Tool sleeve for mold die

Abstract

A device changes the shape of a die used to compression mold a part. The device includes a sleeve placed between the die and a charge to be molded. The sleeve has an inner face generally conforming to a face of the die, and a outer face for molding a part.

Claims

1. A device comprising: a die for use in continuous compression molding a part; a plurality of sleeves disposable between the die and a charge to be molded into the part, each of the plurality of sleeves having a respective shape related to a shape of the part to be formed using the plurality of sleeves, each of the plurality of sleeves having a first corresponding shape different than every other sleeve of the plurality of sleeves, each of the plurality of sleeves having a corresponding inner face having a second corresponding shape that substantially matches a cross sectional shape of the die, wherein the plurality of sleeves are removable from the die during a compression molding operation to form the part and installable onto the die to fully cover a face of the die during the compression molding operation.

2. The device of claim 1, wherein the plurality of sleeves include cavities on the corresponding inner face.

3. The device of claim 1 further comprising: at least one shim for filling a gap between a sleeve of the plurality of sleeves and the die.

4. The device of claim 1, wherein: for a first sleeve in the plurality of sleeves, a first portion of the die and a second portion of the first sleeve have different contours.

5. The device of claim 4, wherein: a third portion of the die and the second portion of the sleeve have substantially the same contours.

6. The device of claim 4, wherein the different contours include at least one of: a radius, a wall thickness, and a joggle.

7. The device of claim 1, wherein the sleeve a first sleeve in the plurality of sleeves has a curved longitudinal axis.

8. A device for changing a shape of a part that may be molded by a compression molding die having a fixed shape, comprising: a plurality of sleeves disposable between the compression molding die and a charge to be molded into the part, each of the plurality of sleeves having a respective shape related to a shape of the part to be formed using the plurality of sleeves, each of the plurality of sleeves having a first corresponding shape different than every other sleeve of the plurality of sleeves, each of the plurality of sleeves having a corresponding inner face having a second corresponding shape that substantially matches a cross sectional shape of the compression molding die, wherein the plurality of sleeves are removable from the compression molding die during a compression molding operation to form the part and installable onto the compression molding die to fully cover a face of the die during the compression molding operation.

9. The device of claim 8, wherein the plurality of sleeves include corresponding thicknesses related to a thickness of the part.

10. The device of claim 8, wherein: the plurality of sleeves are configured to be sleeved over the compression molding die.

11. The device of claim 8, wherein the plurality of sleeves are elongate and have thicknesses that vary along lengths of the plurality of sleeves.

12. The device of claim 8, wherein the plurality of sleeves include outer faces configured to mold into the part at least one of: a radius, a changing wall thickness, and a ramp.

13. The device of claim 8, wherein a first sleeve of the plurality of sleeves has a curved longitudinal axis.

14. The device of claim 8, wherein the plurality of sleeves are formed of at least one of: metal, synthetic polymer, ceramic, and composites.

15. A device for compression molding a family of parts using a same mold die, comprising: a plurality of tool sleeves, each of which tool sleeves may be placed between the mold die and a charge to be molded, each of the plurality of tool sleeves having a respective shape related to a shape of the part to be formed using the plurality of tool sleeves, each of the plurality of tool sleeves having a first corresponding shape different than every other tool sleeve of the plurality of tool sleeves, wherein the plurality of tool sleeves are removable from the die during compression molding operation to form the part and installable onto the die to fully cover a face of the die during the compression molding operation the plurality of tool sleeves each including a corresponding inner face substantially conforming to a shape of the mold die and covering sides of the mold die, and a corresponding outer face for molding one of the parts in the family of parts, each of the plurality of tool sleeves filling a space between the charge being molded and the mold die, and having a feature unique to one of the parts, wherein the feature is one of a thickness, a corner radius, a ramp, a step and a contour.

16. The device of claim 15, wherein, as a whole, the plurality of tool sleeves have features that provide at least two of the thickness, the corer radius, the ramp, the step, and the contour.

