The field of invention relates generally to containers. More particularly, it pertains to an ammunition container lid for use with historical ammunition canisters.
It is known to provide various weapon systems on a variety of vehicles, including aircraft. With respect to helicopters, machine guns have been mounted within cabin areas, on window sills, and on external store supports. A key part of these weapon systems include the ammunition container, which are used to store ammunition and feed the weapon. Current ammunition containers that are known and disclosed in the art utilize a lid that feed and rotate on opposite axes, with one of them being in the forward direction. The ammunition can lids that are known and disclosed in the art present multiple problems to the operator. First, these prior art lids are designed to open directly into airstream during flight. Second, prior art lids and feed trays are independent of one another and open on two axes, one of which is directly opposed the airstream while in flight. As can be appreciated, this design creates unnecessary hazards to the operator, as the lid and/or feed tray can slam shut on the operator while in flight, thereby potentially causing injuries. As is shown from the above, there is a need for a new and improved ammunition can that affords improved safety to the operator while in use.
The present disclosure relates to an ammunition container lid for use with an ammunition canister. The container lid includes a four-sided frame, a cover, a hinge assembly, a feed tray, a latch, and a Last Round Switch. The hinge assembly includes a repeating pattern of ammunition can hinge sections, feed tray hinge sections, and cover hinge sections with a press-fit rod holding the sections together. The lid has an integrated aerodynamic forward face that matches the curvature of the ammunition can. The feed tray assembly is incorporated into the container lid to prevent a reduction in ammunition can capacity. The cover and feed tray rotate on the same axis, thereby resulting in simplified, ergonomic operation, which eliminates the problems inherent in current designs that can open directly into the airstream during flight. The inventive lid does not require special tools for installation/removal and does not reduce ammunition can capacity.
According to an illustrative embodiment of the present disclosure, it is an object of the invention to provide a new and improved ammunition container lid that has all the benefits of the prior art and none of the disadvantages.
According to a further illustrative embodiment of the present disclosure, it is an object of the invention to provide a new and improved ammunition container lid and feed tray that rotate on the same axis in the outboard direction.
According to a yet another illustrative embodiment of the present disclosure, it is an object of the invention to provide a new and improved ammunition container lid that does not open directly into the airstream during flight.
According to a yet another illustrative embodiment of the present disclosure, it is an object of the invention to provide a new and improved ammunition container lid that utilizes existing attachment points on ammunition can.
According to a yet another illustrative embodiment of the present disclosure, it is an object of the invention to provide a new and improved ammunition container lid that does not require special tools for installation/removal.
According to a yet another illustrative embodiment of the present disclosure, it is an object of the invention to provide a new and improved ammunition container lid that does not reduce ammunition can capacity.
According to a yet another illustrative embodiment of the present disclosure, it is an object of the invention provide to a new and improved ammunition container lid with a latch that is easy to operate one-handed with gloves.
According to a yet another illustrative embodiment of the present disclosure, it is an object of the invention to provide a new and improved ammunition container lid with an integrated aerodynamic forward face, matching the curvature of can.
Additional features and advantages of the present invention will become apparent to those skilled in the art upon consideration of the following detailed description of the illustrative embodiment exemplifying the best mode of carrying out the invention as presently perceived.
The detailed description of the drawings particularly refers to the accompanying figures in which:
The embodiments of the invention described herein are not intended to be exhaustive or to limit the invention to precise forms disclosed. Rather, the embodiments selected for description have been chosen to enable one skilled in the art to practice the invention.
Generally, provided is an ammunition canister lid for an ammunition canister comprising: a four-sided frame, a cover, a hinge assembly, a feed tray, a latch, and a Last Round Switch; wherein the four-sided frame attaches to the ammunition container at one or more ammunition can attachment points; wherein the hinge assembly comprises a repeating pattern of ammunition can hinge sections, feed tray hinge sections, and cover hinge sections with a rod holding the ammunition can hinge sections, the feed tray hinge sections, and the cover hinge sections together; wherein the hinge assembly attaches to the four-sided frame on one side; and wherein the cover and the feed tray rotate independently and on a same axis.
In an illustrative embodiment, the hinge assembly comprises a one-piece rod that secures the ammunition can hinge sections, the feed tray hinge sections, and the cover hinge sections together. In an illustrative embodiment, the hinge assembly comprises a first rod that secures a first set of ammunition can hinge sections, the feed tray hinge sections, and the cover hinge sections together, and a second rod that secures a second set of ammunition can hinge sections, the feed tray hinge sections, and the cover hinge sections together. In an illustrative embodiment, the Last Round Switch comprises an actuator, a steel flap, and an indicator; wherein the actuator is depressed by the steel flap that is in contact with ammo feeding through the feed tray; wherein once a quantity of the ammo has been depleted and is no longer pushing against the flap, the actuator extends and sends a signal to the indicator. In an illustrative embodiment, the ammunition canister lid further comprises an integrated aerodynamic forward face that matches the curvature of the ammunition canister. In an illustrative embodiment, the latch comprises a ball grip with a square spring. In an illustrative embodiment, the feed tray comprises a bottom surface that does not extend into the ammunition container envelope to prevent a reduction in ammunition can capacity.
In one illustrative embodiment, the integrated aerodynamic forward face 109 matches the curvature of can. The designs that currently exist in the art are not aerodynamic, and therefore increase aerodynamic drag. Additionally, the rounded design of the container lid 101 reduces snag hazards. In an illustrative embodiment, the integrated aerodynamic forward face 109 comprises 0.25″ rounds added to container lid 101 to reduce elbow hazard risk during gun operation. An additional advantage of the inventive lid is that it has a smaller footprint than currently existing ammunition container lids. In an illustrative embodiment, the underside is hollow for weight reduction.
Although the invention has been described in detail with reference to certain preferred embodiments, variations and modifications exist within the spirit and scope of the invention as described and defined in the following claims.
The present application claims priority to U.S. Provisional Patent Application Ser. No. 63/316,563, filed Mar. 4, 2022, entitled “WEAPON SYSTEM AMMUNITION CANISTER LID,” the disclosure of which is expressly incorporated by reference herein.
The invention described herein was made in the performance of official duties by employees of the Department of the Navy and may be manufactured, used and licensed by or for the United States Government for any governmental purpose without payment of any royalties thereon. This invention (Navy Case 210,073 is assigned to the United States Government and is available for licensing for commercial purposes. Licensing and technical inquiries may be directed to the Technology Transfer Office, Naval Surface Warfare Center Crane, email: Crane_T2@navy.mil.
Number | Date | Country | |
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63316563 | Mar 2022 | US |