DEVICES TO SUPPORT A VARIETY OF DIFFERENT COMPOSITE STRINGERS

Description

BACKGROUND

[0001] Aircraft utilize various components, such as stringers, to resist bending, torsional, shear, and direct loads. Stringers are typically formed from a lightweight composite using, e.g., a tape or fabric with fibers embedded in a resin matrix. For example, a composite layup is processed in a forming tool to define the shape. The shaped component is then transferred to a curing device for curing. Up until the curing is completed, the stringer requires sufficient support to retain its shape. This shape is often defined by in-plane and / or out-of-plane bends in addition to cross-sectional profiles that vary from one stringer to another. Furthermore, the shaped stringer may subjected to various operations, prior to the curing, such as trimming, inspection, installation of additional components, and the like. This support to the uncured stringer is typically provided by either the forming tool or the curing tool, which limits the throughput by either one of these tools and slows down the overall processing speed.

[0002] What is needed are new methods and devices for supporting of variety of different composite stringers after forming and prior to curing.

[0003] Document US 2017 / 348919 A1, according to its abstract, discloses systems and methods for utilizing support tools for forming laminates. One embodiment is a system that includes a pair of dies that hold a multi-layer laminate over a gap, a male die that presses the laminate into the gap causing the laminate to change shape, and a support tool inserted into the gap beneath the laminate. The support tool includes a base that extends in a lengthwise direction, struts fixedly attached to the base that project upward from the base and are distributed along the lengthwise direction, and a cap that is slidably attached to the struts, and that covers the struts to form an upper surface of the support tool. Each of the struts rises from the base to the cap.

[0004] Document EP 3115185 A1, according to its abstract, discloses a flexible punch and die to form a flat composite laminate charge into a stiffener having a desired cross sectional shape. A desired contour is formed in the stiffener by bending the punch and die.SUMMARY

[0005] The present disclosure provides a post-forming processing device for supporting pre-cured composite stringers prior to curing having the features disclosed at claim 1. The dependent claims outline advantageous forms of embodiment of the device.

[0006] Furthermore, the present disclosure describes another post-forming processing device for supporting pre-cured composite stringers prior to curing having the features disclosed at claim 8. The dependent claims outline advantageous forms of embodiment of the device.BRIEF DESCRIPTION OF THE DRAWINGS

[0007] FIG. 1A a process flowchart of fabricating a composite stringer. FIG. 1B is a process flowchart of fabricating a composite stringer, in accordance with other examples of the present disclosure. FIGS. 1C, 1D, and 1E are different examples of composite stringers. FIG. 2A is a schematic cross-sectional view of a post-forming processing device, comprising a flexible support structure, in accordance with some examples of the present disclosure. FIG. 2B is a schematic cross-sectional view of the post-forming processing device in FIG. 2A, showing the flexible support structure conforming to the hat portion of a - composite stringer prior to curing, in accordance with some examples of the present disclosure. FIG. 2C is a schematic cross-sectional view of the post-forming processing device in FIGS. 2A and 2B, showing the cover sealed against the base and enclosing the - composite stringer prior to curing, in accordance with some examples of the present disclosure. FIG. 2D is a schematic cross-sectional view of a post-forming processing device, comprising a flexible support structure and a flexible insert, both positioned in a channel, in accordance with some examples of the present disclosure. FIG. 2E is a schematic cross-sectional view of a post-forming processing device, illustrating a tapered channel, in accordance with some examples of the present disclosure. FIG. 2F is schematic top view of a post-forming processing device, illustrating bladder seals, in accordance with some examples of the present disclosure. FIG. 3A is a schematic cross-sectional view of a post-forming processing device, comprising a pre-formed support structure. FIG. 3B is a schematic cross-sectional view of the post-forming processing device in FIG. 3A, showing the flexible support structure engaging a - composite stringer prior to curing, in accordance with some examples of the present disclosure. FIG. 3C is a schematic cross-sectional view of the post-forming processing device in FIGS. 3A and 3B, showing the cover sealed against the base and enclosing the - composite stringer prior to curing, in accordance with some examples of the present disclosure. FIG. 4 is a process flowchart corresponding to a method of fabricating a composite stringer. FIG. 5A is a schematic illustration of a laminated layup, disposed on a processing surface of a forming base and extending over a cavity, in accordance with some examples of the present disclosure. FIG. 5B is a schematic illustration of the laminated layup, shaped into a composite stringer prior to curing, by the forming device, in accordance with some examples of the present disclosure. FIG. 5C is a schematic illustration of the - composite stringer, supported by a post-forming processing device, in accordance with some examples of the present disclosure. FIG. 5D is a schematic illustration of a bladder, installed into the - composite stringer prior to curing, while the - composite stringer prior to curing is supported by the post-forming processing device, in accordance with some examples of the present disclosure. FIG. 5E is a schematic illustration of a noodle installed, at an interface between the bladder and the - composite stringer prior to curing, while the - composite stringer prior to curing is supported by the post-forming processing device, in accordance with some examples of the present disclosure. FIG. 5F is a schematic illustration of a cover sealed against the base of the post-forming processing device, in accordance with some examples of the present disclosure. FIG. 5H is a schematic illustration of the - composite stringer transferred together with the bladder and the noodle to a curing device, in accordance with some examples of the present disclosure. FIG. 5I is a schematic illustration of a composite stringer being removed from the curing device, in accordance with some examples of the present disclosure. FIG. 5J is a schematic illustration of an additional - composite stringer prior to curing, supported by a post-forming processing device, in accordance with some examples of the present disclosure. FIGS. 6A and 6B are top schematic views of a post-forming processing device, showing in-plane bending, in accordance with some examples of the present disclosure. FIG. 7 is a process flowchart corresponding to a method of supporting a - composite stringer prior to curing in a post-forming processing device. FIG. 8 is a process flowchart corresponding to a method for manufacturing and service the aircraft. FIG. 9 illustrates a block diagram of an example of an aircraft, in accordance with some examples of the present disclosure. DETAILED DESCRIPTION