17. The device of claim 15, wherein, as a whole, the plurality of tool sleeves have features that provide all of the thickness, the corer radius, the ramp, the step, and the contour.

Description

BRIEF DESCRIPTION OF THE ILLUSTRATIONS

(1) FIG. 1 is an illustration of a cross section of a part being molded by a compression die having a tool sleeve installed thereon according to the disclosed embodiments.

(2) FIG. 2 is an illustration of a plan view of the part molded by the die and tool sleeve shown in FIG. 1.

(3) FIG. 2A is an illustration of a perspective view of a tool sleeve that is curved along its longitudinal axis.

(4) FIG. 3A is an illustration of a cross section of the die shown in FIG. 1, having molded a part without the use of the tool sleeve.

(5) FIG. 3B is an illustration similar FIG. 3A but wherein a tool sleeve has been installed on the die for molding a variation of the part shown in FIG. 3A.

(6) FIG. 3C is an illustration similar to FIG. 3B but showing another tool sleeve having been installed on the die for molding a second variation of the part shown in FIG. 3A.

(7) FIG. 4 is an illustration of a sectional view of a tool sleeve on a die used to mold a part having a step feature.

(8) FIG. 5 is an illustration of a sectional view of another tool sleeve on the die shown in FIG. 4, used to mold a part having a ramp feature.

(9) FIG. 6 is an illustration of a further tool sleeve on the die shown in FIG. 4, used to mold a part having a gradually tapering thickness.

(10) FIG. 7 is a an illustration of a longitudinal side view of a pair of dies using a tool sleeve to compression mold a part according to another embodiment.

(11) FIG. 8 is an illustration of a sectional view taken along the line 8-8 in FIG. 7.

(12) FIG. 9 is an illustration of a sectional view taken along the line 9-9 in FIG. 7.

(13) FIG. 10 is an illustration of a method of molding parts using the tool sleeve.

(14) FIG. 11 is an illustration of a flow diagram of an exemplary aircraft manufacturing and service method.

(15) FIG. 12 is an illustration of a block diagram of an aircraft.

DETAILED DESCRIPTION

(16) Referring first to FIGS. 1 and 2, a die 22 includes a fixed die face 23 used to compression mold a part 20 which may be for example and without limitation, a fiber reinforced thermoplastic. The part 20 may be molded from a charge (not shown) and may comprise any of a variety of thermoplastic resins. The resins may include, but are not limited to PEKK, PPS, and PEI, reinforced with any of a variety of fibers, including but not limited to carbon, fiberglass and other fibers. The fixed die face 23 includes a bottom face 23a and side faces 23b. As used herein, a fixed die face and fixed shape die refer to the fact that the shape and dimensions of the die 22, including those of the die face 23, are fixed, or constant, due to the fact that the die 22 is formed from hard materials such as, without limitation, tool steel, aluminum, ceramic or composites. Thus, features of the die may not be readily altered except by machining or similar processes.

(17) In the illustrated example, the part 20 is an elongate structural member having a substantially C-shaped cross section defined by a web 26 connecting a pair of flanges 28, 30. The die 22 compresses the charge (not shown) against a lower die 27a which applies a reaction force indicated by the arrows 21 against the bottom face 23a of the die 22. Additionally, dies 27b may apply reaction forces in the direction of the arrows 31 against the side faces 23b of the die 22 in order to form the pair of flanges 28, 30.

(18) Although not shown in the drawings, the die 22 illustrated in FIG. 1 may be used in any of a variety of compression molding machines, including continuous compression molding machines as described in the following U.S. patent applications, the disclosures of all of which applications are incorporated by reference herein: Ser. No. 11/347,122 filed Feb. 2, 2000; Ser. No. 11/584,923 filed Oct. 20, 2006; Ser. No. 11/701,789 filed Feb. 3, 2007; and, Ser. No. 11/699,653 filed Jan. 29, 2007.

