EP1884297A1 - Formkonstruktionsverfahren, Form, Herstellungsverfahren für eine Hohlkammerplatte und Hohlkammerplatte - Google Patents
Formkonstruktionsverfahren, Form, Herstellungsverfahren für eine Hohlkammerplatte und Hohlkammerplatte Download PDFInfo
- Publication number
- EP1884297A1 EP1884297A1 EP20070011703 EP07011703A EP1884297A1 EP 1884297 A1 EP1884297 A1 EP 1884297A1 EP 20070011703 EP20070011703 EP 20070011703 EP 07011703 A EP07011703 A EP 07011703A EP 1884297 A1 EP1884297 A1 EP 1884297A1
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- European Patent Office
- Prior art keywords
- die
- hollow panel
- strain
- extrusion
- region
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- 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.)
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21C—MANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES OR PROFILES, OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
- B21C25/00—Profiling tools for metal extruding
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21C—MANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES OR PROFILES, OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
- B21C23/00—Extruding metal; Impact extrusion
- B21C23/02—Making uncoated products
- B21C23/04—Making uncoated products by direct extrusion
- B21C23/14—Making other products
- B21C23/142—Making profiles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21C—MANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES OR PROFILES, OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
- B21C25/00—Profiling tools for metal extruding
- B21C25/10—Making tools by operations not covered by a single other subclass
Definitions
- the present invention relates to a die-designing method, a die, a method for production of hollow panel, and a hollow panel.
- Japanese Patent No. 3645453 discloses a die which consists of more than one entry port for flow splitting of raw material, a chamber (merging space) in which the flows of raw material passing through each entry port merge and weld together, and a forming space in which the raw material which has been welded together in the merging space is formed into a hollow section by extrusion.
- the hollow section extruded from the die has more than one weld mark resulting from the welding of the split raw material passing through the entry ports.
- the die-designing method disclosed in said patent specifies each entry port which has an adequate position of gravitational center and an adequate area of orifice so that there exists a correspondence between the ratio of volume distribution among regions welded together in the hollow section and the ratio of flows of raw material passing through each entry port.
- the thus designed die permits uniform extrusion from the forming space without causing excess distortion to the raw material. This yields hollow sections with high dimensional accuracy and straightness.
- the present invention was completed for production of well-shaped thin, wide hollow panels free of the foregoing problem.
- the entry ports and the merging space are assigned characteristic design values so that no difference exceeding ⁇ 10% occurs between the average value of strain in all regions in the welded parts and the individual values of strain in each region in the welded parts.
- the thus designed extrusion die yields a hollow panel with a limited strain which differs only slightly from one region of the welded parts to another.
- the limited strain prevents the extruded hollow panel from suffering unintended wavy distortion. This is true particularly in the case of thin, wide hollow panels with low stiffness.
- the extrusion die according to the present invention is suitable for production of thin, wide hollow panels free of distortion.
- the above-mentioned die-designing method should preferably be modified by changing the characteristic design values of said entry ports and said merging space such that said hollow panel extruded from said die has a limited strain which does not differ more than ⁇ 6% between the average value of strain in all regions in the welded parts and the individual values of strain in each region in the welded parts.
- the thus designed extrusion die yields a hollow panel with a limited strain which differs only slightly from one region of the welded parts to another.
- the limited strain prevents the extruded hollow panel from suffering unintended wavy distortion. This is true particularly in the case of thin, wide hollow panels with thick parts and an opening at the center in the widthwise direction.
- the extrusion die according to the present invention is suitable for production of thin, wide hollow panels free of distortion.
- the die-designing method should preferably be further modified by changing the characteristic design values of said entry ports and said merging space such that said hollow panel extruded from said die has a limited strain which does not differ more than ⁇ 3% between the average value of strain in all regions in the welded parts and the individual values of strain in each region in the welded parts.
- the thus designed extrusion die yields a hollow panel with a limited strain which differs only slightly from one region of the welded parts to another.
- the limited strain prevents the extruded hollow panel from suffering unintended wavy distortion. This is true particularly in the case of thin, wide hollow panels with thick parts and uneven stiffness and an opening away from the center in the widthwise direction.
- the extrusion die according to the present invention is suitable for production of thin, wide hollow panels free of distortion.