[0008] In the following description, numerous specific details are set forth in order to provide a thorough understanding of the presented concepts. In some examples, the presented concepts are practiced without some or all of these specific details. In other instances, well known process operations have not been described in detail so as to not unnecessarily obscure the described concepts. While some concepts will be described in conjunction with the specific examples, it will be understood that these examples are not intended to be limiting.Introduction

[0009] Composite stringers and other shaped composite structures are used for many applications, such as aircraft, land vehicles, and the like. Fabrication of these composite structures involves various handling and processing of - shaped components, such as trimming, inspection, bladder installations, and such. Prior to curing, these shaped components require sufficient support to retain the shape, which can be challenging due to differences in shapes and sizes of these - components. For example, a modern aircraft uses hundreds of different composite stringers, which have different sizes, cross-sectional shapes, in-plane bends, and / or out-of-plane bends. Providing a dedicated support for each type of these composite stringers is challenging and expensive, adding to an already large number of specialized tools used in fabrication of composite stringers.

[0010] FIGS. 1A and 1B illustrate two process flowcharts representing different examples of fabrication a composite stringer and corresponding tools used for various operations. FIGS. 1A and 1B are presented to provide some context and general overview of key components, tools, and steps. In both examples, the process starts with forming device 510 shaping composite layup 502, thereby forming - composite stringer 190. Curing device 540 then cures - composite stringer 190, thereby forming composite stringer 198. - composite stringer 190 prior to curing and composite stringer 198 have the generally same shape, but different material and mechanical properties. For example, the resin of - composite stringer 190 prior to curing is not fully crosslinked or not as cross-inked as the resin of composite stringer 198. As such, composite stringer 190 prior to curing is still able to change the shape and requires support before curing.

[0011] Both forming device 510 and curing device 540 are specifically shaped to accommodate a particular design of composite stringer 198. Therefore, either one or both of forming device 510 and curing device 540 can be used for supporting - composite stringer 190 prior to curing after completing the forming operation and before initiating the curing operation, which corresponds to the example shown in FIG. 1A. However, this approach occupies one or both forming device 510 and curing device 540 for operations that are not core functions of these devices. Furthermore, many of these operations and even storage of - composite stringer 190 prior to curing may take significant periods of time. As a result, the throughput of one or both forming device 510 and curing device 540 can be limited by these intermediate operations and storage associated with - composite stringer 190 prior to curing.

[0012] Referring to FIG. 1B, post-forming processing device 100 is used to receive - composite stringer 190 prior to curing after - composite stringer 190 prior to curing is formed / shaped. Post-forming processing device 100 is also used to support - composite stringer 190 prior to curing up until the curing operation. Post-forming processing device 100 effectively relieves forming device 510 and curing device 540, increasing their processing throughputs. Post-forming processing device 100 is used for various operations, performed on - composite stringer 190 prior to curing, and, in some examples, for storing - composite stringer 190 prior to curing.

[0013] However, if a post-forming processing device is specifically and permanently shaped for accommodating the shape of each specific composite stringer, then the numbers of such post-forming processing devices would be the same as the number of different stringers. This approach is not desirable from a space and cost savings perspective and can complicate the overall process by requiring a large number of additional tools. Furthermore, post-forming processing devices, which are specifically and permanently shaped, may not be always stackable due to the design variations, which complicates their storage. It should also be noted that the supply base is limited based on complexity of the post-forming processing device. Also, 3-D geometry increases complexity for shuttling the stringers around. Finally, 3-D geometry likely increases weight which will inhibit manual handling for a variety of reasons including maintenance.

[0014] Design variations of composite stringers or, more specifically, different examples of composite stringer 190 prior to curing are shown in FIGS. 1C, 1D, and 1E. In each example, composite stringer 190 comprises flange portions 196, which define contact surface 197. Contact surface 197 is used for connecting the composite stringer, formed from - composite stringer 190 prior to curing, to other components, e.g., a composite skin of an aircraft. These other components define the shape of contact surface 197. In some examples, contact surface 197 is planar. Alternatively, contact surface 197 and, more generally, the entire stringer has an out-of-plane bend.

[0015] Each of - composite stringers 190 prior to curing also comprises hat portion 191, which interconnects and is positioned between flange portions 196. Hat portion 191 extends away from contact surface 197, defining stringer cavity 192. Hat portion 191 is defined by the height (H) of hat portion 191, which is defined as a maximum deviation from contact surface 197. Hat portion 191 is also defined by the width (W) of hat portion 191, which is defined as the gap between flange portions 196.

[0016] Referring to FIG. 1C, in some examples, hat portion 191 is formed by straight walls. Alternatively, in some examples, hat portion 191 is formed by a continuous curved wall, e.g., as shown in FIG. 1E. FIG. 1D illustrates an example where hat portion 191 is formed by a combination of straight and curved walls. FIGS. 1C, 1D, and 1E illustrate that - composite stringers 190, shown in these figures, require different types of support from post-forming processing device 100. Furthermore, FIGS. 1C, 1D, and 1E illustrate that - composite stringers 190 are not stackable. Therefore, if permanently-rigid supports are used for these - composite stringers, these supports will not be stackable either. For purposes of differentiating composite stringers, an example shown in FIG. 1E may be referred to as additional - composite stringers 199. Processing different types of - composite stringers prior to curing using the same post-forming processing device 100 is described below with reference to FIG. 4.

