The present invention relates in general to the application of sealant to fasteners, such as rivets and bolts, and more specifically to the application of sealant to fasteners for use in aerospace manufacture and repair.
In many aerospace applications, particularly aircraft manufacture, fasteners are often used to connect one or more substrates together. Many fasteners, such as rivets, pins, threaded bolts, or other screw-type fasteners, pass through the substrates from an upper exposed surface (the top side) to the back-side of the substrates. Such fasteners can be secured on the backside by several methods including a shop head (buck tail), collar, nut, or nutplate.
In many cases, sealant must be applied to the backside portion of the fastener, for example to prevent leakage or corrosion. Typically, sealant has been applied to directly exposed fasteners using a brush, spatula, or stick applicator. The results of such an application process are shown in
What is needed therefore is an improved process for applying sealant to the backside of fasteners for use in aerospace manufacture and repair.
An object of the invention, therefore, is to provide such an improved process for applying sealant to the backside of fasteners. Preferred embodiments of the present invention use a novel sealant cap as a mold for applying sealant. Embodiments of the present invention are especially suited for applying sealant to the backside of fasteners used in aircraft production. In preferred embodiments, the sealant caps allow the application of a metered amount of sealant only at the required/desired locations around an installed aircraft fastening element. Embodiments of the present invention thus prevent the over/under application of sealant and reduce the amount of time required to seal a fastener. Further, embodiments of the present invention help improve quality inspections by producing a consistent profile with smooth surfaces and well defined features making the identification of flaws much easier.
The foregoing has outlined rather broadly the features and technical advantages of the present invention in order that the detailed description of the invention that follows may be better understood. Additional features and advantages of the invention will be described hereinafter. It should be appreciated by those skilled in the art that the conception and specific embodiments disclosed may be readily utilized as a basis for modifying or designing other structures for carrying out the same purposes of the present invention. It should also be realized by those skilled in the art that such equivalent constructions do not depart from the spirit and scope of the invention as set forth in the appended claims.
This disclosure, in general, relates to sealant caps used as molds for applying sealant over fasteners or fastener elements such as nutplates (collectively referred to herein as fasteners). Sealant caps according to embodiments of the invention can be filled with the desired amount of sealant for a particular fastener application and then placed over the fastener to mold the sealant in place until the sealant has cured. In particular embodiments, after curing is sufficiently complete, the sealant caps can then be removed from the fasteners leaving behind a metered amount of sealant only at the required/desired locations around an installed fastener.
Embodiments of the present invention are especially suited for applying sealant to the backside of fasteners used in aircraft production. Particularly for aerospace applications, it is desirable to apply a precisely metered amount of sealant because the application of too much sealant contributes to excess weight of an aircraft. Embodiments described herein allow a controlled amount of sealant to be added to the sealant cap rather than applying sealant directly to the fastener as in the prior art methods described above. The sealant cap is then used to control exactly where the sealant is applied and to mold the sealant in place. Embodiments of the present invention thus prevent the over/under application of sealant and reduce the amount of time required to seal a fastener. Removal of the sealant caps after the molding and curing processes are complete also reduces the weight of the finished aircraft. Further, embodiments of the present invention help improve quality inspections after fasteners are installed and sealed by producing a consistent profile with smooth surfaces and well-defined features that make the identification of flaws much easier.
Much of the description herein refers to sealant caps used to seal enclosed dome nutplates. However, embodiments of the present invention are equally suited for other simpler sealing applications where a high quality, repeatable, aesthetically pleasing seal is preferred or required. For example, the single-part sealant caps described below are especially suited for fasteners such as Eddie-bolts or other similar fasteners designed for blind applications where the anchor nuts are inaccessible.
Sealant cap 100 is a multi-part sealant cap that includes mold base 102, plunger 108, and a stop tab or blade 110 that is used to adjust the sealant cap for fasteners components of different heights. Mold base 102 serves as the reservoir for the proper amount of uncured sealant for the particular fastener application, and has a central opening for receiving plunger 108. In the embodiment of
Central opening 120 is sized so plunger 108 can slide up or down relative to the mold base. In some embodiments, central opening can have grooves and/or ribs that match with corresponding ribs and/or grooves on the plunger to prevent the plunger from rotating relative to the mold base once it is installed. This helps ensure a tight enough fit that sealant is substantially prevented from escaping between the alignment cylinder and the mold base when the filled sealant cap is installed. In some embodiments, the exterior surface of the plunger can also have longitudinally arranged rows of teeth that mate with one or more interior edges or ratchets in the central opening. This generally holds the plunger in position with respect to the mold base, while still allowing the plunger to slide up or down upon the application of sufficient force. In particular embodiments, the arrangement of teeth and ratchets allows the plunger to be readily moved between an upper position and a lower position, but does not allow the plunger to be pulled up and out of the opening in the mold base, which helps ensure that the entire assembled sealant cap (plunger with stop blade and the mold base) will be completely removed once sealant curing is complete.