(19) In accordance with the disclosed embodiment, a tool sleeve 24 may be installed on the die 22 to alter the shape of a part molded by the die 22. As used herein, shape is intended to include the size and/or dimensions and/or geometry of a part 20, such as the length, width, thickness and/or contour of the part 20. In effect, the tool sleeve 24 changes the shape of the fixed die face 23 so that the same die 22 may be used to mold parts having shapes that are different from that which could be molded by the die 22 itself. The tool sleeve 24 may comprise, without limitation, steel, a synthetic polymer such as a thermoplastic, ceramic or a composite, and may be fabricated by any suitable forming or molding techniques that are rapid and low cost. In this example, the tool sleeve 24 has a constant thickness bottom 45 and constant thickness sides 53 forming a cavity 55 for receiving the die 22 therein. However, as will be discussed below, the tool sleeve 24 may have a varying thickness either along its length or its width. The bottom 45 of the tool sleeve 24 includes a first, inner face 65 and a second, outer face 67. When the tool sleeve 24 is installed on the die 22, the bottom face 23a of the die 22 engages the inner face 65 of the tool sleeve 24, and the sides 53 the tool sleeve 24 engage the side faces 23b of the die 22. It should be noted here that where the die 22 is curved (not shown), the tool sleeve 24 may be similarly curved along its longitudinal axis 37, as shown in FIG. 2A. Also, it should be noted that while the tool sleeve 24 is shown installed between the die 22 and the charge (not shown) that is molded into the part 20, the tool sleeve 24 may be installed between the charge and the dies 27A and 27B. In some embodiments, sleeves 24 may be installed both between the charge and the die 22, and between the charge and the dies 27A and/or 27B.

(20) The sleeve 24 is removably installed on the die 22. Thus, several different sleeves 24 may be used with a single die 22 to mold differently shaped parts. In the illustrated example, the sides 53 of the sleeve 24 may be sleeved over the die 22 during installation of the sleeve 24. In other embodiments, the sleeve 24 may not include sides 53 and other means (not shown) may be used to hold the sleeve 24 on the face 23 of the die 22.

(21) A gap 51 may be present between the die 22 and the tool sleeve 24 in order to accommodate machining tolerance build-up and/or thermal expansion. As will be discussed later, a shim (not shown) formed of brass, steel or other materials may be placed in the gap 51 to provide a tight fit between the die 22 and the tool sleeve 24.

(22) Although the tool sleeve 24 illustrated in FIGS. 1 and 2 has a C-shaped cross section as, the tool sleeve 24 and related method may be employed to produce parts having a variety of other cross sectional shapes possessing varying dimensions and features, including, but not limited to T, I and J shapes.

(23) As will be discussed below, the bottom 45 and sides 53 of the tool sleeve 24 may have a constant thickness or variable thickness along its length to mold parts of various dimensions and/or shapes while using the same die 22, the shape and dimensions of which are fixed. In other words, the die 22 has a fixed cross sectional shape. The contour of the outer face 67 of the tool sleeve 24 that engages the charge (not shown) is constant, for constant thickness parts, or may be variable for parts that have joggles or stepped or varying thicknesses along their length. The contour of the inner face 65 of the tool sleeve 24 that contacts the die 22 is constant, and matches or conforms to the constant contour of the die face 23. It is possible for the die face 23 to have a contour that is not constant, in which case the inner face 65 of the tool sleeve will be formed to have a contour that conforms to the contour of the die face 23.

(24) The tool sleeve 24 may include features such as outside radiused corners 47 having radii r1 which may different from the corresponding radii on the corners 26b of the die 22. In the illustrated example, because of the presence of the side walls 53 on the tool sleeve 24, the overall width 25 of the part 20 is greater than the width of the part that would be molded using the die 22 without the tool sleeve 24. Also, although the outer face 67 of the tool sleeve 24 is shown as being flat across its width (cross section), the outer face 67 may be curved across its width or have other contours. Similarly, the outer face 67 of the side walls 53 of the tool sleeve 24 may also be curved over their heights or along their lengths, or have other contours.

