The present disclosure relates to a vibration resistant initiator assembly having an exploding foil initiator.
This section provides background information related to the present disclosure which is not necessarily prior art.
Initiator assemblies are employed to detonate an input charge to release energy that is subsequently employed to initiate detonation, deflagration or combustion in an output charge. There is a trend in the field of initiator assemblies to employ an exploding foil initiator as the means for initiating detonation of the input charge. Electrical energy input to an exploding foil initiator causes a thin metal bridge to vaporize, which propels a flyer through a barrel and into contact with the input charge. The flyer is typically formed of a relatively thin plastic material and must be accelerated over a relatively short distance (i.e., less than 0.050 inch) to a velocity that is sufficient to initiate the detonation of the input charge. Moreover, the flyer must strike the input charge in a manner that is perpendicular to the axis of the barrel to reduce the risk that contact between the flyer and the input charge will initiate detonation of the input charge.
In situations where the initiator assembly is subjected to a relatively large amount of vibration, there is a risk that portions of the output charge will break apart and migrate within the initiator assembly onto the flyer. This situation is detrimental because it greatly increases the risk that the exploding foil initiator will not be able to detonate the input charge. In this regard, if even a relatively small mass of the material that forms the output charge falls onto the flyer, the additional mass could prevent the flyer from being accelerated to a threshold velocity that is needed to cause the input charge to detonate and/or could cause the flyer to tilt relative to the longitudinal axis of the barrel so that the shock produced by contact between the flyer and the input charge is distributed over time (rather than all at once) so that the input charge is not shocked to a degree that initiates detonation of the input charge.
This section provides a general summary of the disclosure, and is not a comprehensive disclosure of its full scope or all of its features.
In one form, the present disclosure provides an initiator assembly that includes a housing, a base, an exploding foil initiator and an input charge assembly. The housing defines a cavity. The base coupled to the housing and closes the cavity. The exploding foil initiator is mounted to the base and has a barrel that defines an initiation axis. The input charge assembly is received in the cavity and includes a holder and an input charge. The holder has a first axial end and a second axial end that are spaced apart along the initiation axis. The first axial end is closer to an output of the barrel than the second axial end. A charge aperture is formed through the first axial end of the holder and does not extend through the second axial end of the holder. The input charge is formed of an explosive material and is received into the charge aperture.
In another form, the present disclosure provides an initiator assembly that includes a housing, an output charge, an input charge assembly, and a base/EFI assembly. The housing has a housing member and a cover. The housing member has a first axial end and a second axial end and defines a cavity with a first cavity portion, a second cavity portion and a third cavity portion. The first cavity portion extends through the first axial end of the housing member. The third cavity portion extends through the second axial end of the housing member. The second cavity portion is disposed between the first and third cavity portions. The first cavity is larger in diameter than the second cavity portion so as to define a first annular shoulder on the housing member where the first and second cavity portions intersect one another. The second cavity portion is larger in diameter than the third cavity portion so as to define a second annular shoulder on the housing member where the second and third cavity portions intersect one another. The cover is fixedly coupled to the second axial end of the housing member to close an end of the cavity. The output charge is received in the third cavity portion and is at least partly formed of an explosive material. The input charge assembly has a holder and an input charge. The holder is fixedly coupled to the housing member and has a first holder portion and a second holder portion. The first holder portion defines a charge aperture that does not extend fully through the holder. The second holder portion is smaller in diameter than the first holder portion. A third annular shoulder is formed on the holder radially outwardly of where the second holder portion intersects the first holder portion. The first holder portion is received into the second cavity portion and is located along the initiation axis such that the third annular shoulder is spaced apart from the second annular shoulder on the housing member. The second holder portion is partly received in the third cavity portion. The input charge is received into the charge aperture and is formed of an explosive material. The base/EFI assembly has a base, a plurality of terminals, and an exploding foil initiator. The base is fixedly coupled to the housing member. The terminals extend through the base and are electrically coupled to the exploding foil initiator. The exploding foil initiator is coupled to the base. The base/EFI assembly is slidably received into the first cavity portion and closes the cavity on a side of the housing member opposite the cover. The base/EFI assembly is abutted against either an axial end of the holder or a barrier that is abutted against the axial end of the holder.