- each of said entry ports and said merging space have characteristic design values such that there exists a correspondence between the ratio of volume distribution among regions welded together in the hollow panel and the ratio of flows of raw material passing through each entry port and said hollow panel has a limited strain which does not differ more than ⁇ 10% between the average value of strain in all regions in the welded parts and the individual values of strain in each region in the welded parts.
- the die designed in this manner achieves extrusion such that there exists a correspondence between the ratio of volume distribution among regions welded together in the hollow panel and the ratio of flows of raw material passing through each entry port.
- the die designed in this manner gives a hollow panel characterized by a limited strain which does not differ more than ⁇ 10% between the average value of strain in all regions in the welded parts and the individual values of strain in each region in the welded parts. Therefore, it is capable of forming a satisfactory thin, wide hollow panel as mentioned above.
- the resulting hollow panel has a high dimensional accuracy and good straightness.
- the die according to the present invention is produced by any one of the above-mentioned die-designing methods. It is capable of extruding hollow panels while suppressing unintended wavy distortion. Hence, it is suitable for extrusion of thin, wide hollow panels in good shape.
- the present invention also covers a method for producing hollow panels by extrusion through the above-mentioned die. This method permits extrusion of hollow panels without unintended wavy distortion and hence is suitable for extrusion of thin, wide hollow panels in a good shape.
- the present invention also covers the hollow panel produced by the above-mentioned method for producing a hollow panel.
- the hollow panel has a thin, wide structure in a good shape free of unintended wavy distortion.
- the present invention provides a thin, wide hollow panel in a good shape.
- Figs. 1 and 2 show the structure of the hollow panel 1 formed by extrusion through the die 24 (mentioned later) according to the first embodiment of the present invention.
- the hollow panel 1 consists of paired flat sheets 2 and 2.
- the sheets 2 and 2 are arranged parallel to each other, a certain distance away from each other in their thickness direction, and they are joined to each other with a number of ribs 4 formed between them.
- the sheets 2 and ribs 4 have the same thickness.
- This hollow panel 1 is produced by using a forming apparatus 10 shown in Fig. 3.
- the forming apparatus 10 consists of a container 12, a platen 14 (positioned away from the container 12), and a forming unit 16 (positioned between them).
- the container 12 has an inner hole 12a extending in the direction of extrusion of the billet 18 (blank) of aluminum alloy.
- the inner hole 12a is provided with a stem 19 which is driven by a driving mechanism (not shown).
- the stem 19 is movable back and forth in the direction of extrusion of the billet 18.
- the platen 14 is fixedly positioned in the downstream of extrusion of the billet 18 from the container 12. (This position is at the right side in Fig. 3.)
- the forming unit 16 consists of a die slide 20, a die ring 22, a die 24, a backer 26, and a bolster 28.
- the die slide 20 is movable in the direction perpendicular to the direction of extrusion of the billet 18. It is so constructed as to move back and forth between the set position (intermediate between the container 12 and the platen 14) and the retreat position away from the set position in the direction perpendicular to the direction of extrusion of the billet 18.
- the die ring 22 is held by the die slide 20.
- the die ring 22 and the bolster 28 are juxtaposed to each other (in the lateral direction in Fig. 3), and they are held between the container 12 and the platen 14.
- the die ring 22 is an annulus ring, which holds therein the die 24 and the backer 26.
- the die 24 and the backer 26 are sequentially arranged in the direction of extrusion.
- the die 24 consists of a male die 30 and a female die 31. It is constructed as shown in Fig. 4, which is a partly cut-away perspective view.
- the male die 30 and the female die 31 are sequentially arranged in the direction of extrusion of the billet 18, so that the male die 30 fits into the female die 31.
- the male die 30 has the entry ports 30a that penetrate in the direction of extrusion.
- the entry ports 30a communicate with the inner hole 12a of the container 12. See Fig. 3.
- the male die 30 has a projection 30b extending in the direction of extrusion of the billet 18.
- the projection 30b has one end (close to the female die 31) which conforms to the shape of the internal space 6 of the hollow panel 1.
- the female die 31 has a merging space 31a (which communicates with the entry port 30a of the male die 30) and a forming hole 31b (which communicates with the merging space 31a).
- the merging space 31a permits communication between the entry port 30a and the forming space 31b.
- the forming hole 31b has a cross section (perpendicular to the direction of extrusion) which conforms to the peripheral shape of the hollow panel 1.
