Patent Application
20050140045
The present application is based on and claims priority of Japanese patent application No. 2003-433888 filed on Dec. 26, 2003, the entire contents of which are hereby incorporated by reference.
1. Field of the invention
The present invention relates to a method and apparatus for molding a thermosetting composite material used for example for forming aircrafts and vehicles.
2. Description of the related art
Aircrafts have many curved surfaces in the main portions of the airframe including the body, the main plane and the tail plane in order to enhance the performance of the airframe, and the aircrafts adopt a semimonocoque construction in which beams and skin layers are assembled together. Along with the growth in size of the aircrafts, it has become essential to reduce the weight of the airframe, so during the recent years, the use of composite materials containing reinforced fiber such as carbon fiber have increased.
The preferred main material for forming a primary structure is a combination of carbon fiber-epoxy resin (having thermosetting property) that satisfies the required performance, which in many cases is processed in the form of a prepreg to assure stability of quality.
According to the conventional molding method, prepregs or other materials are layered in a mold, which are then vacuumed, heated and pressed in an autoclave (pressure vessel).
This conventional method can be applied in the following ways, for example, to form a main plane of an aircraft.
According to above method 1, the prepregs are softened when heat is applied thereto, so the method requires molds to be disposed at both the upper surface and the lower surface of the prepregs that have high accuracy and that can apply pressure evenly to the layered prepregs. As for methods 2 and 3, it is sufficient to dispose a rubber-like mold to correspond to the upper surface of the prepregs, but these methods require a separate mold for forming the beams.
A method for continuously molding a prepreg material is proposed by the present applicant and disclosed in the patent document mentioned below. By changing a portion of this molding apparatus, it is possible to control the curing reaction of the prepreg. The general outline of the apparatus will be described using an L-shaped member as an example. The prepreg materials cut into slits having predetermined widths are set to required number of rolls, and after layering a predetermined number of prepreg sheets, release films are disposed on the upper and lower surfaces of the layered sheets. Next, the prepreg with release films disposed on the upper and lower surfaces thereof is deformed gradually into an L-shape, and then pulled into a hot-press which is heated to a fixed temperature. The hot-press is interlocked with a puller mentioned in detail later, and pulls in a predetermined amount of prepreg when it is opened. The curing reaction of the laminated prepreg progresses as the prepreg passes through the hot-press, and the air between the layers are pushed out so that the prepreg is formed into a shape close to its final form. A device for cooling the prepreg is disposed directly after the hot-press, in which the prepreg is cooled and further curing reaction is suppressed. A puller for pulling the prepreg is disposed directly after the cooling device, which controls the time and the amount of pulling the prepreg per one process cycle with respect to the temperature of the hot-press so that a predetermined amount of heat is constantly provided to the prepreg. The prepreg being pulled out by the puller is cut into predetermined lengths.
The prepreg having passed through the aforementioned processes is formed into a shape close to its final form, and the curing reaction thereof is progressed to a certain extent, but by returning the prepreg to room temperature, further reaction is stopped (this prepreg is hereinafter referred to as preform).
The preform being cut to predetermined lengths is then deformed into desired shapes by either of the two following methods.
The deformed preform is then set together with a prepreg serving as the skin layer, and after further setting a release film, an upper rubber mold, a vacuum film and so on, the set preform is subjected to vacuuming and integral molding in an autoclave.
The present invention provides a method and an apparatus for molding a composite material that is capable of saving work for prepreg lamination, cutting down other materials used for autoclave molding and reducing the number of required molds, by continuously molding a beam member while controlling the curing rate of the prepreg, and by subjecting the beam member having been deformed into the desired shape to integral molding with a skin layer.
The method for molding a thermosetting composite material which is a prepreg material formed by impregnating a carbon fiber or a glass fiber with thermosetting resin and semi-curing the same includes continuously layering sheet-shaped prepreg materials and forming the same into a desired shape; and heating the formed prepreg material in a mold for a predetermined time and controlling a curing rate F of the prepreg material so as to mold a linear-shaped preform.
Here, curing rate F can be defined by the following equation:
F=[(B−A)/B]×100(%),
Further, the method includes cutting the preform into a predetermined length; and deforming a part or an entirety of the preform cut into the predetermined length using a hot press while controlling the curing rate thereof.
The present invention is also capable of molding a product having a curved surface by attaching a molded product to a sheet-shaped prepreg material.
Moreover, the present invention provides a molding apparatus for a thermosetting composite material in which a preform of a prepreg material molded linearly is molded into a curved shape, the apparatus comprising: a hot press unit having a mold with a curvature; a cold press unit having a mold with a curvature disposed immediately subsequent to the hot press unit; and a feeder for feeding the mold along the curvature.