When installed into the mold base, plunger 108 is used to properly align the sealant cap with a fastener and to prevent sealant from being applied to portions of the fasteners. This serves to reduce material costs and reduce the overall weight of an aircraft. Plunger 108 has an upper portion that engages with the mold base and a lower portion that is generally cylindrical (to match the shape of the fastener portion or nutplate) with an internal cavity that will slide down over a portion of the fastener during installation. Stop blades 110 (as described below) can be used to prevent the plunger from sliding too far down the fastener. As shown in
As shown in
In
In
In particular embodiments, the different lock positions for a stop blade will each correspond to a proper plunger placement for a different standard fastener height. For example, with respect to nutplate fasteners, for a given diameter of nutplate, a series of different fastener heights are typically used with each varying from the previous nutplate in the series by 1/16 inches. By setting the distance between the stop blade teeth so that each step reduces fastener height by 1/16 inches, each step will correspond to proper installation of a typical fastener. As will be appreciated by persons of skill in the art, sealant caps according to embodiments described herein could be produced in any desired diameter, shape, or height to match virtually any desired fastener size.
In some embodiments, the interior diameter of internal cavity 118 will be just slightly larger than the fastener on which the sealant cap is being installed. Integral o-rings 117 (or a similar narrowing structure) at the base of interior cavity 118 can have a narrower diameter that is roughly equal to (or even slightly smaller than) the exterior diameter of the fastener. Because plunger 108 can be made from am at least slightly elastic plastic or polymer (as described below) the flexibility of the plunger can be used to insure a snug fit around the base of the plunger. This not only holds the sealant cap in position, but also helps insure than no sealant can squeeze up into the plunger cavity upon installation.
In particular embodiments, once a sealant cap such as the embodiment shown in
“Sealant” as used herein refers to material that can be applied to a seam, gap, or interface between two materials to form a barrier through the physical properties of the sealant itself and by adhesion to one or more substrate materials against penetration by moisture, air flow, and/or other liquids and/or gases. Sealant formulations suitable for practicing some embodiments of the invention will be flowable when in an uncured or partially uncured condition, but which become at least largely solid (non-flowable) as the sealant cures. Embodiments of the invention are not limited to any particular type of sealant or method of curing. In some embodiments, a suitable sealant will be one that is approved for use with aerospace fasteners.
In some embodiments, a suitable sealant will be flowable when uncured or partially uncured, and will also have a high enough viscosity to maintain position and shape when deposited into the mold base reservoir and then inverted during application. Examples of sealants suitable for use with embodiments of the present invention would be sealants that comply with U.S. military specification AMS 3277, such as PR-2001 Fuel Tank Sealant available commercially from PRC-DeSoto, and sealants that comply with U.S. military specification AMS 3281, such as PR 1776 also available from PRC-DeSoto, or AC380 available from 3M.
Filling the mold base reservoir should be done so as to avoid introducing air bubbles in the sealant. In some embodiments, both the positioning/inversion of the sealant cap and the addition of the uncured sealant to the mold base can be performed in an automated fashion using, for example a robotic positioning system and a computer-controlled sealant dispenser that dispenses the uncured sealant through a nozzle or tip. In other embodiments, positioning of the sealant cap and/or application of the sealant can be performed by hand.
Curing times for suitable sealants can vary widely, from minutes to hours after curing is initiated. In some embodiments, the mold can be prefilled with sealant automatically, and subsequently cooled to a temperature at which the sealant cure rate is halted or drastically slowed. This process can be done off-site, allowing the prefilled molds to be delivered ready to thaw and install. The use of pre-mixed frozen sealant is well known in the prior art.
In some embodiments, the sealant can be added until the mold base is completely filled. In automated processes, the amount of sealant to be added to the mold base can be precisely metered using known methods.
Once filled, the sealant cap 100 can re-oriented top side up and installed onto a fastener as shown in
Once the sealant has sufficiently cured, the entire sealant cap, including plunger 108, stop blade 110, and mold base 102 can be removed, leaving behind a sealed fastener.
Cylindrical neck 1220 preferably has a central opening 1224 through which the alignment cylinder 904 is inserted. Central opening 1224 is sized so the alignment cylinder can slide up and down relative to the mold base, but with a tight enough fit that sealant is substantially prevented from escaping between the alignment cylinder and the mold base when the filled sealant cap is installed (as described below).
