Aspects relate, in general, to non-incendiary tracer rounds.
Tracers are projectiles that, when fired, provide a visible trajectory to enable the flight path of the projectile to be determined. The visible trajectory thus enables a user to visualise the path of the projectile, and to make ballistic alterations so as to correct the flight path and thus ultimately the end impact point of the projectile. A tracer round will typically comprise a pyrotechnic composition that is ignited when the round is fired. The composition is such that the visible trajectory can be seen by the naked eye in daylight as well as night-time.
According to an example, there is provided a non-incendiary tracer projectile structure for housing an electrically powered illumination source, the tracer projectile structure comprising a jacket comprising a generally pointed forward end and a generally blunt rearward end defining a rear opening, an internal retaining structure disposed towards the rearward end of the jacket to support a protective window that is transparent to a selected electromagnetic wavelength, wherein a portion of the rearward end of the jacket tapers in a radially inward direction whereby to define a circumferential narrowing of the rear opening so configured as to mechanically protect the internal retaining structure. The internal retaining structure can comprise a circumferentially continuous collar on an internal surface of the jacket. The internal retaining structure can comprise multiple radially inwardly projecting protrusions. The internal retaining structure can comprise a circumferential channel in an internal surface of the jacket. The internal retaining structure can comprise multiple circumferential channel portions in an internal surface of the jacket. The multiple circumferential channel portions can be arranged in the same plane.
In an example, the non-incendiary tracer projectile structure can comprise a second internal retaining structure disposed towards the rearward end of the jacket, the second internal retaining structure being axially displaced from the internal retaining structure whereby to define a channel to receive the protective window. The second internal retaining structure can comprise a circumferentially continuous collar on an internal surface of the jacket. The second internal retaining structure can comprise multiple radially inwardly projecting protrusions. The second internal retaining structure can comprise a circumferential channel in an internal surface of the jacket. The second internal retaining structure can comprise multiple circumferential channel portions in an internal surface of the jacket. The multiple circumferential channel portions can be arranged in the same plane. The second internal retaining structure can be displaced, in an axial direction, from the internal retaining structure towards the forward end of the jacket. The second internal retaining structure can be displaced, in an axial direction, from the internal retaining structure towards the rear opening. The internal retaining structure can be disposed on the portion of the rearward end of the jacket. The internal retaining structure can be disposed above, in an axial direction, the portion of the rearward end of the jacket. The second internal retaining structure can be disposed on the portion of the rearward end of the jacket.
According to an example, there is provided a tracer projectile comprising a non-incendiary tracer projectile structure as provided herein, in which the non-incendiary tracer projectile structure is partially provided in a cartridge configured to store a pyrotechnic composition.
Embodiments will now be described, by way of example only, with reference to the accompanying drawings, in which
Example embodiments are described below in sufficient detail to enable those of ordinary skill in the art to embody and implement the systems and processes herein described. It is important to understand that embodiments can be provided in many alternate forms and should not be construed as limited to the examples set forth herein.
Accordingly, while embodiments can be modified in various ways and take on various alternative forms, specific embodiments thereof are shown in the drawings and described in detail below as examples. There is no intent to limit to the particular forms disclosed. On the contrary, all modifications, equivalents, and alternatives falling within the scope of the appended claims should be included. Elements of the example embodiments are consistently denoted by the same reference numerals throughout the drawings and detailed description where appropriate.
The terminology used herein to describe embodiments is not intended to limit the scope. The articles “a,” “an,” and “the” are singular in that they have a single referent, however the use of the singular form in the present document should not preclude the presence of more than one referent. In other words, elements referred to in the singular can number one or more, unless the context clearly indicates otherwise. It will be further understood that the terms “comprises,” “comprising,” “includes,” and/or “including,” when used herein, specify the presence of stated features, items, steps, operations, elements, and/or components, but do not preclude the presence or addition of one or more other features, items, steps, operations, elements, components, and/or groups thereof.
Unless otherwise defined, all terms (including technical and scientific terms) used herein are to be interpreted as is customary in the art. It will be further understood that terms in common usage should also be interpreted as is customary in the relevant art and not in an idealized or overly formal sense unless expressly so defined herein.