- the forming hole 31b holds therein the projection 30b of the male die 30, with a gap left between the projection 30b and the inner wall of the forming hole 31b.
- the gap (between the projection 30b of the male die 30 and the inner wall of the forming hole 31b of the female die 31) constitutes the forming space S which conforms to the shape of the hollow panel 1.
- the forming space S communicates with the merging space 31a.
- Fig. 5 shows the process in which the billet 18 (as a blank) changes in shape in the forming apparatus 10 during its extrusion into the hollow panel 1 through the die 24.
- the following steps proceed to form the hollow panel 1.
- the billet 18 is forced into the die 24 by the stem 19 from the inner hole 12a of the container 12.
- the billet is split into the flows 18a of raw material by the entry ports 30a.
- the flows 18a of raw material are forced out of the entry ports 30a.
- the flows 18a of raw material merge (weld together) into the single flow 18b of raw material in the merging space 31a.
- the flow 18b of raw material is formed into the hollow panel 1 (with a hollow cross section) by extrusion through the forming space S.
- the resulting hollow panel 1 has the linear weld lines 1a extending in the direction of extrusion.
- the weld lines 1a are formed as the flows 18a of raw material weld together after passing through the entry ports 30a.
- the hollow panel 1 has the (unwelded) regions 1b between the weld lines 1a at the positions corresponding to the positions of the flows of raw material 18a passing through the entry ports 30a.
- the extrusion process mentioned above causes the flows 18a (18b) of raw material to move from the entry ports 30a into the forming space S through the merging space 31a. However, they do not necessarily move in the entire region of the entry ports 30a and the merging space 31a.
- This is illustrated in Fig. 4, in which each of the entry port 30a and the merging space 31a is divided into two regions by the imaginary line A. In the region inside the imaginary line A, the flow of raw material 18a (18b) moves toward the forming space S, while in the region outside the imaginary line A, the flow 18a (18b) of raw material stops.
- the present inventors' investigation to address the above-mentioned problem revealed that the unintended wavy distortion in the thin, wide hollow panel 1 (shown in Fig. 6) is due to difference in strain existing in the regions 1b between the weld lines 1a. This finding led to a technical idea of suppressing unintended distortion in the hollow panel 1 by reducing difference in strain in the regions 1b between the weld lines 1a.
- the first embodiment of the present invention is intended to design the die 24 by establishing the design characteristic value for each of the entry ports 30a and the design characteristic value for the merging space 31a such that there exists a correspondence between the ratio of volume distribution ratio (Vi) among the regions 1b between the weld lines 1a of the hollow panel 1 and the ratio of flow (Xi) of raw material 18a passing through each entry port 30a and the hollow panel 1 has a limited strain which is defined by a difference ( ⁇ ) not exceeding ⁇ 10% between the average value of strain ( ⁇ i) in all regions 1b in the welded parts 1a and the individual values of strain ( ⁇ i) in each region in the welded parts 1a.
- the ratio of volume distribution (Vi) is defined as the ratio of the individual volume of the region 1b between the welded part 1a to the total volume of the unit length of extrusion of the hollow panel 1.
- the ratio of flow (Xi) is defined as the ratio of the individual flow of raw material 18a passing through each entry port 30a to the total flow of raw material 18a passing through all the entry ports 30a.
- the design characteristic values for the entry port 30a include Sei (which is the sectional area perpendicular to the direction of extrusion), Lei (which is the circumferential length), Hei (which is the depth, shown in Fig. 4), and rei (which is the center position).
- the design characteristic values for the merging space 31a include Hc (which is the depth, shown in Fig. 4).
- the depth (Hei) of the entry port 30a is the length (in the direction of extrusion) of the entry port 30a formed in the male die 30.
- the depth (Hc) of the merging space 31a is the length in the direction of extrusion of the entry port 30a between the end (adjacent to the male die 30) of the female die 31 and the bottom of the merging space 31a.
- the die 24 is practically designed in the following manner.
- the first step is to temporarily establish the position of each welding part 1a of the hollow panel 1.
- the second step is to calculate the total volume per unit extrusion length of the hollow panel 1.
- the third step is to calculate individually the volume of the region 1b between the welding parts 1a.