Further areas of applicability will become apparent from the description provided herein. The description and specific examples in this summary are intended for purposes of illustration only and are not intended to limit the scope of the present disclosure.
The drawings described herein are for illustrative purposes only of selected embodiments and not all possible implementations, and are not intended to limit the scope of the present disclosure.
Corresponding reference numerals indicate corresponding parts throughout the several views of the drawings.
With reference to
With reference to
In the example provided, the housing 12 includes a housing member 50 and a cover 52 that are assembled to one another, but it will be appreciated that the housing 12 could be unitarily and integrally formed as a single, discrete component. The housing member 50 can be a tubular structure having a first axial end 54 and a second axial end 56. A through-bore 58 can be formed through the housing member 50 that is sized to the diameter of the third cavity portion 40. A first counterbore 60 can be formed into the first axial end 54 of the housing member 50 and can form the first annular shoulder 38. A second counterbore 62 can be formed into the first annular shoulder 38 and can form the second annular shoulder 42. It will be appreciated that the first and second annular shoulders 38 and 42 are spaced apart from one another along the initiation axis 36. The through-bore 58 that forms the third cavity portion 40 can extend from the second annular shoulder 42 through the second axial end 56 of the housing member 50. Accordingly, it will be appreciated that the first cavity portion 32 can extend through the first axial end 54 of the housing member 50, while the third cavity portion 40 can extend through the second axial end 56 of the housing member 50.
The cover 52 can be fixedly coupled to the second axial end 56 of the housing member 50 to close an end of the cavity 30. In the example shown, the cover 52 is received into a third counterbore 66 that is formed into the second axial end 56 of the housing member 50. The third counterbore 66 defines a third annular shoulder 68 against which the cover 52 is abutted. Any desired means may be employed to fixedly couple the cover 52 to the housing member 50 to close an end of the cavity 30 on the second axial end 56 of the housing member 50. In the particular example provided, the cover 52 is laser welded to the housing member 50.
With reference to
The exploding foil initiator 16 can include a foundation structure 90, a pair of bridge contacts 92, a bridge 94, a flyer layer 96 and a barrel 98. The foundation structure 90 can be formed of any desired electrically insulating material, such as a ceramic material and/or a resin-impregnated fiberglass material. The bridge contacts 92 and the bridge 94 can be mounted onto the foundation structure 90 in a desired manner, such as via vapor deposition in one or more layers. The flyer layer 96 can be disposed over the bridge contacts 92, the bridge 94 and the foundation structure 90 and can be formed of a suitable material, such as a layer of polyamide. The barrel 98 can be disposed over and abut the flyer layer 96 and can be formed of a suitable material, such as a layer of polyamide. The barrel 98 can define a barrel aperture 100 that can extend fully through the barrel 98 and can be disposed concentrically about the initiation axis 36. The exploding foil initiator 16 can be mounted to the base 14 and each of the bridge contacts 92 can be electrically coupled to an associated one of the terminals 72. The base 14 and the exploding foil initiator 16, together with exploding foil initiator 16 can form a base/EFI assembly 102 that is received at least partly into the first cavity portion 32 of the housing 12.
As shown in
Returning to
The input charge 112 is received into the charge aperture 122 and is formed of a suitable explosive material, such as a secondary explosive material. In the particular example provided, the input charge is formed of RSI-007 which is a secondary explosive material that is available from Reynolds Systems Incorporated of Middletown, California. Those of ordinary skill in the art will appreciate that the term “input charge” not only connotates that the element is formed of an energetic material, but also that this charge is the first charge (and possibly the only charge) in a line or string of charges that are operated when a “flyer” is discharged during operation of the exploding foil initiator 16. In this regard, a shockwave produced when the “flyer” impacts against another structure, such as the input charge 112 or a barrier/cover member 130, is transmitted into the input charge (i.e., either directly or indirectly) to cause the input charge 112 to detonate. Accordingly, it will be understood that the input charge 112 detonates in response to a shockwave that is produced through motion and impact of the “flyer” and not through in response to a shockwave produced by detonation of a charge of an energetic material.