The use of pyrotechnic compositions in incendiary tracers means that the location of the shooter can easily be determined by simple visual inspection of the starting point of the visible path that has been caused by ignition of the pyrotechnic agent in question. This can be detrimental to a user if there are hostile observers in the vicinity. Furthermore, since the pyrotechnic composition is gradually exhausted as the tracer is in flight, the trajectory will alter in a manner that is different to that of non-tracer projectiles. The reliability of pyrotechnic tracers can be lowered due to tolerances and environmental factors when creating/processing pyrotechnic chemical ingredients during manufacture, and also when stored and operated in environments with higher humidity (i.e. delayed chemical reaction or in some cases none at all when fired). Furthermore, use of pyrotechnic tracers in hot operational environments can create unintentional fires, causing collateral damage.
Non-incendiary tracers can use a rearwardly directed illumination source that is configured to emit light as the tracer is in flight. The extreme conditions present at the point that the tracer is fired mean that enormous stresses are placed on the light source and associated electronics and power source. There is also an increased risk of failure because exhaust gases present at the point of firing can exert massive pressures on the part of the tracer housing the light source.
According to an example, there is provided a non-incendiary tracer projectile structure for housing an electrically powered illumination source. The tracer projectile structure comprises a jacket comprising a generally pointed forward end and a generally blunt rearward end defining a rear opening. The rear opening can define an aperture which enables the illumination source to emit light from the structure. In an example, an internal retaining structure is disposed towards the rearward end of the jacket to support a protective window that is transparent to a selected electromagnetic wavelength. That is, a protective window can be provided in or near the aperture. The window can be transparent to a selected wavelength that corresponds to the wavelength of light emitted by the illumination source. For example, the illumination source may be configured to emit in the infra-red region of the EM spectrum. Accordingly, a material for the window can be selected to enable transmission of infra-red at the selected wavelength. The material may substantially block (that is, not transmit) other wavelengths, such as those in the visible region of the EM spectrum for example. A portion of the rearward end of the jacket tapers in a radially inward direction whereby to define a circumferential narrowing of the rear opening so configured as to mechanically protect the internal retaining structure.
The circumferential narrowing 113 of the rear opening 107 forms a ‘boat-tail’ feature. Exhaust gases that are produced as a by-product of the firing of a tracer are produced as the primer ignites the propellant. That is, as the propellant burns it generates gases—the sudden, high pressure of this gas that is produced ejects the tracer projectile from the end 201 of the cartridge 200. It is forced down e.g. the barrel of the firing apparatus at high speed (of the order of several hundred m/s). The cartridge 200 remains in the firing apparatus for ejection. The boat-tail feature 113 of the tracer projectile structure protects the internal retaining structure 109, along with the window 111 and any components in the internal section 205 of the jacket 200 from the action of the exhaust gases. It also protects any sealing mechanism used in conjunction with the internal retaining structure 109. For example, adhesive may be used to seal the window to the internal retaining structure 109. Such a seal may fail under normal circumstances as a result of the action of the exhaust gases. The boat-tail feature provides protection by deflecting a proportion of the exhaust gases towards the outside surface 207 of the projectile structure. For example, with reference to
According to an example, the non-incendiary tracer projectile structure can further comprise a second internal retaining structure disposed towards the rearward end of the jacket.
In an example, the second internal retaining structure may be displaced, in an axial direction, relative to the internal retaining structure towards the forward or rearward end of the jacket, that is away from or towards the rear opening. The internal retaining structure can be disposed on the portion of the rearward end of the jacket. That is, the internal retaining structure can be disposed on the portion of the jacket that narrows to form the boat-tail feature. Alternatively, the internal retaining structure can be disposed above, in an axial direction, that (narrowing) portion of the rearward end of the jacket. Similarly, the second internal retaining structure can be disposed on the narrowing portion of the rearward end of the jacket.
The present inventions can be embodied in other specific apparatus and/or methods. The described embodiments are to be considered in all respects as illustrative and not restrictive. In particular, the scope of the invention is indicated by the appended claims rather than by the description and figures herein. All changes that come within the meaning and range of equivalency of the claims are to be embraced within their scope.
Number | Date | Country | Kind |
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20275120 | Jul 2020 | EP | regional |
2010965 | Jul 2020 | GB | national |
Filing Document | Filing Date | Country | Kind |
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PCT/GB2021/051661 | 6/30/2021 | WO |
Publishing Document | Publishing Date | Country | Kind |
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WO2022/013522 | 1/20/2022 | WO | A |
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Number | Date | Country | |
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20230266107 A1 | Aug 2023 | US |