- the fourth step is to calculate the ratio of the individual volume to the total volume, thereby obtaining the ratio of volume distribution (Vi) of each region 1b between the welding parts 1a.
- the subsequent step is to derive the function f(rei) expressing the relation between position and flow rate, the function g(Sei,Lei,Hei) expressing the relation between shape and flow rate, and the function h(Sei,Hei) expressing the relation between dimension and flow rate, from the above-mentioned design characteristic values (Sei,Hei,rei) of each entry port 30a.
- These functions are combined together to give the following formula (1) that represents the ratio of flow (Xi) passing through each entry port 30a.
- Xi f rei ⁇ g Sei ⁇ Lei ⁇ Hei ⁇ h Sei ⁇ Hei
- the formula (1) is given arbitrary design characteristic values (Sei, Hei, and rei) to obtain the ratio of flow (Xi), and the thus obtained value of Xi is compared with the ratio (Vi) of volume distribution. If no correspondence between Xi and Vi is reached, the design characteristic values Sei, Lei, Hei, and rei are partly or entirely modified and the above-mentioned procedure is repeated until a correspondence between Vi and Xi is reached. In this way the design characteristic values (Sei, Lei, Hei, and rei) are obtained as desired.
- This strain ( ⁇ i) is obtained from the following formula (2), in which Sei represents the sectional area (perpendicular to the direction of extrusion) of each entry port 30a and Soi represents the sectional area (perpendicular to the direction of extrusion) of the corresponding region 1b of the hollow panel 1.
- ⁇ i log Sei , / Soi
- the strain ( ⁇ i) obtained from the formula (2) is put in the following formula (3) to give the relative error ( ⁇ ) of the strain ( ⁇ i) in each region 1b between the welding parts 1a to the average value ( ⁇ i/n) of the strain in each region 1b between the welding parts 1a.
- the design characteristic values (Sei, Lei, Hei, and rei) obtained as mentioned above are employed to form the entry ports 30a, and the characteristic value (Hc) obtained as mentioned above is employed to form the merging space 31a. In this way the die 24 is produced.
- the resulting die 24 is attached to the forming apparatus 10. Extrusion through the die 24 yields the hollow panel 1 in which there exists a correspondence between Vi (the ratio of volume distribution in each region 1b between the welding parts 1a of the hollow panel 1) and Xi (the ratio of flow of raw material 18a passing through the die 24 and the entry ports 30a) and there is a relative error ( ⁇ ) within ⁇ 10% for the strain ( ⁇ i) in each region 1b between the welding parts 1a to the average value of the stain ( ⁇ i) in each region 1b between the welding parts 1a.
- Vi the ratio of volume distribution in each region 1b between the welding parts 1a of the hollow panel 1
- Xi the ratio of flow of raw material 18a passing through the die 24 and the entry ports 30a
- the first embodiment gives the hollow panel 1 in which there exists a correspondence between Vi (the ratio of volume distribution in each region 1b between the welding parts 1a) and Xi (the ratio of flow of raw material 18a passing through the die 24 and the entry ports 30a).
- Vi the ratio of volume distribution in each region 1b between the welding parts 1a
- Xi the ratio of flow of raw material 18a passing through the die 24 and the entry ports 30a.
- the first embodiment permits the die 24 to extrude the hollow panel 1 in which there is a relative error ( ⁇ ) within ⁇ 10% for the strain ( ⁇ i) in each region 1b between the welding parts 1a to the average value of the stain ( ⁇ i) in each region 1b between the welding parts 1a.
- the resulting hollow panel 1 has a reduced difference in strain (( ⁇ i) among the individual regions 1b between the welding parts 1a. This helps reduce unintended wavy distortion in the thin, wide hollow panel 1 with low stiffness which is extruded from the die 24. Therefore, the first embodiment permits extrusion of thin, wide hollow panels with a good shape as well as a high dimensional accuracy and straightness.
- Fig. 7 shows the structure of the hollow panel 41 according to the second embodiment of the present invention.
- the second embodiment is concerned with extrusion of the hollow panel 41 which has thick-walled parts 43 at its both lateral ends and an opening at the center of its width.
- the hollow panel 41 according to the second embodiment has at its lateral ends the thick-walled parts 43 which are thicker than the sheet 2 and the rib 4. It has its lateral ends closed by the thick-walled parts 43, and it has the upward opening 45 at the center of its width.
