Thermoclamps |
| US4268246A (en) * | 1979-09-21 | 1981-05-19 | Chicago Bridge & Iron Company | Method and apparatus for metal object heat treatment |
| DE3572081D1 (en) * | 1984-09-28 | 1989-09-07 | Philips Nv | Method of drape drawing a shadow mask for a colour display tube and device for such a method |
| FR2620956A1 (en) * | 1987-09-29 | 1989-03-31 | Inst Francais Du Petrole | METHOD FOR FORMING TITANIUM OR TITANIUM ALLOY SURFACE SHEET ELEMENT |
| US4984348A (en) * | 1989-01-17 | 1991-01-15 | Rohr Industries, Inc. | Superplastic drape forming |
| US5119535A (en) * | 1989-09-18 | 1992-06-09 | The Boeing Company | Method of reconfiguring rigid and semirigid structures |
| US5823034A (en) * | 1997-10-10 | 1998-10-20 | Hyperform Technologies, Inc. | Superplastic metalforming with self-contained die |
| AU3854400A (en) * | 1999-06-01 | 2000-12-18 | Mehmet Terziakin | Instant heating process with electric current application to the workpiece for high strength metal forming |
| DE10063287B4 (en) * | 2000-12-19 | 2007-05-03 | Airbus Deutschland Gmbh | Method for forming a metal sheet |
| US6776020B2 (en) * | 2002-10-11 | 2004-08-17 | General Motors Corporation | Method for stretching forming and transporting and aluminum metal sheet |
| US6910358B2 (en) * | 2003-08-25 | 2005-06-28 | General Motors Corporation | Two temperature two stage forming |
| US20060230807A1 (en) * | 2005-04-14 | 2006-10-19 | Shultz Stephen W | Creep forming a work piece |
| US7669452B2 (en) * | 2005-11-04 | 2010-03-02 | Cyril Bath Company | Titanium stretch forming apparatus and method |
-
2006
- 2006-05-11 US US11/432,045 patent/US20070261461A1/en not_active Abandoned
-
2007
- 2007-05-08 CN CNA200780016841XA patent/CN101505888A/en active Pending
- 2007-05-08 JP JP2009509814A patent/JP2009536881A/en not_active Withdrawn
- 2007-05-08 WO PCT/US2007/011115 patent/WO2007133548A2/en not_active Ceased
- 2007-05-08 EP EP07794657A patent/EP2016279A4/en not_active Withdrawn
- 2007-05-08 KR KR1020087028366A patent/KR20090008383A/en not_active Withdrawn
Also Published As
| Publication number | Publication date |
|---|---|
| EP2016279A4 (en) | 2010-06-23 |
| WO2007133548A2 (en) | 2007-11-22 |
| KR20090008383A (en) | 2009-01-21 |
| US20070261461A1 (en) | 2007-11-15 |
| WO2007133548A3 (en) | 2009-03-26 |
| JP2009536881A (en) | 2009-10-22 |
| CN101505888A (en) | 2009-08-12 |
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Legal Events
| Date | Code | Title | Description |
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| PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
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| 17P | Request for examination filed |
Effective date: 20081110 |
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| AX | Request for extension of the european patent |
Extension state: AL BA HR MK RS |
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| R17D | Deferred search report published (corrected) |
Effective date: 20090326 |
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| A4 | Supplementary search report drawn up and despatched |
Effective date: 20100525 |
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| RIC1 | Information provided on ipc code assigned before grant |
Ipc: B21D 11/02 20060101AFI20100518BHEP |
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| 17Q | First examination report despatched |
Effective date: 20100609 |
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| STAA | Information on the status of an ep patent application or granted ep patent |
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| 18D | Application deemed to be withdrawn |
Effective date: 20101221 |