[0017] Described methods and devices are used for supporting of variety of different composite stringers, such as ones shown in FIGS. 1A-1C. More specifically, the same post-forming processing device is configured to support - composite stringers prior to curing with different cross-sectional profiles of their hat portions. Specifically, a post-forming processing device comprises a channel and a support structure, at least partially extending within the channel. The support structure is configured to conform to each of differently shaped hat portions the - composite stringers prior to curing and to retain the shape of these hat portions while providing the support. In some example, the support structure is made from a flexible material that conforms to any shape of the hat portions.

[0018] Within examples of the present disclosure, the disclosed post-forming processing device is used for supporting different - composite stringers prior to curing while various operations are performed on these stringers, such as stringer trimming, inspection, installation of bladders and noodles, and the like. Furthermore, in some examples, the disclosed post-forming processing device is used for storing - composite stringers prior to curing. Overall, adding the disclosed post-forming processing device into the overall process flow allows increasing processing throughputs of other devices, such as forming devices and curing devices. Overall, the disclosed post-forming processing devices provide high rate automation of stringer installation by merging the gap between forming and curing devices with these post-forming processing devices.

[0019] The described methods also incorporate alignment fittings to ensure the proper alignment between the stringer and the bladder for dead end fittings. Offset of the bladder helps to provide proper support and functionality during cure. For example, in some instances, a bladder is terminated inside of the edge of the part. Specific examples include door structures, window structures, and convergence structures (e.g., aircraft structures with pointy ends).

[0020] It should be noted that the cavity is used for forming stringer, accommodate both a stringer and a bladder. If the bladder does not extend past the stringer, the bladder will either interfere or leave an unacceptably large gap inside the tool. Since the bladder is aligned and locked to the stringer at the kitting stage, it is beneficial for that the bladder be indexed in the correct position to avoid rework at later stages.

[0021] Additionally, some bladders receive one or more layers of material wrapped around these bladders prior to insertion to corresponding stringers. In some examples, this assembly includes a glass ply, aligned to the end of the stringers to add the corrosion protection inside the stringer. In other examples, this assembly includes a carbon wrap, which adds strength to the stringer. In these later examples, the bladder wrap is aligned with the stringer.Examples of Post-Forming Processing Device

[0022] FIG. 2A is a schematic cross-sectional view of post-forming processing device 100 for supporting - composite stringers 190, in accordance with some examples. Post-forming processing device 100 comprises base 110, support structure 120, and cover 130.

[0023] Base 110 is formed from a rigid material, such as carbon fiber, aluminum, a pultruded polyester / glass solution, and the like. Base 110 comprises support surface 114, which faces cover 130, when cover 130 is present. Support surface 114 is configured to seal against cover 130 and, in some examples, comprises one or more sealing features. During the operation of post-forming processing device 100, support surface 114 is used to support flange portions 196 of stringer 190, e.g., by compressing flange portions 196 between support surface 114 and cover. In some examples, support surface 114 is planar. In general, support surface 114 conforms to the shape of flange portions 196 of stringer 190.

[0024] Base 110 also comprises channel 112, partially extending through base 110 and having opening 113. Opening 113 separates two portions of support surface 114. As shown in FIG. 2A, channel 112 has a channel width (CW) and a channel height (CH). The channel width (CW) is measured in the direction parallel to support surface 114 (along the Y axis). The channel height (CH) is measured in the direction perpendicular to support surface 114 (along the Z axis). In some examples, the channel width (CW) is constant along the length (the X axis (see, e.g., Figure 2F)) of base 110. In the same or other examples, the channel height (CH) is constant along the length (the X axis) of base 110. In some examples, the channel width (CW) is constant along the channel height (the Z axis) as, for example, shown in FIG. 2A. This type of channel 112 may be referred to as a straight channel. Alternatively, the channel width (CW) differs along the channel height (the Z axis) as, for example, shown in FIG. 2E. In this example, the channel width (CW) is the greatest at opening 113. This type of channel 112 may be referred to as a tapered channel and allows for stacking post-forming processing device 100.

[0025] Channel 112 is used to accommodate hat portion 191 of - composite stringer 190 prior to curing when - composite stringer 190 prior to curing is supported using post-forming processing device 100. Referring to FIG. 2B, hat portion 191 protrudes into channel 112, while flange portions 196 rest on support surface 114. It should be noted that the same post-forming processing device 100 is used for supporting different types of composite stringers 190 prior to curing, which may have different shapes and sizes of hat portions 191. As such, the channel width (CW) is larger than the width of hat portions 191 of - composite stringers 190 or, more specifically, larger than the width of the widest hat portion 191 among all - composite stringers 190 prior to curing, processed on post-forming processing device 100. For purposes of this disclosure, the width of hat portion 191 is defined as the largest width, e.g., when hat portion 191 has a tapered or curved cross-section. Furthermore, the channel height is larger than the height of hat portion 191 of composite stringers 190 prior to curing or, more specifically, larger than the height of the tallest hat portion 191 among all - composite stringers 190 prior to curing, processed on post-forming processing device 100. In general, the cross-sectional profile of channel 112 is sufficient to accommodate any hat portion 191 of stringer 190, processed using post-forming processing device 100.