- the opening 45 extends in the lengthwise direction (or the direction of extrusion) of the hollow panel 41.
- the region 2a near the opening 45 and the region 2b under the opening 45 are thicker than the upper and lower sheets 2.
- the regions 2a and 2b are joined together by the ribs 4a, which are also thicker than other ribs 4.
- the hollow panel 41 with such a structure has the region near the opening 45 reinforced by the thick-walled regions surrounding the opening 45.
- the hollow panel 41 mentioned above is more subject to unintended wavy distortion than the hollow panel 1 (shown in Fig. 2) according to the first embodiment because of variation in thickness and unbalanced stiffness due to the opening 45.
- this object is achieved by establishing the design characteristic values for the entry ports 30a (which include the sectional area Sei (perpendicular to the direction of extrusion), the circumferential length Lei, the depth Hei, and the central position rei of the entry port 30a) and the design characteristic value for the merging space 31a (which includes the depth Hc) by using the formulas (2) and (3) mentioned above in the first embodiment, so that the relative error ( ⁇ ) is within ⁇ 6%.
- the second embodiment is also carried out in the same way as the first embodiment.
- the procedure consists of steps of calculating the design characteristic values (Sei, Lei, Hei, and rei) for the entry ports 30a by using the formula (1) mentioned above, so that there exists a correspondence between the ratio of volume distribution (Vi) and the ratio of passing flow (Xi).
- the foregoing steps are repeated in order to reconfirm the correspondence between Vi and Xi and the relative error ( ⁇ ) within ⁇ 6%, in the same way as in the first embodiment.
- the die 24 designed as mentioned above yields the hollow panel 41 which is less liable to unintended distortion than the hollow panel in the first embodiment on account of the reduced difference in strain ( ⁇ i) in each region 41b between the welding parts 41a.
- the second embodiment is identical with the first embodiment except for the above-mentioned constitution.
- the second embodiment permits the die 24 to extrude the hollow panel 41 in which there is a relative error ( ⁇ ) within ⁇ 6% for the strain ( ⁇ i) in each region 41b between the welding parts 41a to the average value of the stain ( ⁇ i) in each region 41b between the welding parts 41a.
- the resulting hollow panel 41 has a reduced difference in strain ( ⁇ i) among the individual regions 41b between the welding parts 41a, owing to the specifically established design characteristic values for the entry ports 30a and the merging space 31a. This helps reduce unintended wavy distortion in the hollow panel 41 having the thick-walled part 43 and the opening 45 at the center of the width.
- Fig. 8 shows the structure of the hollow panel 51 according to the third embodiment of the present invention.
- the third embodiment is concerned with extrusion of the hollow panel 51 which is similar in structure to the hollow panel 41 (shown in Fig. 7) according to the second embodiment except that the opening 55 is shifted from the center of its width.
- the hollow panel 51 (shown in Fig. 8) according to the third embodiment has the opening 55 in its upper sheet at a position shifted rightward from the center of its width.
- the opening 55 extends in the lengthwise direction (or the direction of extrusion) of the hollow panel 51.
- the hollow panel 51 lacks uniform stiffness, unlike the hollow panel 41 (shown in Fig. 7) according to the second embodiment, because of the opening 55 formed at a position shifted from the center of its width. Therefore, it is more subject to unintended wavy distortion than the hollow panel 41 (shown in Fig. 7) according to the second embodiment.
- this object is achieved by establishing the design characteristic values for the entry ports 30a (which include the sectional area Sei (perpendicular to the direction of extrusion), the circumferential length Lei, the depth Hei, and the central position rei of the entry port 30a) and the design characteristic value for the merging space 31a (which includes the depth Hc) by using the formulas (2) and (3) mentioned above in the first embodiment, so that the relative error ( ⁇ ) is within ⁇ 3%.
- the third embodiment is also carried out in the same way as the first embodiment.
- the procedure consists of steps of calculating the design characteristic values (Sei, Lei, Hei, and rei) for the entry ports 30a by using the formula (1) mentioned above, so that there exists a correspondence between the ratio of volume distribution (Vi) and the ratio of passing flow (Xi).
- the foregoing steps are repeated in order to reconfirm the correspondence between Vi and Xi and the relative error ( ⁇ ) within ⁇ 3%, in the same way as in the first embodiment.