In the operation of two-part sealant cap 1300 according to an embodiment of the invention, a fastener element such as a nutplate 1306 is first cleaned and prepared, as is known in the prior art. Alignment cylinder 1304 preferably positioned inside the central opening of mold 1302 so that the top of alignment cylinder 1304 is flush with the top cylindrical neck. This results in the bottom of alignment cylinder 1304 extending well beyond the mold base.
In some embodiments, the sealant can be added until the mold base is completely filled. In particular embodiments, the alignment cylinder (which is positioned in the center of the mold base) can have one or more fill lines formed on the surface of the cylinder indicating the appropriate sealant level (as shown in
Filled sealant cap 1100 can then be re-oriented top side up and placed over a fastener element 1106 as shown in
In some embodiments, the mold portion of the sealant cap will be formed from a transparent or translucent material that will allow bubble or voids in the sealant to be observed from the outside when the filled sealant is in position over a fastener. In some embodiments, a portion of the sealant cap, such as the molds shown in
In some embodiments of the present invention, a one-piece sealant cap (without an alignment cylinder) can be used. Such a sealant cap will typically be less expensive, but will result in a layer of sealant over the entire fastener. Such a one-piece sealant cap is shown in
Another embodiment of a one-piece sealant cap is shown in
Once the sealant has cured, the one-piece sealant cap can be removed from the fastener, as shown in
The invention described herein has broad applicability and can provide many benefits as described and shown in the examples above. The embodiments will vary greatly depending upon the specific application, and not every embodiment will provide all of the benefits and meet all of the objectives that are achievable by the invention. Note that not all of the activities described above in the general description or the examples are required, that a portion of a specific activity may not be required, and that one or more further activities may be performed in addition to those described. Still further, the order in which activities are listed are not necessarily the order in which they are performed.
In the foregoing specification, the concepts have been described with reference to specific embodiments. However, one of ordinary skill in the art appreciates that various modifications and changes can be made without departing from the scope of the invention as set forth in the claims below. Accordingly, the specification and figures are to be regarded in an illustrative rather than a restrictive sense, and all such modifications are intended to be included within the scope of invention. After reading the specification, skilled artisans will appreciate that certain features are, for clarity, described herein in the context of separate embodiments, may also be provided in combination in a single embodiment. Conversely, various features that are, for brevity, described in the context of a single embodiment, may also be provided separately or in any subcombination. Further, references to values stated in ranges include each and every value within that range.
As used herein, the terms “comprises,” “comprising,” “includes,” “including,” “has,” “having” or any other variation thereof, are intended to cover a non-exclusive inclusion. For example, a process, method, article, or apparatus that comprises a list of features is not necessarily limited only to those features but may include other features not expressly listed or inherent to such process, method, article, or apparatus. Further, unless expressly stated to the contrary, “or” refers to an inclusive-or and not to an exclusive-or. For example, a condition A or B is satisfied by any one of the following: A is true (or present) and B is false (or not present), A is false (or not present) and B is true (or present), and both A and B are true (or present). Also, the use of “a” or “an” are employed to describe elements and components described herein. This is done merely for convenience and to give a general sense of the scope of the invention. This description should be read to include one or at least one and the singular also includes the plural unless it is obvious that it is meant otherwise.
Benefits, other advantages, and solutions to problems have been described above with regard to specific embodiments. However, the benefits, advantages, solutions to problems, and any feature(s) that may cause any benefit, advantage, or solution to occur or become more pronounced are not to be construed as a critical, required, or essential feature of any or all the claims.
Although the present invention and its advantages have been described in detail, it should be understood that various changes, substitutions and alterations can be made to the embodiments described herein without departing from the spirit and scope of the invention as defined by the appended claims. Moreover, the scope of the present application is not intended to be limited to the particular embodiments of the process, machine, manufacture, composition of matter, means, methods and steps described in the specification. As one of ordinary skill in the art will readily appreciate from the disclosure of the present invention, processes, machines, manufacture, compositions of matter, means, methods, or steps, presently existing or later to be developed that perform substantially the same function or achieve substantially the same result as the corresponding embodiments described herein may be utilized according to the present invention. Accordingly, the appended claims are intended to include within their scope such processes, machines, manufacture, compositions of matter, means, methods, or steps.
The present application claims priority from PCT Application No. PCT/US 14/42020, filed Jun. 11, 2014, entitled “SEALANT CAP” by Malcolm D. Prouty et al., which in turn claims priority from U.S. Provisional Patent Application Ser. No. 61/833,725 filed Jun. 11, 2013, entitled “SEALANT CAP” by Malcolm D. Prouty et al., all of which are all incorporated by reference herein in their entirety.
This invention was made with Government support and the Government has certain rights in the invention.
Filing Document | Filing Date | Country | Kind |
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PCT/US14/42020 | 6/11/2014 | WO | 00 |
Number | Date | Country | |
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61833725 | Jun 2013 | US |