[0026] While FIGS. 2A-2C illustrate a rectangular cross-sectional profile of channel 112, any cross-sectional profile capable of accommodating hat portions 191 of - composite stringers 190 prior to curing is within the scope of the present disclosure, such as tapered profile shown in FIG. 2E, semi-circular profile, and the like. In some examples, the cross-sectional profile of channel 112 corresponds to the cross-sectional profile of hat portions 191, e.g., both are tapered.

[0027] Referring to FIG. 2A, support structure 120 at least partially extends within channel 112 and along the length of channel 112. In some examples, support structure 120 is configured to conform to each hat portion 191 and to retain the cross-sectional shape of that hat portion 191 when - composite stringers 190 prior to curing is supported by and processed using post-forming processing device 100. It should be noted that the same support structure 120 is used for different types and profiles of hat portion 191. Support structure 120 is able to conform to these different types and profiles while providing sufficient support.

[0028] In some examples, support structure 120 is formed from an elastic material, configured to change the shape when conforming to different types of hat portions 191. Some examples of suitable elastic materials include, but are not limited to, latex, silicone (e.g., peroxide or platinum cured silicon), and other like materials. Some considerations for material selection includes weight, clean-ability, solvent resistance, stiffness, tear strength, elongation to failure, and hardness.

[0029] In accordance with independent claim 8, support structure 120 is attached to base 110 at side walls of channel 112 as, e.g., is schematically shown in FIG. 2A. In these examples, support surface 114 remains exposed and available for interfacing with flange portions 196 of - composite stringers 190. In other words, support structure 120 does not interfere when flange portions 196 are positioned on support surface 114, e.g., compressed between support surface 114 and cover 130. These examples are schematically shown in FIGS. 2A and 2B.

[0030] In accordance with independent claim 1, support structure 120 comprises a plastically deformable material. More specifically, support structure 120 is co-formed or co-shaped with one of composite stringers 190 prior to curing and then retains the shape of this stringer while supporting this stringer. For example, the shape of support structure 120 is initially different than that of - composite stringer 190 prior to curing. It should be noted that at this stage - composite stringer 190 is not yet formed. Both support structure 120 and a composite layup are loaded into a forming device, various examples of which are described below, and the shape of support structure 120 is adjusted, while - composite stringer 190 prior to curing is being formed. Hence, support structure 120 is co-formed or co-shaped with - composite stringer 190 prior to curing.

[0031] This shape is retained by support structure 120 during various operation of post-forming processing device 100 while supporting this particular stringer. In some examples, the shape is retained while processing multiple stringers of the same type, e.g., the same cross-sectional shape of hat portions. When a different type of stringer is to be supported, the shape of support structure 120 is changed, e.g., by co-forming or shaping with that other stringer. These examples are schematically shown in FIGS. 3A and 3B.

[0032] Referring to FIG. 3A, in some examples, support structure 120 comprises support flanges 124 extending over support surface 114 of base 110 and outside channel 112. Similar to a portion of support structure 120, extending into channel 112 and supporting hat portions 191 of stringer 190, support flanges 124 are specifically shaped to support flange portions 196 of stringer 190. In some examples, the shape of support flanges 124 is different from the shape of support surface 114. Therefore, the same post-forming processing device 100 may be used for supporting stringers with different shapes of flange portions.

[0033] In some examples, support structure 120 is removable from base 110. For example, support structure 120 is removed from base 110 to change the shape of support structure 120. In some examples, different types of support structure 120 are used with the same base 110.

[0034] Cover 130 is configured to attach to base 110, such that the corresponding one of composite stringers 190 prior to curing is positioned between cover 130 and base 110 while supported by post-forming processing device 100. More specifically, flange portions 196 of composite stringer 190 prior to curing are positioned and, in some examples, are compressed between cover 130 and support surface 114 as, for example, is schematically shown in FIG. 3C. Cover 130 is configured to seal against base 110. Specifically, cover 130 comprises vacuum seal 132, which engages seal receiver 115.

[0035] In some examples, base 110 comprises pass-through 116, fluidically coupled with channel 112 and configured to control pressure inside channel 112 and under support structure 120. For example, pass-through 116 is used to maintain the pressure under support structure 120 to be the same as in the environment, e.g., when hat portion 191 of composite stringer 190 prior to curing is inserted into channel 112 and engages support structure 120 or, more specifically, when hat portion 191 pushes support structure 120 deeper into channel 112 thereby reducing the volume under support structure 120.

[0036] In some examples, post-forming processing device 100 further comprises flexible insert 140 as, e.g., shown in FIG. 2D. Flexible insert 140 is positioned with channel 112 and under support structure 120 and is used to provide additional support to hat portion 191. Flexible insert 140 allows using support structure 120 that are very flexible and able to conform to a larger variation of hat portion 191 than, for example, when support structure 120 is used without flexible insert 140. In some examples, flexible insert 140 is made from an elastomeric rubber, such as MOSITES ®< rubber, latex, or something similar.

