JPH1052772A - Method for manufacturing honeycomb panel and honeycomb structure - Google Patents

Abstract

PROBLEM TO BE SOLVED: To manufacture a highly precise and inexpensive structure by joining a face plate with a core material using a solid phase joining method utilizing the plastic flow of a metal. SOLUTION: A reinforcing material 3 is arranged between the face plate consisting of an Al alloy and the core material 2, and these are simultaneously joined with the solid phase joining method. That is, a rotating tool 4 is inserted into the joining part among the face plate 1, core material 2 and reinforcing material 3, and the face plate 1, core material 2 and reinforcing material 3 are simultaneously joined by transferring the rotating tool while rotating without melting. Thus, a joined part 5 is formed and the honeycomb panel of high quality is inexpensively manufactured. In other words, the thickness of the face plate 1 or core material 2 becomes thin by using the reinforcing material 3, and even the honeycomb panel uncapable of joining because of deformation due to the load of the rotating tool is easily manufactured. By this way, the joining without any defect is allowed even when the gap in the joining part is large.

Description

DETAILED DESCRIPTION OF THE INVENTION

[0001]

The present invention can be applied to any structure using a honeycomb panel, such as a vehicle, an automobile, a ship, an aviation, an elevator, a pressure vessel and the like.

[0002]

2. Description of the Related Art As a method for manufacturing a honeycomb panel, Japanese Patent Application Laid-Open Nos. 50-60452, 58-134736, 58-196165, 62-16673, 1-48697, 1-48697, and 1-Japanese No. 280613 discloses a manufacturing method using a brazing method.
In Japanese Patent Application Laid-Open No. 63-268, there is disclosed a method of manufacturing by electronic beam.
583, a laser beam in JP-A-1-43349, a resistance welding method in JP-A-1-40180, a diffusion welding in JP-A-1-176454 and JP-A-1-218636, and a fusion welding in JP-A-1-116133. JP-A-58-108128, JP-A-62-25
5132, JP-A-63-206545, JP-A-1-42
No. 297 discloses a manufacturing method using an adhesive. Japanese Patent Application Laid-Open No. 2-109297 is known as a structure of a honeycomb panel manufactured by a brazing method.

[0003] Furthermore, honeycomb panels manufactured by extrusion and drawing processes are also known.

On the other hand, Japanese Patent Application Laid-Open No.
In 05090, a tool made of a material substantially harder than the workpiece is inserted into the welded portion of the workpiece, and the tool is moved while rotating the tool, so that the rotating tool and the workpiece are connected to each other. 2. Description of the Related Art A joining method for joining workpieces by plastic flow due to frictional heat generated during welding is known.

[0005] The conventional friction welding method involves rotating the workpieces and welding by frictional heat between the workpieces. On the other hand, Japanese Patent Application Laid-Open No. 7-505090 discloses a method in which a welding member is fixed. It can be joined by moving the tool while rotating it. Therefore, there is an advantage that even a member that is substantially infinitely long in the welding direction can be continuously solid-phase bonded in the longitudinal direction. Furthermore, for solid-phase joining utilizing the plastic flow of metal due to frictional heat between the rotating tool and the welding member,
Joining can be performed without melting the joining portion. Further, since the heating temperature is low, deformation after bonding is small. Since the joint is not melted, there are many advantages, such as fewer defects.

[0006]

The above-described manufacturing method in which a honeycomb material is melted and welded by a heat source such as an arc, a plasma, an electron beam, or a laser beam causes a large deformation after the manufacturing. , Defects are likely to occur in the weld. In the case of an electron beam, there is a problem that the size and shape of the honeycomb panel are limited because welding is performed in a vacuum. Also, the production cost of lasers and electronic beams is high because the equipment is expensive.

[0007] In the case of the brazing method, there is a problem in the reliability of the brazed portion due to the selection of the brazing material, corrosion by flux, and the like. Furthermore, in the case of brazing in a vacuum, there is a problem that the size and shape of the honeycomb panel are limited.

[0008] The manufacturing method using an adhesive has problems in the strength and reliability of the bonded portion.

A honeycomb panel manufactured by extrusion or drawing has a problem in that the thickness and width of the honeycomb material are limited, and as a result, the weight of the honeycomb panel increases. Further, there is a limit to the size of the honeycomb panel that can be manufactured.

On the other hand, when the above-described method of inserting a rotary tool according to Japanese Patent Application Laid-Open No. 7-505090 into a workpiece and moving the rotary tool while rotating the same is applied to a honeycomb panel. However, there are the following problems.