(25) FIG. 3A illustrates a part comprising a molded C-shaped channel 20a that is molded with the die 22, without the use of the tool sleeve 24. The molded C-shaped channel 20a has a Height 1a, and a Width 2a.

(26) FIG. 3B illustrates the die 22 shown in FIG. 3A fitted with a first sleeve 24a using a shim 34 of suitable thickness to create a substantially tight fit between the first sleeve 24a and the die 22. As of a result of the thickness t.sub.1 added by the first sleeve 24a, the Height 1b and Width 2b of a molded C-shaped channel 20b are respectively greater than the Height 1a and Width 2a of channel 20a shown in FIG. 3A. In addition, the first sleeve 24a includes an outside corner radius 29 that is dimensioned to mold an inside radius r.sub.3 in the channel 20b which is tighter (less) than radius r.sub.2 of channel 20a shown in FIG. 3A.

(27) FIG. 3C illustrates another C-shaped channel 20c that is molded using a sleeve 24b fitted over the die 22 using a shim 34. In this example, the wall thickness t.sub.2 of the sleeve 24b is greater than the wall thickness t.sub.1 of the sleeve 24a shown in FIG. 3B. As a result of this increased wall thickness t.sub.2, the molded C-shaped channel 20c has a Height 3 and Width 3 which are respectively greater than the Height 2 and Width 2 of the channel 20b shown in FIG. 3B.

(28) From FIGS. 3A-3C, it is apparent that various dimensions and features of a part such as the part 20 can be varied using differently shaped and/or dimensioned sleeves 24a fitted onto a single die 22 having a fixed shape and dimensions.

(29) As previously mentioned, the sleeve 24 may be used with a single die 22 of fixed shape and dimensions to produce any of a variety of features in a part, in addition to altering the dimensions of the part as previously discussed in connection with FIGS. 3A-3C. For example, referring to FIG. 4, a sleeve 24c fitted over a die 22 may be employed to mold a step feature 35 into a part 20d along at least a portion of its length. Similarly, as shown in FIG. 5, a sleeve 24d fitted over the die 22 is employed to mold a joggle or ramp feature 39 into a part 20e along at least a portion of its length. FIG. 6 illustrates a sleeve 24e fitted over the die 22 to mold a linearly changing thickness 41 along at least a portion of the length of a part 20f.

(30) Attention is now directed to FIGS. 7-9 which illustrate another embodiment of a tool sleeve 42 that may be used in conjunction with a single set of dies 38, 40 to mold a thermoplastic composite part 36 having an L-shaped cross section. The sleeve 42 may be formed as by molding a suitable material such as thermoplastic, and may be used in conjunction with a single set of dies 38, 40 to mold a thermoplastic composite part. An L-shaped cross section is illustrated in FIGS. 8 and 9. However, a variety of other cross sectional shapes may be molded using the sleeve 42, including but not limited to I, C, T and J shapes. The thermoplastic composite part 36 molded by the sleeve 42 may have a constant or stepped thickness along its length L (FIG. 7) that is different than the single constant thickness cross section part that could be molded using the dies 38, 40 without the use of the sleeve 42.

(31) In the illustrated example, the thermoplastic composite part 36 includes a section 44 of reduced thickness t.sub.1 (FIG. 8) and a double stepped section 46 along its length. Sleeve 42 has an increased thickness t.sub.2 along section 44 so as to at least substantially fill the space W between the dies 38, 40. As shown in FIG. 9, the thermoplastic composite part 36 has a greater thickness t.sub.3 along section 48, and accordingly the sleeve 42 has corresponding reduced thickness t.sub.4 along section 48. Thus, it can be appreciated from FIGS. 7-9 that the sleeve 42 is designed to fill the space between the dies 38, 40 and the thermoplastic composite part 36. A release layer 50 may be placed between the thermoplastic composite part 36 and the sleeve 42 to facilitate ease of separation of the thermoplastic composite part 36 from the sleeve 42. The release layer 50 may be formed of any of various materials such as, for example and without limitation, Kapton film or a metal foil.