[0037] Referring to FIG. 2F, in some examples, post-forming processing device 100 comprises pass-through bladder seal 180 and dead end bladder seal 182. It should be noted that bladder 520, which is further described below with reference to FIGS. 5D-E, is a tube made, e.g., from silicone, VITON ®< , or other like materials. In some examples, the material of bladder 520 is reinforced or layered. During processing, bladder 520 is vented to the autoclave atmosphere during cure and vented to the ambient atmosphere during any compaction / vacuum bag. As such, in some examples, one end of bladder 520 comprises a fitting with a vent hole. Pass-through bladder seal 180, shown in FIG. 2F, connects this fitting allowing bladder 520 to vent, when bladder 520 is inside post-forming processing device 100. In some examples, post-forming processing device 100 comprises pass-through bladder seals on both ends.Examples of Methods of Fabricating Composite Stringer

[0038] FIG. 4 is a process flowchart corresponding to a non-claimed method 400 of fabricating composite stringer 198, see, e.g., FIG. 1B, in accordance with some examples. Composite stringer 198 should be differentiated from - composite stringer 190 prior to curing, which is an intermediate structure used to form composite stringer 198. As such, in some examples, - composite stringer 190 and composite stringer 198 have the same size and shape. Therefore, FIGS. 1C-1E are representative of both - composite stringer 190 prior to curing and composite stringer 198. In some examples, composite stringer 198 comprises a fiber reinforced composite material, which may be also referred to as a reinforced composite material. This type of material comprises one or more non-homogeneous polymer-based components and one or more non-polymeric based components (e.g., carbon-fibers). Method 400 is described in greater detail below with reference to FIG. 4 and FIGS. 5A-H.

[0039] Method 400 comprises forming (block 410) - composite stringer 190 prior to curing, e.g., using composite layup 502. This operation is performed using forming device 510 (shown in FIGS. 5A and 5B), which is different from post-forming processing device 100, used in later operation (shown in FIGS. 5C - 5F). As noted above, post-forming processing device 100 increases throughput of forming device 510 since various later operations are performed using post-forming processing device 100.

[0040] In some examples, composite layup 502 comprises an uncured pre-impregnated reinforcing tape or fabric, which may be referred to as a prepreg. The tape or fabric comprises fibers, such as graphite fibers, embedded within a matrix material, such as a polymer or, more specifically, an epoxy or phenolic resin. In some examples, the tape or fabric is unidirectional or woven depending on the design and the degree of reinforcement desired in the resulting composite stringer 198.

[0041] During the forming operation (block 410), composite layup 502 is positioned on forming device 510 as, e.g., is shown in FIG. 5A. In some examples, support structure 120 is positioned between composite layup 502 and forming device 510, e.g., when support structure 120 is co-formed together with - composite stringer 190 prior to curing. These examples are further described below with reference to block 412. Forming device 510 comprises forming base 511 with forming cavity 512, which defines the shape of hat portion 191 of - composite stringer prior to curing. Referring to FIG. 5B, forming device 510 also comprises forming die 513, which pushes a part of composite layup 502 into forming cavity 512 and against the walls of forming cavity 512.

[0042] Upon completion of this operation, composite layup 502 is formed into - composite stringer 190. - composite stringer 190 prior to curing comprises hat portion 191, which is disposed between forming die 513 and the walls of forming cavity 512. - composite stringer 190 prior to curing also comprises flange portions 196, which extend outside of forming cavity 512 and, e.g., conform to forming surface 514 of forming base 511. In some examples, forming die 513 comprises specially configured bladders, pressing on flange portions 196. These bladders are pressurized and contact flange portions 196 prior to forming hat portion 191, in some examples to different pressure level to allow composite layup 502 to slip on forming surface 514 while hat portion 191 is being formed.

[0043] In some examples, forming - composite stringer 190 prior to curing on forming device comprises forming (block 412) support structure 120 of post-forming processing device 100. In some examples, support structure 120 is shaped in a separate operation from - composite stringer 190 prior to curing. Alternatively, support structure 120 and composite stringer 190 prior to curing are co-formed or co-shaped in the same overall operation, e.g., the operation represented by block 412 is a part of the operation represented by block 410, as shown in FIG. 4. In other words, support structure 120 is placed into forming device 510 together with composite layup 502. At this stage, the shape of support structure 120 is different than the shape of - composite stringer 190 prior to curing, which will be formed on and defined by forming device 510. For example, support structure 120 has been previously used for supporting another - composite stringer prior to curing, which has a different shape. During concurrent operations represented by block 410 and block 412, - composite stringer 190 prior to curing is formed while support structure 120 is also co-formed or co-shaped. This support structure forming operation (block 412) may be also referred to as a shape changing operation.

[0044] In some examples, method 400 also comprises trimming of - composite stringer 190 prior to curing, e.g., cutting a portion of - composite stringer 190 prior to curing. For example, an ultrasonic knife is used for cutting.

[0045] Method 400 proceeds with transferring (block 420) - composite stringer 190 prior to curing from forming device 510 to post-forming processing device 100. For instance, the transfer of - composite stringer 190 prior to curing from forming device 510 to post-forming processing device 100 is shown in Figures 5B-5C. Various examples of post-forming processing device 100 are described above. In some examples, - composite stringer 190 prior to curing is transferred unsupported. Alternatively, - composite stringer 190 prior to curing is transferred together with support structure 120.

[0046] In some examples, the transferring operation comprises controlling pressure inside channel 112 of base 110. For example, inserting hat portion 191 of - composite stringer 190 prior to curing into channel 112 may cause displacing of air from channel 112, e.g., through pass-through 116.

[0047] In some examples, the transferring operation comprises stretching (block 422) support structure 120 of post-forming processing device 100. In these examples, support structure 120 is formed from an elastic material that conforms to the shape of hat portion 191 of - composite stringer 190 prior to curing as hat portion is inserted into channel 112. More specifically, the elastic material is configured to change the shape when conforming to each of hat portions 191. As noted above, in some examples, hat portions 191 have different cross-sectional shapes. This stretching feature as, e.g., is shown in FIGS. 2A - 2B, of support structure 120 allows supporting - composite stringers 190 with different sizes of hat portions 191.