- the die 24 designed as mentioned above yields the hollow panel 51 which is less liable to unintended distortion than the hollow panel in the first embodiment on account of the more reduced difference in strain ( ⁇ i) in each region 51b between the welding parts 51a.
- the third embodiment is identical with the first embodiment except for the above-mentioned constitution.
- the third embodiment permits the die 24 to extrude the hollow panel 51 in which there is a relative error ( ⁇ ) within ⁇ 3% for the strain ( ⁇ i) in each region 51b between the welding parts 51a to the average value of the stain ( ⁇ i) in each region 51b between the welding parts 51a.
- the resulting hollow panel 51 has a further reduced difference in strain ( ⁇ i) among the individual regions 51b between the welding parts 51a, owing to the specifically established design characteristic values for the entry ports 30a and the merging space 31a. This helps reduce unintended wavy distortion in the hollow panel 51 having the thick-walled part 43 and the opening 55 at a position shifted from the center of the width.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Extrusion Of Metal (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2006211962A JP4824499B2 (ja) | 2006-08-03 | 2006-08-03 | ダイスの設計方法、ダイス、中空パネルの製造方法及び中空パネル |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1884297A1 true EP1884297A1 (de) | 2008-02-06 |
EP1884297B1 EP1884297B1 (de) | 2013-05-29 |
Family
ID=38658179
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP20070011703 Active EP1884297B1 (de) | 2006-08-03 | 2007-06-14 | Verfahren zum Entwerfen einer Matrize |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP1884297B1 (de) |
JP (1) | JP4824499B2 (de) |
HK (1) | HK1117091A1 (de) |
Cited By (10)
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US9316155B2 (en) | 2013-03-18 | 2016-04-19 | General Electric Company | System for providing fuel to a combustor |
US9316396B2 (en) | 2013-03-18 | 2016-04-19 | General Electric Company | Hot gas path duct for a combustor of a gas turbine |
US9322556B2 (en) | 2013-03-18 | 2016-04-26 | General Electric Company | Flow sleeve assembly for a combustion module of a gas turbine combustor |
US9360217B2 (en) | 2013-03-18 | 2016-06-07 | General Electric Company | Flow sleeve for a combustion module of a gas turbine |
US9383104B2 (en) | 2013-03-18 | 2016-07-05 | General Electric Company | Continuous combustion liner for a combustor of a gas turbine |
US9400114B2 (en) | 2013-03-18 | 2016-07-26 | General Electric Company | Combustor support assembly for mounting a combustion module of a gas turbine |
US9631812B2 (en) | 2013-03-18 | 2017-04-25 | General Electric Company | Support frame and method for assembly of a combustion module of a gas turbine |
US10436445B2 (en) | 2013-03-18 | 2019-10-08 | General Electric Company | Assembly for controlling clearance between a liner and stationary nozzle within a gas turbine |
CN112692094A (zh) * | 2020-12-07 | 2021-04-23 | 重庆友利森汽车科技有限公司 | 一种多工头电池框挤压模具 |
US11371709B2 (en) | 2020-06-30 | 2022-06-28 | General Electric Company | Combustor air flow path |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
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JP5641833B2 (ja) * | 2010-09-07 | 2014-12-17 | 昭和電工株式会社 | 押出ダイス |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3527079A (en) * | 1966-08-01 | 1970-09-08 | Dow Chemical Co | Feeder hole die with improved metal flow |
JPH01284423A (ja) * | 1988-05-06 | 1989-11-15 | Showa Alum Corp | 多穴管の押出用ダイス |
US6557388B1 (en) * | 1999-04-06 | 2003-05-06 | The Furukawa Electric Co., Ltd. | Method of determining dimension of extrusion die and extrusion die produced based on the same |
US20040244457A1 (en) * | 2001-10-23 | 2004-12-09 | Kimihisa Hiramoto | Extrusion die for manufacturing tube with small hollow portions, mandrel used for said extrusion die, and multi-hollowed tube manu-factured by using said extrusion die |