(1) During welding, the honeycomb panel is deformed by the load of the rotating tool. For this reason, when the face plate and the core material such as the honeycomb panel are thin, it is difficult to join them.

(2) Due to the friction between the rotary tool and the surface of the honeycomb panel, the surface of the joint is dented. For this reason, the thickness of the joint is substantially reduced, so that the strength of the joint is reduced and there is a problem in reliability.

(3) When there is a gap in the joint portion of the joint portion, a defect is easily generated. That is, conventional MIG or T
The allowable range of the gap is narrower than the fusion welding method such as IG.

[0014]

The present invention can be achieved by the following means.

(1) The honeycomb panel is joined to the rotating tool, which is substantially harder than the honeycomb material, by a solid-state joining method using plastic flow.

(2) At the joint of the honeycomb panels, the honeycomb panel is not deformed by the load of the rotating tool.
Reinforcement is provided at the joint.

(3) The connecting portion of the honeycomb panel has a reinforcing structure so as not to be deformed by the load of the rotating tool.

(4) The thickness of the joined portion of the honeycomb panel is higher than other thicknesses.

The increased thickness is desirably 0.3 mm or more and 2 mm or less. The width of the raised portion is preferably substantially the same as the outer shape of the rotary tool flange.

(5) Joining the honeycomb panel from both front and back. This purpose can be achieved by welding from both sides simultaneously or at different times.

(6) A metal tool made of a material substantially harder than the material of the workpiece is inserted into the joint of the workpiece,
A joining structure for joining a substantially continuous member by plastic flow caused by frictional heat between the tool and the workpiece generated by rotating the tool while rotating;
The joining structure is such that a reinforcing material is provided at the joining portion.
Alternatively, the joining structure is reinforced so that the joining portion is not deformed by the load of the rotating tool.

[Operation] According to the present invention, a metal tool made of a material substantially harder than the material of the honeycomb panel is inserted into the joint portion of the honeycomb panel, and the rotation of the tool and the honeycomb material are connected to each other. The honeycomb panel is manufactured by joining by plastic flow due to frictional heat. In order to achieve the above object, the present invention is characterized in that a reinforcing material is provided at the joint of the honeycomb panel or the joint structure of the joint is a reinforcing structure. ADVANTAGE OF THE INVENTION According to this invention, even if it is a honeycomb panel made of a thin face plate, a highly reliable honeycomb panel with little deformation can be manufactured with high accuracy and at low cost. Further, since the honeycomb panel is not melted, it can be joined from both left and right or upper and lower surfaces. For this reason, the honeycomb panel structure can be efficiently and inexpensively manufactured without inverting the honeycomb panel.

A second feature of the present invention is that the joining portion of the honeycomb panel is higher than other portions. As a result, the thickness of the joint is reduced by the cutting effect of the rotary tool, the joint strength is reduced, and a decrease in the reliability of the honeycomb panel can be prevented. Further, by increasing the thickness of the joint, even when the gap of the joint is large, the gap is compensated for at the portion where the thickness is increased.
For example, the joint structure can be joined without defects even if the joint structure is not only the I type but also the L type or V type. This increases the types of joint structures that can be joined by the present welding method.

[0024]

BEST MODE FOR CARRYING OUT THE INVENTION

Embodiment 1 FIG. 1 is a perspective view showing a method for manufacturing a honeycomb panel according to the present invention. FIG. 2 shows a cross section of FIG. In the method for manufacturing a honeycomb panel according to the present invention, a reinforcing material 3 is arranged between a face plate 1 made of an aluminum alloy and a core material 2, and these are simultaneously bonded by a solid-phase bonding method. That is, the first
As shown in FIG. 2 and FIG. 2, the rotary tool 4 is inserted into the joint between the face plate 1, the core member 2 and the reinforcing member 3, and the rotary tool is inserted.
The face plate 1, the core material 2, and the reinforcing material 3 can be joined at the same time by melting while rotating the metal plate. According to the present invention, the joining portion 5 is formed, and a high quality honeycomb panel can be manufactured at low cost. In other words, the honeycomb panel can be easily manufactured even if the thickness of the face plate 1 or the core member 2 is small due to the reinforcing member 3 and the honeycomb panel cannot be joined by being deformed by the load of the rotating tool.

The diameter of the tip of the rotary tool 4 used in this embodiment is 6 mm, the length is 4 mm, and the diameter of the brim portion is 20 mm.
mm. The rotation speed of the rotary tool 4 is 1000
rpm, the moving speed is 500 mm / min. In addition,
An ordinary M screw is formed at the tip of the rotary tool.