[0048] In some examples, the transferring operation comprises adjusting (block 424) the shape of post-forming processing device 100. FIGS. 6A and 6B illustrate base 110 of post-forming processing device 100, which has a pivot point, defined by first axis 601. Other components of post-forming processing device 100, such as support structure 120, are not shown for simplicity. The pivot point allows base 110 to have an in-plane bending and accommodate both straight - composite stringers prior to curing (in the configuration shown in FIG. 6A) and - composite stringers prior to curing with an in-plane bend (in the configurations shown in FIG. 6B). While only one pivot point is shown in FIGS. 6A and 6B, one having ordinary skill in the art would understand that any number of pivot points may be present. Furthermore, in some examples, post-forming processing device 100 has an out-of-plane bending functionality. It should be noted that some degrees of bending, especially localized bending, of - composite stringers prior to curing can be accommodated by the side of channel 112 within base 110, without bending base 110.

[0049] In some examples, method 400 comprises inspecting (block 430) - composite stringer 190 prior to curing. The inspection is performed while - composite stringer 190 prior to curing is positioned on post-forming processing device 100. For example, the inspection involves checking the surface of - composite stringer 190 prior to curing for wrinkles, bubbles, foreign object debris (FOD), loose fibers, wrinkles, and shape. It should be noted that the inspection operation is performed away from forming device 510 and curing device 540, thereby allowing other - composite stringers prior to curing to be processes on these devices and increasing the overall process throughput.

[0050] Method 400 comprises installing (block 440) bladder 520 on - composite stringer 190 prior to curing as, e.g., schematically shown in FIG. 5D. Bladder 520 is installed while composite stringer 190 is positioned on post-forming processing device 100. In some example, bladder 520 is wrapped into a bladder warp, which is later cured into the skin of the stringer when bladder 520 is removed. Bladder 520 is used during curing operation to provide support inside of - composite stringer 190 prior to curing. In some examples, bladder 520 is a solid object composed of silicone, urethane, or similar materials, including any combination thereof. In some examples, bladder 520 is shaped to substantially correspond with - composite stringer 190 prior to curing.

[0051] Method 400 comprises installing (block 450) noodle 530 at an interface between bladder 520 and - composite stringer 190 and within the plane of support surface 114 of base 110 as, e.g., schematically shown in FIG. 5E. This installing operation is performed while - composite stringer 190 prior to curing is positioned on post-forming processing device 100. Noodle 530 is also referred to as a radius filler.

[0052] In some examples, method 400 comprises compacting (block 460) - composite stringer 190 prior to curing, while - composite stringer 190 prior to curing is positioned on post-forming processing device 100. For example, the compacting operation involves sealing cover 130 of post-forming processing device 100 against base 110 of post-forming processing device 100 as, for example, is schematically shown in FIG. 5F. In some examples, the compacting operation further comprises contacting at least flange portions 196 of composite stringer 190 prior to curing with cover 130 of post-forming processing device 100.

[0053] In some examples, method 400 comprises staging and transporting - composite stringer 190 prior to curing. These operations are performed while - composite stringer 190 is positioned on post-forming processing device 100. Furthermore, post-forming processing device 100 is used for storing - composite stringer 190 prior to curing, while providing support to - composite stringer 190.

[0054] Method 400 proceeds with transferring (block 490) - composite stringer 190 prior to curing from post-forming processing device 100 to curing device 540. For instance, the transfer of - composite stringer 190 prior to curing from post-forming processing device 100 to curing device 540 is shown in FIG. 5F - 5H. In some examples, - composite stringer 190 prior to curing is transferred together with bladder 520 and / or noodle 530, which are installed onto - composite stringer 190 prior to curing while - composite stringer 190 prior to curing was positioned on post-forming processing device 100.

[0055] Method 400 comprises curing (block 492) - composite stringer 190 prior to curing on curing device 540, thereby forming composite stringer 198 as, for example, is schematically shown in FIGS. 5H and 5I. For example, - composite stringer 190 prior to curing, shown in FIG. 5H, is subjected to heat and pressure to cross-link the resin within composite stringer 190 prior to curing. Unlike - composite stringer 190 prior to curing, composite stringer 198, shown in FIG. 5I, does not require the level of support needed for composite stringer 190 prior to curing. As such, post-forming processing device 100 is not used for composite stringer 198.

[0056] In some examples, various operations of method 400 are repeated (decision block 494) with additional - composite stringer 199 prior to curing, e.g., one example of which is shown in FIG. 1E. Specifically, additional - composite stringer 199 prior to curing has a different design than - composite stringer 190 prior to curing, previously processed using the same post-forming processing device 100. Various different designs for - composite stringers prior to curing are shown in FIGS. 1C-1E. Other example designs for the composite stringer prior to curing are possible as well.

[0057] Specifically, method 400 comprises forming 410 an additional - composite stringer 199 prior to curing on an additional forming device. Unlike post-forming processing device 100, which can be universally used across a variety of different designs of - composite stringers prior to curing, forming devices are dedicated tools. In some examples, support structure 120 is reformed or reshaped during this operation of forming additional composite stringer 199 prior to curing. More specifically, support structure 120 has a different shape when supporting additional - composite stringer 199 prior to curing than when supporting - composite stringer 190 prior to curing.

[0058] Method 400 proceeds with transferring (block 420) this additional - composite stringer 199 prior to curing from the forming device to post-forming processing device 100. As noted above, additional - composite stringer 199 prior to curing has a different design and, more specifically, a different cross-sectional profile than - composite stringer 190 prior to curing.