EP1630241A1 (de) * | 2003-04-07 | 2006-03-01 | The Society Of Japanese Aerospace Companies | Hochfestes stranggepresstes aluminiumlegierungsmaterial mit hervorragender korrosionsbeständigkeit und herstellungsverfahren dafür |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5143989B2 (de) * | 1973-10-13 | 1976-11-25 | ||
JPS591488B2 (ja) * | 1977-02-18 | 1984-01-12 | 日本軽金属株式会社 | 複雑な形状の押出材の成型用ダイス |
JPS62279019A (ja) * | 1986-05-29 | 1987-12-03 | Furukawa Alum Co Ltd | 仕切り壁を有する中空型材の押出ダイ |
JPH0957334A (ja) * | 1995-08-23 | 1997-03-04 | Showa Alum Corp | 中空材押出用ダイス |
JP3645453B2 (ja) * | 1999-08-05 | 2005-05-11 | 株式会社神戸製鋼所 | 中空形材押出ダイスおよびその設計方法 |
JP3698927B2 (ja) * | 1999-08-31 | 2005-09-21 | 株式会社神戸製鋼所 | 中空形材押出ダイスおよび薄肉中空形材 |
JP3550682B2 (ja) * | 2000-10-23 | 2004-08-04 | 三協アルミニウム工業株式会社 | 押出しダイス |
JP2003071514A (ja) * | 2001-09-04 | 2003-03-11 | Sumitomo Light Metal Ind Ltd | 中空材成形用押出ダイス |
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2006
- 2006-08-03 JP JP2006211962A patent/JP4824499B2/ja not_active Expired - Fee Related
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2007
- 2007-06-14 EP EP20070011703 patent/EP1884297B1/de active Active
-
2008
- 2008-07-21 HK HK08108020A patent/HK1117091A1/xx not_active IP Right Cessation
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3527079A (en) * | 1966-08-01 | 1970-09-08 | Dow Chemical Co | Feeder hole die with improved metal flow |
JPH01284423A (ja) * | 1988-05-06 | 1989-11-15 | Showa Alum Corp | 多穴管の押出用ダイス |
US6557388B1 (en) * | 1999-04-06 | 2003-05-06 | The Furukawa Electric Co., Ltd. | Method of determining dimension of extrusion die and extrusion die produced based on the same |
US20040244457A1 (en) * | 2001-10-23 | 2004-12-09 | Kimihisa Hiramoto | Extrusion die for manufacturing tube with small hollow portions, mandrel used for said extrusion die, and multi-hollowed tube manu-factured by using said extrusion die |
EP1630241A1 (de) * | 2003-04-07 | 2006-03-01 | The Society Of Japanese Aerospace Companies | Hochfestes stranggepresstes aluminiumlegierungsmaterial mit hervorragender korrosionsbeständigkeit und herstellungsverfahren dafür |
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9316155B2 (en) | 2013-03-18 | 2016-04-19 | General Electric Company | System for providing fuel to a combustor |
US9316396B2 (en) | 2013-03-18 | 2016-04-19 | General Electric Company | Hot gas path duct for a combustor of a gas turbine |
US9322556B2 (en) | 2013-03-18 | 2016-04-26 | General Electric Company | Flow sleeve assembly for a combustion module of a gas turbine combustor |
US9360217B2 (en) | 2013-03-18 | 2016-06-07 | General Electric Company | Flow sleeve for a combustion module of a gas turbine |
US9383104B2 (en) | 2013-03-18 | 2016-07-05 | General Electric Company | Continuous combustion liner for a combustor of a gas turbine |
US9400114B2 (en) | 2013-03-18 | 2016-07-26 | General Electric Company | Combustor support assembly for mounting a combustion module of a gas turbine |
US9631812B2 (en) | 2013-03-18 | 2017-04-25 | General Electric Company | Support frame and method for assembly of a combustion module of a gas turbine |
US10436445B2 (en) | 2013-03-18 | 2019-10-08 | General Electric Company | Assembly for controlling clearance between a liner and stationary nozzle within a gas turbine |
US11371709B2 (en) | 2020-06-30 | 2022-06-28 | General Electric Company | Combustor air flow path |
CN112692094A (zh) * | 2020-12-07 | 2021-04-23 | 重庆友利森汽车科技有限公司 | 一种多工头电池框挤压模具 |
Also Published As
Publication number | Publication date |
---|---|
HK1117091A1 (en) | 2009-01-09 |
JP2008036662A (ja) | 2008-02-21 |
EP1884297B1 (de) | 2013-05-29 |
JP4824499B2 (ja) | 2011-11-30 |
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