Embodiment 2 FIG. 3 shows a cross section of a honeycomb panel having the same shape as the honeycomb panel of FIG. In the present embodiment, a method for manufacturing a honeycomb panel which is simultaneously bonded from both front and back surfaces of the honeycomb panel will be described. That is, the rotating tool 4 is disposed on the front and back of the honeycomb panel, and the face plate 1, the core material 2, and the reinforcing material 3 are joined from both sides by moving the tool 4 while rotating. Thus, a highly accurate honeycomb panel structure can be efficiently manufactured at low cost. The joining conditions in this case are the same as in the first embodiment.

Embodiment 3 FIG. 4 shows the structure of a panel in which a reinforcing member 3 is provided in a part of a panel made of an aluminum alloy. That is, since the core material 2 is corrugated and strong, it supplements the role of the reinforcing material. For this reason, even if the face plate 1 is thin, it can be joined without deformation due to the load of the rotary tool 4. Therefore, the face plate 1 and the core material 2
Can form a structure composed of a honeycomb panel having a lightweight structure in which a sound joining portion 5 is formed.

Embodiment 4 FIG. 5 shows a face plate 1 and a core material 2 made of an aluminum alloy.
The following shows a manufacturing method in which a rotary tool is inserted into the two joints of the above and the two joints are simultaneously joined. In the present invention, the core material 2 supplements the role of the reinforcing material. That is, since the core material 2 is sufficiently strong to withstand the load of the rotating tool 4,
Even when the face plate 1 is thin, the noodle plate 1 and the core material 2 can be joined without deformation. Thus, a highly accurate honeycomb panel structure can be manufactured. The joining conditions are the same as in the first embodiment.

Example 5 FIG. 6 shows a face plate 1 and a core made by extrusion.
By inserting the rotating tool 4 between the honeycomb panels made of the material 2 and the edge material 6 into the portion of the edge material 6, a solid-phase joining portion 5 is formed,
A large honeycomb panel structure is manufactured. That is, the face plate 1, the core material 2, and the edge material 6 are formed by the extrusion method.
The edge material 6 at the end of the honeycomb formed integrally is the reinforcing material of the present invention. Even when the face plate 1 and the core material 2 are thin, they are not deformed by the load of the rotary tool 4. Can be joined. Therefore, a lightweight, high-precision, large-sized honeycomb panel structure can be efficiently and inexpensively manufactured. A high-speed vehicle was manufactured using this honeycomb panel as a railway vehicle body.

Example 6 FIG. 7 shows a face plate 1 and a core made by extrusion.
The honeycomb panels made of the material 2 and the edge material 6 are joined by inserting the rotary tool 4 into the edge material portion. Thus, a large honeycomb structure is manufactured by combining a plurality of honeycomb panels. In the present embodiment, the thickness of the joint portion where the rotary tool 4 contacts is increased by 0.8 mm. As a result, the strength is not substantially reduced even when the joint is depressed by the rotary tool 4. Furthermore, even if the gap at the joint is large, joining can be performed without defects. For this reason, the structure consisting of highly reliable honeycomb panels is efficiently used.
And it can be manufactured at low cost. A high-speed vehicle was manufactured using this honeycomb panel as a railway vehicle body.

Example 7 FIG. 8 shows a face plate 1 manufactured by extrusion and a core.
In joining the honeycomb panels made of the material 2, the reinforcing material 6 is disposed between the honeycomb panels, and the rotary tool 4 is inserted into the reinforcing material portion and joined. Thus, a large honeycomb structure is manufactured by combining a plurality of honeycomb panels. In the present embodiment, the thickness of the reinforcing material at the joint where the rotary tool 4 contacts is increased by 1 mm. As a result, the strength is not substantially reduced even when the joint is depressed by the rotary tool 4. Furthermore, even if the gap at the joint is large, joining can be performed without defects. For this reason, a structure made of a highly reliable honeycomb panel can be manufactured efficiently and at low cost. A high-speed vehicle was manufactured using this honeycomb panel as a railway vehicle body.

Embodiment 8 FIG. 9 is a perspective view of a honeycomb panel manufactured by a brazing method using plastic flow caused by frictional heat between a rotary tool 4 and a honeycomb material.