The present invention enables to form the outer panel of an aircraft formed of curved surfaces or the like using a thermosetting composite material.
Product 10 is a structural member of an aircraft, for example, wherein channel members 30 for reinforcement made of thermosetting composite material are integrally attached to the inner side of a plate member 20 formed of thermosetting composite material.
This product comprises a curved surface, and can be applied as an outer panel of an aircraft.
The plate member 20 can be formed by mounting a material on a mold member corresponding to the desired curved surface and molding the same in an autoclave or other devices, but the channel member 30 cannot be molded to have the desired curved shape by the same process as forming the plate member 20.
The present invention provides a method and apparatus for molding the channel member with a curvature in advance.
The linear L-shaped channel member 120 having been subjected to primary molding is then cut into predetermined lengths by a cutting means C1, and stored in a freezer 250.
The curing rate of this primary-molded preform is 40 to 60%.
The mold temperature of the hot press unit is 170° C.
The long channel member 120 is bent in a secondary molding device 300 to have a radius of curvature R1. The radius of curvature R1 can be, for example, as large as 3 m.
The secondary molding device 300 includes a hot press unit 310 and a cold press unit 320, and continuously molds the straight channel member 120 into an arc. The continuously molded channel member is cut into predetermined lengths by a cutting means C2, so as to form the L-shaped channel members 30 used for reinforcement of the product 10.
If necessary, the L-shaped channel members 30 are stored in a freezer 260. The curing rate of the molded L-shaped channel member 30 is around 60 to 80%.
The secondary molding device, the entire body of which is denoted by reference number 300, comprises a hot press unit 310 and a cold press unit 320 equipped inside a frame 302.
The hot press unit 310 comprises a fixed mold 314 and a movable mold 312, and the movable mold 312 can be moved toward and away from the fixed mold 314 via the movement of a rod 332 in the direction of arrow A driven by a cylinder 330.
The movable mold 312 and the fixed mold 314 of the hot press unit 310 are equipped with electrical or other heating means, and carries out the molding process by adding heat and pressure to the primary molded channel member 120 being supplied thereto.
The cold press unit 320 comprises a fixed mold 324 and a movable mold 322, and the movable mold 322 can be moved toward and away from the fixed mold 324 via the movement of the rod 332 in the direction of arrow A driven by the cylinder 330.
The movable mold 322 and the fixed mold 324 of the cold press unit 320 are equipped with a cooling means, so as to cool the molded channel member to stop the progress of the thermosetting process.
The channel member 120 passing through the secondary molding device 120 is held between pinch rollers 340, 350 and sent toward the direction of arrow F.
A cam plate 360 is attached beneath the frame 302 of the secondary molding device 300, and the cam plate 360 is supported via plural rollers 362.
A cylinder 372 of a feeder 370 of the mold comprises a rod 374 driven in the direction of arrow S, and the front end of a rod 374 is connected via a universal joint 376 to the cam plate 360.
While the molds of the hot press unit 310 and the cold press unit 320 are opened, the rod 374 of the feeder 370 is returned to its original position.
Then, the molds are closed to perform molding and cooling, and the rod 374 of the feeder 370 is elongated to move the entire body of the frame 302 including the molds in the forward direction. By the action of the cam plate 360, this forward movement is set to correspond to the radius of curvature of the L-shaped channel member subjected to secondary molding.
In other words, the cam profile 360a of the cam plate 360 has the same radius of curvature as that of the L-shaped channel member subjected to secondary molding.
After the termination of a pressing process which had been carried out for a predetermined amount of time, the molds are opened and the feeder is returned to its original position.
The above processes are repeatedly performed to form the secondary molded product.
According to the present embodiment, the radius of curvature is set to 3 m, and the mold temperature of the hot press unit is set between 160 and 180° C.
In order to attach the product 10 which is not yet completely cured to the mold member 400, methods such as storing the entire body into an airtight bag and reducing the interior pressure of the bag to negative pressure so as to attach the product 10 to the mold member 400 or pressing the product 10 onto the mold member 400 using a press means are adopted.
According to either method, the channel members 30 subjected to secondary molding and having a predetermined curvature are attached to the back side of the sheet member 20, which are subjected to thermosetting until its curing rate reaches 100%, so as to form a composite material product having a predetermined curvature which is light weight and strong.
As described, the present invention enables to manufacture a structural member with a curved surface for an aircraft, a vehicle or the like, which is required to be light weight and strong.
| Number | Date | Country | Kind |
|---|---|---|---|
| 2003-433888 | Dec 2003 | JP | national |
