EP3940331A1 - Traceurs non incendiaires - Google Patents

Traceurs non incendiaires Download PDF

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Publication number
EP3940331A1
EP3940331A1 EP20275120.2A EP20275120A EP3940331A1 EP 3940331 A1 EP3940331 A1 EP 3940331A1 EP 20275120 A EP20275120 A EP 20275120A EP 3940331 A1 EP3940331 A1 EP 3940331A1
Authority
EP
European Patent Office
Prior art keywords
jacket
retaining structure
internal retaining
incendiary
tracer projectile
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
EP20275120.2A
Other languages
German (de)
English (en)
Inventor
designation of the inventor has not yet been filed The
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
BAE Systems PLC
Original Assignee
BAE Systems PLC
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by BAE Systems PLC filed Critical BAE Systems PLC
Priority to EP20275120.2A priority Critical patent/EP3940331A1/fr
Priority to PCT/GB2021/051661 priority patent/WO2022013522A1/fr
Priority to US18/005,409 priority patent/US11965722B2/en
Priority to CA3189132A priority patent/CA3189132A1/fr
Priority to AU2021309750A priority patent/AU2021309750A1/en
Priority to EP21737766.2A priority patent/EP4182627A1/fr
Publication of EP3940331A1 publication Critical patent/EP3940331A1/fr
Ceased legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
    • F42B12/38—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information of tracer type
    • F42B12/382—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information of tracer type emitting an electromagnetic radiation, e.g. laser beam or infrared emission

Definitions

  • 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.
  • 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.
  • 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.
  • 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.
  • 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.
  • 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.
  • 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.
  • the illumination source may be configured to emit in the infra-red region of the EM spectrum.
  • 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.
  • FIG. 1 is a schematic representation of a non-incendiary tracer projectile structure according to an example.
  • the comprises a jacket 100 comprising a generally pointed forward end 103 and a generally blunt rearward end 105.
  • the rearward end 105 defines a rear opening 107.
  • An internal retaining structure 109 is disposed towards the rearward end 105 of the jacket 100 to support a protective window 111 that is transparent to a selected electromagnetic wavelength.
  • a portion 113 of the rearward end 105 of the jacket 100 tapers in a radially inward direction (D) whereby to define a circumferential narrowing of the rear opening 107 so configured as to mechanically protect the internal retaining bead 109.
  • the protective window 111 may comprise Polycarbonate, Sapphire, Fused Quartz, Laminated Toughened Glass.
  • FIG. 2 is a schematic representation of a non-incendiary tracer projectile structure according to an example.
  • the structure as described with reference to figure 1 is shown in combination with a cartridge 200.
  • the cartridge is used to house a propellant and a primer that are used to eject the tracer projectile structure from a firing apparatus (such as a gun for example).
  • the cartridge 200 does not form part of the present projectile structure but is described with reference to figure 2 in order to explain a function of the circumferential narrowing of the rear opening 107.
  • the bottom cartridge 200 of the tracer covers the majority of the tracer up to approximately the horizontal line 202 at the base of the nose 103.
  • the cartridge 200 will be expelled, leaving the tracer and nothing obstructing the window 107 during flight.
  • the tracer projectile structure and cartridge form a tracer projectile.
  • 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.
  • exhaust gases moving in direction E are deflected around the boat-tail feature of the structure towards a region defined by the outer surface 207 of the rearward end 105 of the structure and the internal surface 209 of the cartridge 200.
  • the frangible connection 211 between cartridge and the projectile structure is broken and the tracer is ejected.
  • the continuing action of the exhaust gas as the tracer is in an ejection phase, and specifically its effect on the retaining structure, is mitigated by the boat-tail feature as the tracer is ejected from the firing apparatus.
  • Figure 3 is a schematic representation of a non-incendiary tracer projectile structure according to an example.
  • an internal retaining structure 109 is depicted in greater detail in a side on cut away view.
  • the retaining structure 109 comprises a circumferentially continuous collar 301 on an internal surface 303 of the jacket 100.
  • the window 111 can be provided on the collar, and a seal 305 may be provided to adhere/seal the window to an inner surface of the jacket 100.
  • the seal 305 is provided above the window 111, but may be provided below such as at the interface between the window 111 and the retaining collar 301, or in both locations.
  • Figure 4 is a schematic representation of a non-incendiary tracer projectile structure according to an example.
  • an internal retaining structure 109 is depicted in greater detail in plan view.
  • the retaining structure 109 comprises multiple radially inwardly projecting protrusions 401.
  • the window 111 can be provided on the protrusions 401, and a seal 305 may be provided to adhere/seal the window to an inner surface of the jacket 100.
  • Figure 5 is a schematic representation of a non-incendiary tracer projectile structure according to an example.
  • an internal retaining structure 109 is depicted in greater detail in a cut away side view.
  • the retaining structure 109 comprises a circumferential channel 501 in an internal surface 503 of the jacket 100.
  • the window 111 can be provided in the channel 501, and a seal 305 (or seals) may be provided to adhere/seal the window to an inner surface of the jacket 100.
  • Figure 6 is a schematic representation of a non-incendiary tracer projectile structure according to an example.
  • the internal retaining structure comprises multiple circumferential channel portions 601 in an internal surface of the jacket.
  • the portions 601 may be arranged in the same plane or in different planes. That is, multiple circumferential rows of channels may be provided, each row being offset, in an axial direction, from one another.
  • the window may have multiple circumferential protrusions arranged to complement the multiple channels. That is, the protrusions of the window may be so arranged as to engage into channels in the jacket whereby to enable the window to be fixedly mounted within the jacket.
  • the non-incendiary tracer projectile structure can further comprise a second internal retaining structure disposed towards the rearward end of the jacket.
  • Figure 7 is a schematic representation of a non-incendiary tracer projectile structure according to an example.
  • the second internal retaining structure 701 is axially displaced from the internal retaining structure 109 whereby to define a channel 703 to receive the protective window.
  • the channel in the example of figure 7 is defined by way of the retaining structures rather than being provided within the inner wall of the jacket as in the example of figure 5 for example.
  • the second internal retaining structure 701 may comprise a circumferentially continuous collar on an internal surface of the jacket, or may be composed of multiple radially inwardly projecting protrusions, similarly to other examples described above.
  • the second internal retaining structure 701 may comprise a circumferential channel in an internal surface of the jacket, or multiple circumferential channel portions in an internal surface of the jacket.
  • the multiple circumferential channel portions can be arranged in the same plane such that they form an annular band of channel portions, or in different planes (in an axial direction) from one another, thereby forming more than one annular band of channel portions.
  • 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.
  • the internal retaining structure can be disposed above, in an axial direction, that (narrowing) portion of the rearward end of the jacket.
  • the second internal retaining structure can be disposed on the narrowing portion of the rearward end of the jacket.