FIG. 10 shows the sectional structure of FIG. As shown in FIGS. 9 and 10, the face plate 1, the core material 2, and the edge material 6 are joined by a brazing layer 7. The joining of the honeycomb panels according to the present invention is performed at the edge member 6. That is, the edge member 6 supplements the role of the reinforcing member against the load of the rotating tool, and can be joined without deformation even when the face plate 1 and the core member 2 are thin. According to the above-described method, a large-sized honeycomb panel structure can be manufactured by a solid-phase joining method between honeycomb panels joined by a brazing method.

Using this honeycomb panel as a railway vehicle body, a high-speed vehicle was manufactured.

Embodiment 9 FIG. 11 is a perspective view of a method for manufacturing a railway vehicle according to the present invention. First, the rotary tool 4 is inserted into the edge material 6 of a honeycomb panel having a length of 25 m and a width of 0.4 m manufactured by an extrusion method, and the honeycomb panels are solid-phase bonded from both sides.

FIG. 12 shows a detailed sectional structure of the manufacturing method of FIG. A honeycomb panel including a face plate 1, a core material 2, and a rim material 6 manufactured by an extrusion method is disposed on a fixed base, and is fixed by a fixing jig 7 from right and left and up and down directions. In this embodiment, the height of the face plate at the joint is about 0.6 mm higher than other portions. The joining is performed by rotating the tool 4 from above and below on the edge 6 of the honeycomb panel.
Insert The rotary tool is attached to the robot 8 and moves in the direction of the welding line while rotating by the driving force of the motor 9. By the above method, the honeycomb panels are solid-phase bonded to each other. The rotation tool can be automatically moved up and down according to the deformation of the honeycomb panel surface.
Further, the rotary tool 4 can be automatically moved in the left-right direction along the welding line.

FIG. 13 is a perspective view of a railway vehicle manufactured by the above method. Part of the length of the joint 5 is 12.5
m, but a maximum length of 25 m is formed from the front and back use surfaces to produce a railway vehicle.

Embodiment 9 FIG. 14 shows a joint structure of a joint according to the present invention. FIGS. 14A to 14E show an example in which a reinforcing member 3 is provided in joining the face plates 1 of the honeycomb panel. In other words, a reinforcing member 3 that is not deformed by the load of the rotating tool 4 is disposed below the left and right face plates 1 to be joined, and the reinforcing members 3 are also joined together. Thereby, the face plate 1 of the joining member
Can be solid-phase bonded even with an infinitely long honeycomb without being deformed by the load of the rotating tool. FIGS. 15A and 15B show an example in which one of the face plates 1 is manufactured integrally with the reinforcing member 3. That is, the load of the rotating tool is supported by the reinforcing member 3 integrated with the face plate 1.

FIGS. 16 (a) to 16 (d) show a joint structure in which both the face plate 1 and the reinforcing member 3 are integrally formed. In this case, the load of the rotating tool is supported by both reinforcing members 3.

FIGS. 17A to 17E show a joint structure in which the thickness of the joint is thicker than other portions.
(A) and (b) show an I-shaped joint structure, (c) and (d) show a Le-shaped joint structure, and (e) and (f) show a V-shaped joint structure. That is, by increasing the thickness of the joint by 0.3 mm or more from the other portions, the space in the gap of each joint structure is replenished with the increased thickness of the joint. The range can be increased. In addition, since the space can be replenished even in the case of a re-type or a V-type, bonding can be performed without defects.

[Structure of the Present Invention] The structure of the present invention is achieved by one or more of the following. (1) A reinforcing material is provided at a joint or a reinforcing structure is provided.

(2) The thickness of the joining portion is made thicker than other portions.

(3) Joining from both front and back sides of the honeycomb panel.

[0044]

According to the present invention, by providing a reinforcing material at the joint portion or by using a reinforcing structure, even when the face plate and the core material of the honeycomb panel are thin, they can be manufactured with high precision and at low cost. In addition, by increasing the thickness of the joining portion compared to other portions, joining can be performed without defects even when the gap at the joining portion is large. Furthermore, by joining from both sides, a honeycomb panel and a structure composed of honeycomb panels can be efficiently manufactured.

[Brief description of the drawings]

FIG. 1 is a perspective view showing a method for manufacturing a honeycomb panel of the present invention.

FIG. 2 is a longitudinal sectional view of FIG.

FIG. 3 is a cross-sectional view illustrating a manufacturing method according to another embodiment.

FIG. 4 is a longitudinal sectional view showing a manufacturing method of another embodiment.

FIG. 5 is a cross-sectional view illustrating a manufacturing method according to another embodiment.

FIG. 6 is a cross-sectional view illustrating a manufacturing method according to another embodiment.