(32) FIG. 10 broadly illustrates the steps of a method of compression molding parts using tool sleeves 24, 42 of the type previously described in conjunction with a die having a substantially constant shape and fixed dimensions. Starting at 51, one or more tool sleeves 24, 42 are produced in which outer face 67 of the tool sleeve 24, 42 substantially matches the size and shape of a die 22. The inner face 65 of the tool sleeve 24, 42 fills the space between the die 22 and a part 20 to be molded. Next, at 52, a tool sleeve 24, 42 having the desired shape is selected which corresponds to the desired part 20. At 54, the selected tool sleeve 24, 42 is installed, either by fitting the tool sleeve 24, 42 over one of the dies 22, or by placing the tool sleeve 24, 42 between dies 38, 40 in a die set. At step 56, a charge is placed between the installed tool sleeve 24, 42 and the die 22, and the charge is then compression molded into the part 20. Following molding of the thermoplastic composite part 36, the tool sleeve 24, 42 may be used to mold additional parts using the dies 22.

(33) Embodiments of the disclosure may find use in a variety of potential applications, particularly in the transportation industry, including for example, aerospace, marine and automotive applications. Thus, referring now to FIGS. 11 and 12, embodiments of the disclosure may be used in the context of an exemplary aircraft manufacturing and service method 60 as shown in FIG. 11 and an aircraft 62 as shown in FIG. 12. Aircraft applications of the disclosed embodiments may include, for example, without limitation, composite stiffened members such as fuselage skins, wing skins, control surfaces, hatches, floor panels, door panels, access panels and empennages, to name a few. During pre-production, exemplary aircraft manufacturing and service method 60 may include specification and design 64 of the aircraft 62 and material procurement 66, in which the disclosed method may be specified for use in fabricating components. During production, component and subassembly manufacturing 68 and system integration 70 of the aircraft takes place. The disclosed device and method may be used to fabricate components that are then assembled and integrated with other subassemblies. Thereafter, the aircraft 62 may go through certification and delivery 72 in order to be placed in service 74. While in service by a customer, the aircraft 62 is scheduled for routine maintenance and service 76 (which may also include modification, reconfiguration, refurbishment, and so on). The components fabricated by the disclosed method and device may be used to replace components on the aircraft 62 during the maintenance and service 76.

(34) Each of the processes of exemplary aircraft manufacturing and service method 60 may be performed or carried out by a system integrator, a third party, and/or an operator (e.g., a customer). For the purposes of this description, a system integrator may include without limitation any number of aircraft manufacturers and major-system subcontractors; a third party may include without limitation any number of vendors, subcontractors, and suppliers; and an operator may be an airline, leasing company, military entity, service organization, and so on.

(35) As shown in FIG. 12, the aircraft 62 produced by exemplary aircraft manufacturing and service method 60 may include an airframe 78 with a plurality of high-level systems 80 and an interior 82. Examples of systems of plurality of high-level systems 80 include one or more of a propulsion system 84, an electrical system 86, a hydraulic system 88, and an environmental system 90. Any number of other systems may be included. Although an aerospace example is shown, the principles of the disclosure may be applied to other industries, such as the marine and automotive industries.

(36) Systems and methods embodied herein may be employed during any one or more of the stages of the exemplary aircraft manufacturing and service method 60. For example, components or subassemblies corresponding to production process 68 may be fabricated or manufactured in a manner similar to components or subassemblies produced while the aircraft 62 is in service. Also, one or more apparatus embodiments, method embodiments, or a combination thereof may be utilized during the production stages 68 and 70, for example, by substantially expediting assembly of or reducing the cost of an aircraft 62. Similarly, one or more of apparatus embodiments, method embodiments, or a combination thereof may be utilized while the aircraft 62 is in service, for example and without limitation, to maintenance and service 76.

(37) Although the embodiments of this disclosure have been described with respect to certain exemplary embodiments, it is to be understood that the specific embodiments are for purposes of illustration and not limitation, as other variations will occur to those of skill in the art.