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Health & Medical Sciences (AREA)
  • Electromagnetism (AREA)
  • Optics & Photonics (AREA)
  • Toxicology (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
EP20275120.2A 2020-07-16 2020-07-16 Traceurs non incendiaires Ceased EP3940331A1 (fr)

Priority Applications (6)

Application Number Priority Date Filing Date Title
EP20275120.2A EP3940331A1 (fr) 2020-07-16 2020-07-16 Traceurs non incendiaires
PCT/GB2021/051661 WO2022013522A1 (fr) 2020-07-16 2021-06-30 Traceurs non incendiaires
US18/005,409 US11965722B2 (en) 2020-07-16 2021-06-30 Non-incendiary tracers
CA3189132A CA3189132A1 (fr) 2020-07-16 2021-06-30 Traceurs non incendiaires
AU2021309750A AU2021309750A1 (en) 2020-07-16 2021-06-30 Non-incendiary tracers
EP21737766.2A EP4182627A1 (fr) 2020-07-16 2021-06-30 Traceurs non incendiaires

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP20275120.2A EP3940331A1 (fr) 2020-07-16 2020-07-16 Traceurs non incendiaires

Publications (1)

Publication Number Publication Date
EP3940331A1 true EP3940331A1 (fr) 2022-01-19

Family

ID=71786883

Family Applications (1)

Application Number Title Priority Date Filing Date
EP20275120.2A Ceased EP3940331A1 (fr) 2020-07-16 2020-07-16 Traceurs non incendiaires

Country Status (1)

Country Link
EP (1) EP3940331A1 (fr)

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2013133854A1 (fr) * 2011-04-12 2013-09-12 Armtec Defense Products Co. Actionnement/déclenchement par gaz propulseur d'un traceur de projectile non-pyrotechnique
DE102014111852A1 (de) * 2014-08-19 2016-02-25 Rheinmetall Waffe Munition Gmbh Leuchtspursatz für aus einer Rohrwaffe verschießbare Leuchtspurmunition
EP3457077A1 (fr) * 2017-09-18 2019-03-20 BAE SYSTEMS plc Munition trançante éléctronique

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2013133854A1 (fr) * 2011-04-12 2013-09-12 Armtec Defense Products Co. Actionnement/déclenchement par gaz propulseur d'un traceur de projectile non-pyrotechnique
DE102014111852A1 (de) * 2014-08-19 2016-02-25 Rheinmetall Waffe Munition Gmbh Leuchtspursatz für aus einer Rohrwaffe verschießbare Leuchtspurmunition
EP3457077A1 (fr) * 2017-09-18 2019-03-20 BAE SYSTEMS plc Munition trançante éléctronique

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