FIG. 7 is a cross-sectional view illustrating a manufacturing method according to another embodiment.

FIG. 8 is a cross-sectional view illustrating a manufacturing method according to another embodiment.

FIG. 9 is a perspective view of solid-state joining of honeycomb panels manufactured by a brazing method.

FIG. 10 is a longitudinal sectional view of a main part of FIG. 9;

FIG. 11 is a perspective view showing an embodiment for manufacturing a panel of a railway vehicle.

FIG. 12 is a longitudinal sectional view of a main part of FIG. 11;

FIG. 13 is a perspective view of a vehicle body of a railway vehicle.

FIG. 14 is a longitudinal sectional view showing various joint structures of the present invention.

FIG. 15 is a longitudinal sectional view showing various joint structures of the present invention.

FIG. 16 is a longitudinal sectional view showing various joint structures of the present invention.

FIG. 17 is a longitudinal sectional view showing various joint structures of the present invention.

[Explanation of symbols]

 1: face plate, 2: core material, 3: reinforcing material, 5: joint.

Continued on the front page (51) Int.Cl. ⁶ Identification number Office reference number FI Technical display location B61D 17/00 B61D 17/00 C 17/04 17/04 // B23K 101: 02 (72) Inventor Kinya Aota 794, Higashi-Toyoi, Hitachi, Ltd., Kudamatsu City, Yamaguchi Prefecture (72) Inventor Masakuni Esumi, Masanori Esumi 794, Higashi-Toyoi, Kazamatsu City, Yamaguchi Prefecture, Japan In Kasado Plant, Hitachi, Ltd. (72) Inventor, Yasuo Ishimaru 794 Kazamatsu, Kudamatsu City, Yamaguchi Prefecture Inside the Kasado Plant of Hitachi, Ltd.

Claims (12)

[Claims] 1. A method for manufacturing a honeycomb panel basically comprising a face plate and a core material, wherein the bonding between the face plate and the core material is performed by a solid-phase bonding method utilizing plastic flow of metal. Characteristic method of manufacturing honeycomb panel. 2. The solid-phase joining method according to claim 1, wherein the rod-shaped tool made of a material substantially harder than the material of the honeycomb panel.
The tool is generated by inserting a tool into a joint portion of the honeycomb panel and moving the tool while rotating the tool.
A method for manufacturing a honeycomb panel, which is a joining method utilizing frictional heat between the honeycomb panel and the honeycomb material. 3. A method for manufacturing a honeycomb panel according to claim 1, wherein a reinforcing material is provided at a joint portion of the honeycomb panel, and the reinforcing material is simultaneously bonded. 4. The method of manufacturing a honeycomb panel according to claim 1, wherein the thickness of the joined portion of the honeycomb panel is 0.3 mm or more higher than other portions. 5. The method for manufacturing a honeycomb panel according to claim 1, wherein the honeycomb panel is joined from both front and back surfaces. 6. A tool formed by inserting a metal tool made of a material substantially harder than the material of the workpiece into the joint of the workpiece and moving the tool while rotating the tool.
A joining structure for joining substantially continuous members by plastic flow caused by frictional heat between the metal plate and the workpiece, wherein a reinforcing material is provided at the joining portion. 7. A tool made by inserting a metal tool made of a material substantially harder than the material of a workpiece into a joint of the workpiece and moving the tool while rotating the tool. In a joining structure for joining a substantially continuous member by plastic flow due to frictional heat between the tool and the workpiece, the joining portion is a reinforcing structure that substantially withstands the load of the tool. Honeycomb panel joint structure. 8. A tool formed by inserting a metal tool made of a material substantially harder than the material of the workpiece into the joint of the workpiece and moving the tool while rotating the tool.
In a joining structure for joining a substantially continuous member by plastic flow due to frictional heat of the workpiece and the workpiece, a thickness of the joining portion is larger than other portions of the honeycomb panel. Joint structure. 9. A tool formed by inserting a metal tool made of a material substantially harder than the material of a workpiece into a joint portion of the workpiece and moving the tool while rotating the tool. A method of joining substantially continuous members by plastic flow caused by frictional heat between a metal panel and a workpiece, wherein the honeycomb panel is joined from both front and back surfaces. 10. A honeycomb panel structure according to any one of claims 1 to 9, wherein the honeycomb panel is made of Al or an Al alloy. 11. A honeycomb structure manufactured by the method according to any one of claims 1 to 10. 12. A railway vehicle body comprising a honeycomb panel manufactured by the method according to any one of claims 1 to 11.