The invention relates generally to platforms for canister munitions. In particular, the invention relates to modular equipment to interchangeably secure containerized ordnance for aerial deployment or transport.
Conventional mounting interfaces for containerized munitions yield disadvantages addressed by various exemplary embodiments of the present invention. In particular, various exemplary embodiments provide a mounting platform for securing munitions. The platform includes a flat plate, a front block and a rear block. The plate includes a plurality of cutouts. The front block has a first saddle disposed between first flanking ends and at least one flange at one of the flanking ends for inserting into a first opening of the cutouts. The rear block has a second saddle disposed between second flanking ends at least one pad for inserting into a second opening of the cutouts. The munitions are disposable atop the first and second saddles of the front and rear blocks.
These and various other features and aspects of various exemplary embodiments will be readily understood with reference to the following detailed description taken in conjunction with the accompanying drawings, in which like or similar numbers are used throughout, and in which:
In the following detailed description of exemplary embodiments of the invention, reference is made to the accompanying drawings that form a part hereof, and in which is shown by way of illustration specific exemplary embodiments in which the invention may be practiced. These embodiments are described in sufficient detail to enable those skilled in the art to practice the invention. Other embodiments may be utilized, and logical, mechanical, and other changes may be made without departing from the spirit or scope of the present invention. The following detailed description is, therefore, not to be taken in a limiting sense, and the scope of the present invention is defined only by the appended claims.
The disclosure generally employs quantity units with the following abbreviations: length in inches (in), mass in pounds (lbm), time in seconds (s) and angles in degrees (°). Supplemental measures can be derived from these, such as density in pounds-per-cubic-inch (lbm/in3), and the like. The purpose of the modular block and mounting plate is to define a common mounting interface for canisterized munitions with varying diameters and lengths designed for quick installation and adjustment.
Conventionally, the only way to launch a canisterized munition from a platform is to use the vendor's launcher, which is exclusive to its own specific munitions. The goal of the exemplary modular block design is to accommodate any munition from the leading suppliers and establish a common mounting interface. Exemplary embodiments provide a modular assembly for attaching canisterized munitions with minimal components in various configurations, including for aerial deployment, loiter and transport.
Holes 750 along the bottom of the flanges 710 enable bolts to be inserted to secure the surface 720 to the plate 620. The block 630 further includes a strap 760 that ends around the outer rods 740 for securing a canister. A hinged clamp 770 cinches the strap 760 in position. The configuration shown includes a pair of flanges 710 joined by rods 740, but this configuration can be expanded to a larger plurality of concatenated flanges 710 in tandem for less concentrated weight distribution.
The exemplary design comprises four components including the rear modular block 120, the front modular block 130 and the mounting plate 140, or alternatively the flanges 630 and the wider mounting plate 620. The front and rear modular blocks 130 and 120 each have a V-shape opening as 370 and 230 respectively that accept Echelon-2 munitions 150 with ranging diameters which are then tied down with the retaining strap 170. The front modular block 130 can be flipped over to accept Echelon-1 munitions 160 using either a Picatinny rail mount adapter 340 or utilizing the flat bridge 330 and retaining strap 170. Alternatively or additionally, generic modular blocks 630 can be similarly employed to provide V-shape saddles 735 to accept a variety of munitions.
The mounting plate 140 includes cutouts 510, 520, 530, 545 and 550 that accept mounting flanges 380 in the front modular blocks 130. For the rear modular block 120, the cutout is isolated to the back of the mounting plate 140, and there is only one corresponding location per Echelon-2 munition 150. For the front modular block 130, the mounting plate 140 has a patterned cutout that facilitates adjustment fore and aft to accommodate munitions of different lengths.
To install the front modular block 130, the bottom pads 270 are disposed into the designated cutouts 520 in the mounting plate 140 at an oblique angle. Then the rear modular block 120 is pivoted down to lie flat on the mounting plate 140 where the bottom feet 260 fall into their designated cutouts 510. The block 130 is then pressed back against the rear block 120 and is locked in place by securing the four latches 210 that drop into their respective cutouts 530.
Installing the front modular block 130 denotes a similar process. The curved flange 380 is dropped at an angle into a pair of its several evenly spaced cutouts row 540 in the mounting plate 140 based on the length of the desired munition 150. The front block 130 is then rotated down to lie flat on the mounting plate 140 where the bottom tangs 390 fall into their respective row of cutouts 540. The front block 130 is then locked down by securing the two downward facing latches 310 into the cutouts under the row 540.
To mount the front modular block 130 upside down for attaching Echelon-1 munitions 160, the same procedure is employed, but utilizing the latches 310 on the opposite face. The tangs 390 have lips that enable the unused latches 310 to secure to and prevent nuisance rattling. The mounting plate 140 can be easily scaled to accept larger canisterized munitions if necessary. Employing the same cutout design, the mounting plate 140 can become longer and provide even more flexibility.
The advantage to the exemplary modular block design utilized in the common launcher is its ability to effectively mount varying sized canisterized munitions. A range of munitions can be locked into position to safely resist the largest launch loads seen in Echelon-2 munitions 150 currently on the market.
The mounting plates 620 include V-shape supports 630 that resemble a shortened version of the front block 130 and featured in detail in view 700. A variety of missiles 870 can be supported by the assembly 810, identified as 871, 872, 873, 874, 875 and 876 in approximate sequential decrease by size.
In these examples, the box 840 contains missiles 872, 873 and 876, while the upper plate 620 supports missiles 871, 874 and 875. For purposes of scale, an example distance between the actuator 870 and a line parallel to the hinge 855 is slightly more than one foot.
No conventional launcher is designed to provide this level of modularity with such easy adjustment within each firing cell. Previously, the U.S. Navy developed a common launcher design. However like the conventional vender-supplied version, that configuration was designed and built around a specific munition or set of munitions and each cell of the launcher could only accept the munition specified.
There is definite commercial potential with this design. Conventionally, companies need to design and manufacture different launchers for each munition they build. Having a design like this one will greatly reduce their testing budget and make their company more desirable by being able to advertise to customers that only one launcher is needed for several of their munitions.
While certain features of the embodiments of the invention have been illustrated as described herein, many modifications, substitutions, changes and equivalents will now occur to those skilled in the art. It is, therefore, to be understood that the appended claims are intended to cover all such modifications and changes as fall within the true spirit of the embodiments.
The invention described was made in the performance of official duties by one or more employees of the Department of the Navy, and thus, the invention herein may be manufactured, used or licensed by or for the Government of the United States of America for governmental purposes without the payment of any royalties thereon or therefor.