Projectile with pyrotechnically timed release of a secondary payload
11561075 ยท 2023-01-24
Assignee
Inventors
Cpc classification
F42C19/0838
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F42B12/58
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F42B12/48
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F42C9/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F42B12/62
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F42B12/62
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F42C19/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F42C9/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F42B12/32
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
The present invention relates to a firearm projectile capable of releasing a secondary payload mid-flight through a pyrotechnic timing mechanism. Once the firearm is fired, the powder in the casing pushes out the projectile as a typical round. In addition, the powder ignites the delay column. The formulation and amount of delay pyrotechnics determines the delay time. When the delay column is burned, the final portion ignites an expelling charge. The expelling charge builds pressure in the projectile casing and separates the base plug from the main projectile housing. The expelling assembly pushes out the secondary payload out the rear of the projectile. Although the payload exits the rear of the projectile at minimum velocity, the net velocity of the payload is still in the forward direction.
Claims
1. A projectile comprising; a projectile body, a projectile base, a delay column section having a first end and a second end, at least one opening in the projectile body for the delay column section, a delay composition, at least one expelling charge, an expelling assembly, and a secondary payload; wherein, when the projectile is fired, the delay composition burns from the first end towards the second end of the delay column section, thereby igniting the at least one expelling charge; wherein igniting of the at least one expelling charge separates the projectile base from the projectile body and causes the expelling assembly to move towards the first end of the delay column section; wherein the expelling assembly pushes the secondary payload out the rear of the projectile body.
2. The projectile of claim 1, wherein the delay column section is adjacent to the expelling charge and the delay composition is disposed within the delay column section such that firing the projectile ignites the delay composition and the delay composition ignites the expelling charge.
3. The projectile of claim 2, wherein the expelling assembly is disposed between the at least one expelling charge and the delay column section, wherein the delay column section comprises a tube that passes through a common central axis of the projectile body and projectile base.
4. A projectile comprising: a projectile body, a projectile base, a delay column section having a first end and a second end, at least one opening in the projectile body for the delay column section, a delay composition, at least one expelling charge, an expelling assembly, and a secondary payload; wherein the delay column section is adjacent to the expelling charge and the delay composition is disposed within the delay column section such that firing the projectile ignites the delay composition and the delay composition ignites the expelling charge; wherein the expelling assembly is disposed between the at least one expelling charge and the delay column section, wherein the delay column section comprises a tube that passes through a common central axis of the projectile body and projectile base; and wherein the secondary payload is disposed radially between the projectile body and the delay column section and disposed axially between the expelling assembly and the projectile base.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) The detailed description of the drawings particularly refers to the accompanying figures in which:
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DETAILED DESCRIPTION OF THE DRAWINGS
(7) 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.
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(9) The pressure created by the expelling charge 11 creates a force on expelling assembly 13, causing expelling assembly 13 to move towards the first end of the delay column section 7 and push the secondary payload 15 (e.g., spheres, flechettes, string/nets, RFID tags, etc.) out the rear of the projectile body 3. Although the secondary payload 15 exits the rear (relative to projectile 1 flight path) of the projectile body 3 at minimum velocity, the net velocity of the secondary payload 15 is still in the forward direction relative to the firearm user. As the secondary payload 15 exits the projectile body, the secondary payload spreads out. Because the secondary payload 15 travels within the projectile body 3 prior to exiting the projectile body, the secondary payload receive the aerodynamic advantages of projectile body 3 during the delay time, allowing the secondary particles to travel further before being subjected to drag upon each individual projectile of secondary payload 15. Secondary payload 15 can be selected based on the desired effect. In at least some embodiments, a tracer composition 19 can be placed within projectile base 5 such igniting the powder in case 17 also ignites the tracer composition. The properties of secondary payload 15 can be selected (e.g., choice of materials, addition of filler, etc.) to modify the flight properties (e.g., stability, aerodynamics, etc.) of projectile 1 and secondary payload 15.
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(14) A method of manufacturing projectiles includes providing a projectile body, a projectile base, delay column section, a delay composition, at least one expelling charge, an expelling assembly, and a secondary payload; inserting the expelling assembly into the projectile body; inserting the secondary payload into the projectile body; inserting the at least one expelling charge into the projectile base; inserting the delay composition within the projectile base; coupling the expelling assembly to the projectile base with a first interference fit; and coupling the projectile base to the projectile body with a second interference fit. The first interference fit should be stronger than the second interference fit so that the projectile base can separate from the projectile body during flight a pull the expelling assembly.
(15) 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.