The subject matter disclosed herein generally relates to armor, more specifically to armor structures and methods of making the same.
Certain lightweight materials used for armor are not very durable. High performance polyethylene (HPPE) is a layered composite that has a very weak inter-laminar strength and very soft resin system. Repeated flexing or impacts can significantly reduce the HPPE's ability to stop projectiles. The resin system used is also very susceptible to fluid damage and certain chemicals common to environments in which the armor is used (e.g., jet fuel in an aircraft).
Generally long, unbroken fibers are desired for composite parts. To this end conventional techniques include wrapping a core in a single sheet of composite in one concurrent layup and cure cycle. However, the resulting product suffers from strength and fluid resistance limitations and such products are prone to failure.
Such conventional methods and systems have generally been considered satisfactory for their intended purpose. However, there is still a need in the art for improved armor and methods of making armor. The present disclosure provides a solution for this need.
Discloses is an item of armor including a ballistics arresting core, a first shell layer disposed on a first side of the ballistics arresting core, and a second shell layer disposed on a second side of the ballistics arresting core such that the second shell layer partially overlaps the first shell layer at an edge of the first shell layer to seal the ballistics arresting core within the first shell layer and the second shell layer.
In addition to one or more of the features described above, or as an alternative, in further embodiments the second shell layer overlaps the first shell layer along the edge of the first shell layer at a side of the ballistics arresting core and/or within an aperture defined in the ballistics arresting core.
In addition to one or more of the features described above, or as an alternative, in further embodiments at least one of the first shell layer and the second shell layer include between two to six plies of material.
In addition to one or more of the features described above, or as an alternative, in further embodiments one or more apertures is defined in at least one of the first shell layer and the second shell layer to correspond to one or more apertures in the ballistics arresting core, wherein walls that form the apertures are covered by the first shell layer and/or second shell layer.
In addition to one or more of the features described above, or as an alternative, in further embodiments at least one of the first shell layer and the second shell layer include fiber reinforced polymer.
In addition to one or more of the features described above, or as an alternative, in further embodiments the fiber reinforced polymer includes pre-impregnated carbon-fiber.
In addition to one or more of the features described above, or as an alternative, in further embodiments one or more exterior coatings.
In addition to one or more of the features described above, or as an alternative, in further embodiments the exterior coatings include one or more of a non-skid coating or paint.
In addition to one or more of the features described above, or as an alternative, in further embodiments an edge of the first shell layer includes a beveled surface.
These and other features of the systems and methods of the subject disclosure will become more readily apparent to those skilled in the art from the following detailed description taken in conjunction with the drawings.
So that those skilled in the art to which the subject disclosure appertains will readily understand how to make and use the devices and methods of the subject disclosure without undue experimentation, embodiments thereof will be described in detail herein below with reference to certain figures, wherein:
Reference will now be made to the drawings wherein like reference numerals identify similar structural features or aspects of the subject disclosure. For purposes of explanation and illustration, and not limitation, an illustrative view of a portion of an embodiment of an item of armor in accordance with the disclosure is shown in
Referring to
Referring to
As shown, the second shell layer 105 can overlap the first shell layer 103 along the edge 103a of the first shell layer 103 at a side 103c of the ballistics arresting core 101. In certain embodiments, the edge 103a of the first shell layer 103 can include a beveled surface as shown (e.g., formed by overlaying a plurality of plies of the same length and bending the plies around a corner of the ballistics arresting core 101).
The first shell layer 103 and/or second shell layer 105 can include between two to six plies of material. The first shell layer 103 and/or the second shell layer 105 can include a polymer (e.g., polyuria). In certain embodiments, the polymer can be fiber reinforced (e.g., using carbon-fiber, fiberglass, or any other suitable material). In certain embodiments, the fiber reinforced polymer can include pre-impregnated carbon-fiber or any other suitable fiber (e.g., wet layup carbon-fiber).
Referring to
Referring again to
A method for manufacturing an item of armor (e.g., item 100, 200, 300) includes coating a first side 101a of a ballistics arresting core 101 with a first shell layer 103 to create a partially coated ballistics arresting core 101. The partially coated ballistics arresting core 101 can be placed in a vacuum bag, and the vacuum bag can be depressurized. The partially coated ballistics arresting core 101 in the depressurized vacuum bag can be cured (e.g., in an autoclave) to create a partially shelled ballistics arresting core 101 (e.g., core 101 with only the first shell layer 103 affixed thereto). The first shell layer 103 and/or the second shell layer 105 can be disposed on the core in any suitable manner (e.g., using wet layup, using pre-impregnated fiber).
The method further includes removing the partially shelled ballistics arresting core 101 from the vacuum bag, coating a second side 101b of the partially shelled ballistics arresting core 101 with a second shell layer 105 to create a fully coated ballistics arresting core 101, and placing the fully coated ballistics arresting core 101 in a vacuum bag. The method includes depressurizing the vacuum bag and curing the fully coated ballistics arresting core 101 in the depressurized vacuum bag to create a fully shelled ballistics arresting core 101 (e.g., as shown in
Coating a second side of the partially shelled ballistics arresting core can include partially overlapping the first shell layer 103 with the second shell layer 105 along an edge 103a of the first shell layer 103 to seal the ballistics arresting core 101 within the first shell layer 103 and the second shell layer 105. Partially overlapping the first shell layer 103 can include overlapping the edge 103a of the first shell layer at a side 103c of the ballistics arresting core 101 and/or within an aperture defined in the ballistics arresting core 101 (e.g., as shown in
Coating the first shell layer 103 and/or second shell layer 105 can include using between two to six plies of material for the first shell layer and/or the second shell layer. In certain embodiments, each ply can be about 0.01 inches thick. Any other suitable number or thicknesses of plies of material is contemplated herein.