[0059] In some examples, method 400 continues with installing an additional bladder on additional - composite stringer 199, while additional - composite stringer 199 prior to curing is positioned on post-forming processing device 100. Furthermore, a noodle is installed on additional - composite stringer 199 prior to curing, while additional - composite stringer 199 prior to curing is positioned on post-forming processing device 100. However, these operations are optional.

[0060] Method 400 proceeds with transferring additional - composite stringer 199 prior to curing together with additional bladder and additional noodle from post-forming processing device 100 to an additional curing device and curing - composite stringer 190 prior to curing using additional curing device, thereby forming an additional composite stringer.

[0061] FIG. 7 is a process flowchart of a non-claimed method 700 of supporting composite stringer prior to curing 190 using post-forming processing device 100, in accordance with some examples of the present disclosure. Method 700 comprises transferring (block 720) - composite stringer 190 prior to curing to post-forming processing device 100 as, for example, is schematically shown in FIG. 5C. Various examples of composite stringer 190 prior to curing are described above. For example, - composite stringer 190 prior to curing comprises comprising hat portion 191, which is supported upon the transfer of - composite stringer 190 to post-forming processing device 100. Post-forming processing device 100 comprises base 110, comprising channel 112. Post-forming processing device 100 also comprises support structure 120, at least partially extending within channel 112 and along the length of channel 112.

[0062] When - composite stringer 190 prior to curing is transferred to post-forming processing device 100, support structure 120 conforming to hat portion 191 of - composite stringer 190 prior to curing, as for, example, is schematically shown in FIG. 5C. More specifically, support structure 120 retains the cross-sectional shape of hat portion 191 of composite stringer 190 prior to curing while - composite stringer 190 prior to curing is positioned in post-forming processing device 100. In some examples, support structure 120 is formed from a flexible material, providing this conformal supports.

[0063] In some examples, the transferring operation (block 720) comprises stretching (block 722) support structure 120 of post-forming processing device 100 as, for example, is schematically shown in FIGS. 2A-2B . In these examples, support structure 120 is formed from an elastic material that conforms to the shape of hat portion 191 of - composite stringer 190 prior to curing as hat portion is inserted into channel 112. This stretching feature of support structure 120 allows supporting - composite stringers 190 prior to curing with different sizes of hat portions 191.

[0064] In some examples, the transferring operation (block 720) comprises adjusting (block 724) the shape of post-forming processing device 100. FIGS. 6A and 6B illustrate base 110 of post-forming processing device 100, which has a pivot point, defined by first axis 601. Other components of post-forming processing device 100, such as support structure 120, are not shown for simplicity. The pivot point allows base 110 to have an in-plane bending and accommodate both straight - composite stringers prior to curing (in the configuration shown in FIG. 6A) and - composite stringers prior to curing with an in-plane bend (in the configurations shown in FIG. 6B). While only one pivot point is shown in FIGS. 6A and 6B, one having ordinary skill in the art would understand that any number of pivot points may be present. Furthermore, in some examples, post-forming processing device 100 has an out-of-plane bending functionality. It should be noted that some degrees of bending, especially localized bending, of - composite stringers prior to curing can be accommodated by the side of channel 112 within base 110, without bending base 110.

[0065] In some examples, the transferring operation (block 720) comprises positioning (block 726) cover 130 of post-forming processing device 100 against base 110 of post-forming processing device 100 as, for example, is schematically shown in FIG. 5F. In some examples, cover 130 is sealed against base 110. Furthermore, in some examples, this cover positioning operation (block 726) compacts at least flange portions 196 of - composite stringer 190 prior to curing.

[0066] In some examples, the transferring operation (block 720) comprises controlling (block 728) pressure inside channel 112 of base 110. For example, inserting hat portion 191 of - composite stringer 190 prior to curing into channel 112 may cause displacing of air from channel 112, e.g., through pass-through 116.

[0067] In some examples, method 700 comprises storing (block 730) - composite stringer 190. More specifically, - composite stringer 190 prior to curing is stored in post-forming processing device 100 prior to removing (block 740) - composite stringer 190 prior to curing from post-forming processing device 100.

[0068] Method 700 proceeds with removing (block 740) - composite stringer 190 prior to curing from post-forming processing device 100. For example, - composite stringer 190 prior to curing is transferred to curing device 540 as, for example, is schematically shown in FIG. 5H. Alternatively, - composite stringer 190 prior to curing is transferred to other equipment, e.g., for inspection.

[0069] Method 700 proceeds or, more specifically repeats, (decision block 794) with transferring (block 720) additional - composite stringer 199 prior to curing to post-forming processing device 100 as, for example, is schematically shown in FIG. 5J. Additional composite stringer 199 prior to curing comprising additional hat portion 193, such that cross-sectional shape of additional hat portion 193 of additional - composite stringer 199 prior to curing, different from the cross-sectional shape of hat portion 191 of - composite stringer 190 prior to curing, shown in FIG. 5C. However, despite this difference in the cross-sectional shapes, support structure 120 of post-forming processing device 100 conforms to additional hat portion 193 of additional - composite stringer 199 prior to curing. Furthermore, support structure 120 retains the cross-sectional shape of additional hat portion 193 of additional - composite stringer 199 prior to curing.Aircraft Examples

[0070] In some examples, methods and systems described above are used on aircraft and, more generally, by the aerospace industry. Specifically, these methods and systems can be used during fabrication of aircraft as well as during aircraft service and maintenance.

