The present invention is concerned with improvements to removable fasteners and is particularly related to removable and re-usable fasteners for use in wet-fit applications, such as joining components that include a sealant or adhesive.
In the manufacture of complex structures such as aircraft frames, removable blind fasteners are used as a temporary fixing. The temporary fixing helps to align the components. After inspection and adjustment as required the removable blind fasteners are removed and permanent blind fasteners installed in the apertures.
Some structures, such as fuel tanks, include a layer of sealant or adhesive between sheet materials. During assembly the inter-sheet viscous adhesive or sealant, or “wet” material can clog the apertures into which the blind fasteners are inserted. The wet material can get into the mechanism of the blind fasteners and shorten their lifespan. The problem to be solved is to find a way of protecting the mechanism of the fastener.
A known swaged collar type fastener is described in U.S. Pat. No. 6,077,012. The fastener includes a flexible end disc attached to its free end. The flexible disc has a slightly larger diameter than the bore in a work-piece through which the fastener is inserted so that the fastener is retained in the bore after insertion. The flexible member pushes some debris out of the bore as the fastener is installed in the bore. The primary function of the end disk is to prevent the fastener from falling out of the bore by catching the edges of the hole and collar to retain the fastener. The end disc must therefore be flexible and a flexible disc would simply smear viscous materials within the bore. This would not be acceptable for applications addressed by the present invention because any material left in the bore, particularly adhesives, may cause the fastener to stick in the hole. An efficient way of clearing all debris from the aperture is required.
The present invention overcomes this problem by providing a rigid plunger of substantially the same diameter as the hole, optimised to remove all debris, including viscous adhesives, sealants, swarf and grease, from the bore. This stops unwanted materials getting into the mechanism of the fastener and shortening its lifespan and also removes any material that may harden and prevent removal of the fastener.
A dowelling fastener is provided having a head end and an insertion end and a cylindrical dowelling portion, wherein the fastener is provided with a plunger at the insertion end for clearing material from a hole as the fastener is inserted into the hole, wherein the plunger is rigid and has a circular cross section with a diameter substantially the same as the dowelling portion of the fastener, the plunger tip thereby being a close fit with the hole, wherein the fastener has a dowelling part and a clamping part held together in use by a threaded member that passes through each part to draw them together upon its rotation, wherein the plunger is mounted on the tip of the threaded member. The plunger of the present invention is intended specifically for clearing materials from the bore and therefore has other features optimised for this purpose, including ridges around its periphery.
The plunger may be rigid and may be made of a rigid plastic or soft metal such as brass. The plunger may be permanently fixed to the threaded member or it may be removable. The plunger tip of the dowelling fastener is cylindrical, wherein the side-wall of the plunger tip has at least one groove around its periphery. The groove allows accumulation of any wet material that managed to get past the forward rim of the plunger.
High performance structures, such as those found on modern aircraft, require high precision fabrication techniques. During assembly of, for example, aircraft structures, a series of holes are drilled through the component materials, and permanent fastenings such as rivets are placed and secured. For small structures clamping of the component materials can be along the edge of the materials. For large structures however it is not possible to achieve accurate alignment with this technique. For the assembly of large structures a series of clamping holes are drilled at selected points across the structure. Temporary fasteners are then inserted into these holes to secure the component materials while further holes are drilled to receive permanent rivet fasteners. When rivets have been placed and secured the temporary fasteners are removed and subsequently replaced with permanent rivet fastenings. The number and location of the temporary fastenings will vary between applications, but for a typical wing set, i.e. two complete wings, for a large commercial passenger aircraft, the number of temporary fastenings used can reach around 25,000. It is convenient for such temporary fasteners to be operated from one side of the work-piece only, i.e. to insert and activate the fastener from above the work-piece without having to perform an operation on the underside of the work-piece, for instance screwing or tightening. Not only does one-sided operation simplify the assembly process, it is often the case that the underside of a work-piece is not accessible at all. Fasteners that are operable from a single side of the work-piece are termed “blind” fasteners. A conventional blind fastener is shown in
Specialised parts of the assembled aircraft structure may require laminations of two or more sheets of materials, sandwiching a layer or layers of “wet” materials, such as adhesives, sealants or resins, including mastic, silicon, epoxies or grease. For example a fuel tank will include a layer of sealant between two sheet materials. These wet materials have the characteristic that they are viscous and sticky and easily coat other materials that they come into contact with and are often difficult to remove. Sometimes they have the additional quality that they harden and set and bond tightly to other materials or bond other materials tightly together.
An embodiment of the present invention overcomes this problem by providing a plunger 204 attached to the tip 203 of the fastener, an embodiment of which is shown in
The plunger 204 is cylindrical, having a circular profile and straight parallel walls, with a front face and a rear face, where the walls meet the front and rear faces at a front rim and a rear rim respectively. The front end is the active end facing away from the fastener and is the end that is first inserted into the aperture in the work-pieces. It may be concave to provide a sharpened front rim and therefore a keen scraping edge to remove viscous or granular materials from the internal walls of the work-piece apertures. The concave front end also acts as a scoop. The plunger 204 is hollow and the threaded member 203 fits into this space. There is a close fit between interior walls of the plunger and the threaded member to ensure that the exterior walls of the plunger are parallel to the walls of the dowelling part of the fastener. The plunger 204 may be fixed to the threaded member 203 using an adhesive such as a potting compound, like epoxy resin.
In use, the apertures 501, 503 in work-pieces 301, 303 are aligned as shown in
Preferably the plunger is made of a rigid material so that it does not deform but that is softer than the material of the work-pieces so that it does not damage the work-pieces. A preferred material is a rigid plastic, such as ABS. A soft plastic or rubber is less desirable because it is likely to deform and allow viscous material past, leaving a coating of viscous material in the apertures that could set and prevent removal of the fastener from the apertures. If the work-pieces are made of steel, then brass would be a suitable material for the plunger. However, ease and cost of manufacture of the plunger component is a factor, therefore plastic is preferable as it can be injection moulded or 3D printed. It is important that the plunger can be produced to a high tolerance with an accurate diameter and for the plunger to retain this dimension in use. The plunger should be a very close fit into the aperture, much like the dowelling part of the fastener and the diameter of these two components should be substantially the same. The dowelling part of the fastener should be a close fit within the apertures because it needs to be able to align the work-pieces very accurately. The plunger should be a close fit within the apertures so that it effectively removes material from within the bore.
The plunger tip is attached to the threaded member after the fastener itself has been assembled using an adhesive to fix it permanently. Alternatively, it may be desirable to remove and replace the plunger, for example if the plunger becomes worn, then it can be removably retained on the threaded member with a nut 606, as shown in
The plunger tip 204 could be provided with performance enhancing features, such as ridges or grooves in the walls, as shown in
The troughs formed between the ridges provide a pressure release cavity that can help to scavenge viscous material from the walls of the apertures. A trough immediately behind the front rim 603 of the plunger can provide a sharper leading edge and improve the scraping action of the plunger.
Alternatively a single deep channel 604 can be provided as shown in
Typical diameters of apertures, and therefore plunger diameters could be between ½ cm and 3 cm. Typical lengths for the plunger tip could be between ½ cm and 5 cm.
Number | Date | Country | Kind |
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1613112.0 | Jul 2016 | GB | national |
Filing Document | Filing Date | Country | Kind |
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PCT/IB2017/054473 | 7/24/2017 | WO | 00 |