With reference to
With reference to
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Likewise, the input charge 112 can be fitted into the charge aperture 122 in the holder 110. The material that forms the input charge 112 may be compacted prior to its insertion into the holder 110, and/or could be compacted in the holder 110. If the input charge 112 is compacted prior to its insertion into the holder 110, the input charge 112 could be fully compacted (i.e., to a desired density, to a desired volume, and to a desired size), or could be compacted to an intermediate level (e.g., to permit the material that forms the input charge 112 to be received into the charge aperture 122 in a slip-fit or press-fit manner) and thereafter fully compacted once it is received into the holder 110. If a barrier or closure member 130 is employed in the initiator assembly 10 and is received into the open end of the charge aperture 122 and/or mounted to the holder 110, the barrier or closure member 130 can be inserted into the charge aperture 122 and/or mounted to the holder 110 as desired.
The input charge assembly 18 can be received into the housing 12 such that the second holder portion 118 is at least partly received into the through-bore 58 and the first holder portion 116 is received into the second counterbore 62. The input charge assembly 18 can abutted against the output charge 20 and can be secured to the housing 12 to inhibit movement of the holder 110 along the initiation axis 36. In the example provided, a force of a predetermined magnitude is applied to the holder 110 such that the second axial end 128 of the holder 110 is not only abutted against the output charge 20, but also the output charge 20 is in a force transmission path between the holder 110 and the housing 12. The holder 110 can be fixedly coupled to the housing 12, for example by laser welding the holder 110 to the housing 12, while the force of the predetermined magnitude is applied to the holder 110, the output charge 20 and the housing 12 to thereby ensure the absence of void space along the initiation axis 36 in the third cavity portion 40 that would potentially permit movement of the output charge 20, in whole or in part, along the initiation axis 36. Preferably, a compressive axial load is maintained on the output charge 20 along the initiation axis 36 after the holder 110 has been fixedly coupled to the housing 12. To ensure that a compressive load can be maintained on the output charge 20 after fixedly coupling the holder 110 to the housing 12, the spacing of the second annular shoulder 42 away from the first annular shoulder 38 along the initiation axis 36 is larger than the distance between the first axial end 126 of the holder 110 and the fourth annular shoulder 120, and the spacing between the second annular shoulder 42 and the cover 52 along the initiation axis 36 is smaller than the sum of the distance from the fourth annular shoulder 120 to the second axial end 128 of the holder 110 and the overall length of the output charge 20 along the initiation axis 36. The holder 110 may be coupled to the housing 12 at one or more discrete points, for example about the circumference of the first holder portion 116/second counterbore 62. Alternatively, the holder 110 may be coupled to the housing 12 around the entirety of the circumference of the first holder portion 116/second counterbore 62, which may effectively seal the first cavity portion 32 from the third cavity portion 40.
The base/EFI assembly 102 can be received into the housing 12 such that the base 14 is at least partly received into the first counterbore 60 and the base/EFI assembly 102 abutted against the input charge assembly 18 (or against the barrier/closure member 130 if one is employed in the initiator assembly 10). To the extent that a barrier or closure member 130 is employed and it is merely disposed between the input charge assembly 18 and the base/EFI assembly 102, then the barrier or closure member 130 can be received into the cavity 30 in the housing 12 prior to the insertion of the base/EFI assembly 102 into the housing 12. Once the base/EFI assembly 102 has been abutted to the input charge assembly 18 (if no barrier or closure member 130 is employed in the initiator assembly 10) or to the barrier or closure member 130 (if a barrier or a closure member is employed in the initiator assembly 10), the base 14 may be coupled to the housing 12 at one or more discrete points, for example about the circumference of the header body 70/first counterbore 60, to close the cavity 30 at a first axial end 54 of the housing member 50. Alternatively, the base 14 may be coupled to the housing 12 around the entirety of the circumference of the header body 70/first counterbore 60, which may effectively seal the first cavity portion 32 from the atmosphere.