[0071] Accordingly, the apparatus and methods described above are applicable for aircraft manufacturing and service method 900 as shown in FIG. 8 and for aircraft 902 as shown in FIG. 9. During pre-production, method 900 includes specification and design 904 of aircraft 902 and material procurement 906. During production, component and subassembly manufacturing 908 and system integration 910 of aircraft 902 takes place. Thereafter, aircraft 902 goes through certification and delivery 912 in order to be placed in service 914. While in service by a customer, aircraft 902 is scheduled for routine maintenance and service 916, which also includes modification, reconfiguration, refurbishment, and so on.

[0072] In some examples, each of the processes of method 900 is 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 includes without limitation any number of aircraft manufacturers and major-system subcontractors; a third party includes without limitation any number of venders, subcontractors, and suppliers; and an operator can be an airline, leasing company, military entity, service organization, and so on.

[0073] As shown in FIG. 9, aircraft 902 produced by method 900 includes airframe 918 with plurality of systems 920, and interior 922. Examples of systems 920 include one or more of propulsion system 924, electrical system 926, hydraulic system 928, and environmental system 930. Any number of other systems can be included. Although an aerospace example is shown, the principles of the examples described herein is applied to other industries, such as the automotive industry.

[0074] Apparatus and methods presented herein can be employed during any one or more of the stages of method 900. For example, components or subassemblies corresponding to manufacturing 908 are fabricated or manufactured in a manner similar to components or subassemblies produced while aircraft 902 is in service. Also, one or more apparatus examples, method examples, or a combination thereof is utilized during manufacturing 908 and system integration 910, for example, by substantially expediting assembly of or reducing the cost of an aircraft 902. Similarly, one or more of apparatus examples, method examples, or a combination thereof is utilized while aircraft 902 is in service, for example and without limitation, to maintenance and service 916.

Claims

1. A post-forming processing device (100) for supporting pre-cured composite stringers prior to curing (190), the pre-cured composite stringers prior to curing comprising hat portions (191), having cross-sections, different among the pre-cured composite stringers prior to curing, the post-forming processing device (100) comprising: a base (110), comprising a channel (112), having a channel width and a channel height, wherein: the channel width is larger than a width of the hat portions (191) of the pre-cured composite stringers prior to curing (190), and the channel height is larger than heights of the hat portions (191) of the pre-cured composite stringers prior to curing (190); a support structure (120), at least partially extending within the channel (112) and along a length of the channel (112) and configured to conform to each of the hat portions (191) and to retain a cross-sectional shape of each of the hat portions (191) when a corresponding one of the pre-cured composite stringers prior to curing (190) is supported by the post-forming processing device (100); a cover (130), configured to attach to the base (110), such that the corresponding one of the pre-cured composite stringers prior to curing (190) is positioned between the cover (130) and the base (110) while supported by the post-forming processing device (100); and wherein the support structure (120) comprises a plastically deformable material.

2. The post-forming processing device (100) of claim 1, wherein the support structure (120) is co-formed with the corresponding one of the pre-cured composite stringers prior to curing (190).

3. The post-forming processing device (100) of claim 1, wherein the support structure (120) comprises support flanges (124) extending over a support surface (114) of the base (110) and outside the channel (112).

4. The post-forming processing device (100) of claim 1, wherein the support structure (120) is removable from the base (110).

5. The post-forming processing device (100) of any of claims 1 to 4, wherein the base (110) comprises a pass-through (116), fluidically coupled with the channel (112) and configured to control pressure inside the channel (112).

6. The post-forming processing device (100) of any of claims 1 to 5, further comprising a flexible insert (140), positioned with the channel (112) and under the support structure (120).

7. The post-forming processing device (100) of any of claims 1 to 6, wherein the cover (130) is configured to seal against the base (110).

8. A post-forming processing device (100) for supporting pre-cured composite stringers prior to curing (190), comprising hat portions (191), having cross-sections, different among the pre-cured composite stringers prior to curing, the post-forming processing device (100) comprising: a base (110), comprising a channel (112), having a channel width and a channel height, wherein: the channel width is larger than a width of the hat portions (191) of the pre-cured composite stringers prior to curing (190), and the channel height is larger than heights of the hat portions (191) of the pre-cured composite stringers prior to curing (190); a support structure (120), at least partially extending within the channel (112) and along a length of the channel (112) and configured to conform to each of the hat portions (191) when a corresponding one of the pre-cured composite stringers prior to curing (190) is supported by the post-forming processing device (100); a cover (130), configured to attach to the base (110), such that the corresponding one of the pre-cured composite stringers prior to curing (190) is positioned between the cover (130) and the base (110) while supported by the post-forming processing device (100); and wherein the support structure (120) is formed from an elastic material configured to change shape when conforming to each of the hat portions (191); and wherein the support structure (120) is attached to the base (110) at side walls of the channel (112).

9. The post-forming processing device (100) of claim 8, wherein the support structure (120) is co-formed with the corresponding one of the pre-cured composite stringers prior to curing (190).

10. The post-forming processing device (100) of claim 8, wherein the support structure (120) comprises support flanges (124) extending over a support surface (114) of the base (110) and outside the channel (112).

11. The post-forming processing device (100) of claim 8, wherein the support structure (120) is removable from the base (110).

12. The post-forming processing device (100) of any of claims 8 to 11, wherein the base (110) comprising a pass-through (116), fluidically coupled with the channel (112) and configured to control pressure inside the channel (112).

13. The post-forming processing device (100) of any of claims 8 to 12, further comprising a flexible insert (140), positioned with the channel (112) and under the support structure (120).

14. The post-forming processing device (100) of any of claims 8 to 13, wherein the cover (130) is configured to seal against the base (110).