The method can include cutting or stamping one or more apertures in the first shell layer 103 and/or the second shell layer 105 to correspond to one or more apertures in the ballistics arresting core 101. For example, a hole can be cut in the first shell layer 103 and/or the second shell layer 105 that aligns with a hole in the ballistics arresting core 101. In certain embodiments, the is hole in the first shell layer 103 and/or the second shell layer can be smaller than a corresponding hole in the ballistics arresting core 101 such that there is sufficient material to cover at least a portion of the walls of the ballistics arresting core 101 that define the hole (e.g., such that the force of the depressurized vacuum bag presses the layer material into the hole to wrap the walls that define the hole).
In certain cases, there may be excess material (e.g., flash 207 as shown in
In certain embodiments, the method can include coating the first shell layer 103 and/or the second shell layer 105 with one or more exterior coatings. The exterior coatings can include one or more of a non-skid coating, paint, or any other suitable coating. Any other suitable preprocessing or post processing for any components as described above is contemplated herein.
Certain embodiments as described above include a composite wrapped armor system encapsulating an armor material in a composite shell. Non ballistic materials can also be incorporated into the shell for use as spacers, mounts, or for any other suitable use. Any suitable number of armor components (e.g., cores 101) can be within sealed within a single shell, or separate armor components (e.g. cores 101) can be placed in a secondary shell (e.g., such that there are alternating layers of shells and cores 101). Multiple items (e.g., 100, 200, 300) can be bonded together by an adhesive or mechanical fastening system to form any suitable armor system (e.g., configured to mount to helicopter or other aircraft). By way of example, aspects of this disclosure can be used in inside or as part of a structural system and/or armor system for any suitable vehicle (e.g., a rotorcraft, an airplane, a ground based vehicle).
As described above, embodiments of the method of manufacture are counterintuitive as multiple layup, cure, and/or trim and/or handling cycles for a single part, whereas traditional methods use only a single stage. The method as described above can allow complex items of armor (e.g., having apertures, mounts, etc.) to be formed. While embodiments of the method described above would appear to increase the time and material cost to make an item of armor, but can actually save time and cost on complex items.
Items of armor as described above provide an improved fluid barrier to separate the internal components for the surrounding environment, provide an improved impact resistance for the internal components, provide an improved structural support to the internal components (e.g., core 101), allow the incorporation of mounting features for one or more items of armor (e.g., for a vehicle armor system), provide increased ballistic performance (e.g., with reduced back deformation), and allows the use of the armor material as the forming tool. Certain embodiments allow for reduced manufacturing time and cost overall, especially for items of armor with complex geometry.
The methods and systems of the present disclosure, as described above and shown in the drawings, provide for improved items of armor with superior properties. While the apparatus and methods of the subject disclosure have been shown and described with reference to embodiments, those skilled in the art will readily appreciate that changes and/or modifications may be made thereto without departing from the spirit and scope of the subject disclosure.
The present invention is a divisional of U.S. patent application Ser. No. 15/428,904, filed Feb. 9, 2017 and published on Oct. 19, 2017 as U.S. 2017/0299346 and claims priority to U.S. Provisional Application Ser. No. 62/294,383 filed Feb. 12, 2016, the contents of which are incorporated herein by reference in their entireties.
Number | Name | Date | Kind |
---|---|---|---|
3649426 | Hodgeman et al. | Mar 1972 | A |
3783449 | Davis | Jan 1974 | A |
4660223 | Fritch | Apr 1987 | A |
5996115 | Mazelsky | Dec 1999 | A |
6053696 | Roberts et al. | Apr 2000 | A |
6185738 | Sidebottom | Feb 2001 | B1 |
6327954 | Medlin | Dec 2001 | B1 |
6571677 | Kaura | Jun 2003 | B1 |
7520205 | Quinn et al. | Apr 2009 | B1 |
8382033 | Reece | Feb 2013 | B2 |
8491835 | Schmidt | Jul 2013 | B2 |
8549803 | Retzloff et al. | Oct 2013 | B1 |
8616113 | Gallo | Dec 2013 | B2 |
8777161 | Pollock et al. | Jul 2014 | B2 |
8968616 | Cioffi | Mar 2015 | B2 |
9032706 | Marshall | May 2015 | B2 |
20050193667 | Henry et al. | Sep 2005 | A1 |
20070034074 | Ravid et al. | Feb 2007 | A1 |
20080092730 | Hall | Apr 2008 | A1 |
20080264244 | Ravid et al. | Oct 2008 | A1 |
20090282968 | Colliflower et al. | Nov 2009 | A1 |
20110214559 | Lampo | Sep 2011 | A1 |
20110214560 | Skertchly | Sep 2011 | A1 |
20110220281 | Dipietro | Sep 2011 | A1 |
20120174759 | Gallo | Jul 2012 | A1 |
20120291621 | Sayre et al. | Nov 2012 | A1 |
20130284339 | Cellarius | Oct 2013 | A1 |
20140230638 | Waldrop | Aug 2014 | A1 |
20150268009 | Tunis, III | Sep 2015 | A1 |
20150323289 | Seauk | Nov 2015 | A1 |
20150362293 | Strauss | Dec 2015 | A1 |
20160231088 | Blackmore et al. | Aug 2016 | A1 |
20170299346 | Hallquist et al. | Oct 2017 | A1 |
Number | Date | Country | |
---|---|---|---|
20180372454 A1 | Dec 2018 | US |
Number | Date | Country | |
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62294383 | Feb 2016 | US |
Number | Date | Country | |
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Parent | 15428904 | Feb 2017 | US |
Child | 16122569 | US |