Because neither the holder 110 nor the base 14 engage a hard stop formed on the housing 12, both the holder 110 and the base 14 are able to move along the initiation axis 36 during the assembly process to ensure that a compressive load of a predetermined magnitude is placed on the output charge 20, and to ensure that the base/EFI assembly 102 in general, and more specifically, the axial end of the barrel 98 of the exploding foil initiator 16 that is most distant from the bridge 94, is spaced relative to the input charge 112 or to the barrier or closure member 130 in a desired manner. Where the various components are welded together, for example, the cover 52 and the housing member 50, the holder 110 and the housing member 50 and/or the base 14 and the housing member 50, the configuration that is described above and illustrated in the drawings permits the formation of a butt weld between components (i.e., the welds between the cover 52 and the housing member 50, the holder 110 and the housing member 50, and the base 14 and the housing member 50 are butt welds in the example illustrated). Given the flexibility in the positioning of the holder 110 and the base 14 within the housing 12, it will be appreciated that the initiator assembly 10 can be designed such that the first axial end 54 of the housing member 50 is flush with an outer axial end of the base 14 and that the first axial end 126 of the holder 110 can be flush with the second annular shoulder 42, but that the outer axial end of the base 14 could be recessed below or protrude from the first axial end 54 of the housing member 50 and/or the first axial end 126 of the holder 110 could be recessed into the second counterbore 62 or extend into the first counterbore 60.
In operation, an electrical signal of a predetermined voltage can be applied to one of the terminals 72 to drive electrical current through the bridge 94 to cause the bridge 94 to suddenly convert from a solid into a plasma. The conversion of the material of the bridge 94 into a plasma is associated with a large change in volume that causes a “flyer” to shear from the flyer layer and propel the “flyer” through the barrel 98. Despite the fact that the “flyer” is relatively thin and can be formed from a material such as polyamide, the “flyer” exits the barrel 98 with sufficient energy to generate a shockwave when it impacts the barrier or cover member 130 (if a solid barrier or cover member is present in the initiator assembly 10) or an axial end of the input charge 112 that faces toward the exploding foil initiator 16 (in situations where no barrier or cover member 130 are present in the initiator assembly 10 or when the barrier or cover member 130 is configured to permit the “flyer” to pass through it an impact against the input charge 112). The shockwave is sufficiently strong so that it migrates into the input charge 112, either directly or through the barrier or cover member 130 (if a solid barrier or cover member 130 is present in the initiator assembly 10) to cause the material of the input charge 112 to detonate. Energy produced by the detonation of the material of the input charge 112 can be employed to generate a second, more powerful shockwave that can be employed to rupture the closed end of the holder 110 and initiate detonation of the material that forms the output charge 20.
The foregoing description of the embodiments has been provided for purposes of illustration and description. It is not intended to be exhaustive or to limit the disclosure. Individual elements or features of a particular embodiment are generally not limited to that particular embodiment, but, where applicable, are interchangeable and can be used in a selected embodiment, even if not specifically shown or described. The same may also be varied in many ways. Such variations are not to be regarded as a departure from the disclosure, and all such modifications are intended to be included within the scope of the disclosure.
This application claims the benefit of U.S. Provisional Application No. 63/067,416 filed Aug. 19, 2020, the disclosure of which is incorporated by reference as if fully set forth in detail herein.
Number | Name | Date | Kind |
---|---|---|---|
7430963 | Hennings et al. | Oct 2008 | B2 |
8408131 | Nance | Apr 2013 | B1 |
8485097 | Nance | Jul 2013 | B1 |
8726808 | Nance | May 2014 | B1 |
9038538 | Nance | May 2015 | B1 |
10267604 | Morales | Apr 2019 | B1 |
10267605 | Meadows | Apr 2019 | B1 |
10345084 | Nance | Jul 2019 | B1 |
10557692 | Amendola | Feb 2020 | B1 |
10605576 | Nance et al. | Mar 2020 | B1 |
10794670 | Nance et al. | Oct 2020 | B1 |
11009319 | Morales | May 2021 | B1 |
20080134921 | Nance | Jun 2008 | A1 |
20080148982 | Hennings | Jun 2008 | A1 |
20090151584 | Desai | Jun 2009 | A1 |
20170045342 | Fisher | Feb 2017 | A1 |
20200109927 | Amendola | Apr 2020 | A1 |
Entry |
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U.S. Appl. No. 17/011,358, filed Sep. 3, 2020. |
Number | Date | Country | |
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63067416 | Aug 2020 | US |