Classifications

• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F41—WEAPONS
  • F41G—WEAPON SIGHTS; AIMING
  • F41G1/00—Sighting devices
  • F41G1/30—Reflecting-sights specially adapted for smallarms or ordnance
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F41—WEAPONS
  • F41G—WEAPON SIGHTS; AIMING
  • F41G1/00—Sighting devices
  • F41G1/32—Night sights, e.g. luminescent
  • F41G1/34—Night sights, e.g. luminescent combined with light source, e.g. spot light
  • F41G1/35—Night sights, e.g. luminescent combined with light source, e.g. spot light for illuminating the target, e.g. flash lights
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F41—WEAPONS
  • F41G—WEAPON SIGHTS; AIMING
  • F41G1/00—Sighting devices
  • F41G1/38—Telescopic sights specially adapted for smallarms or ordnance; Supports or mountings therefor
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F41—WEAPONS
  • F41G—WEAPON SIGHTS; AIMING
  • F41G1/00—Sighting devices
  • F41G1/44—Spirit-level adjusting means, e.g. for correcting tilt; Means for indicating or correcting tilt or cant
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F41—WEAPONS
  • F41G—WEAPON SIGHTS; AIMING
  • F41G3/00—Aiming or laying means
  • F41G3/14—Indirect aiming means
  • F41G3/145—Indirect aiming means using a target illuminator
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F41—WEAPONS
  • F41G—WEAPON SIGHTS; AIMING
  • F41G1/00—Sighting devices
  • F41G1/46—Sighting devices for particular applications
  • F41G1/48—Sighting devices for particular applications for firing grenades from rifles

Definitions

• the present invention relates to a sighting system for ammunition firearm having a bell trajectory.
• EP1 818 645 It is known from EP1 818 645 to superpose on a target a mobile red point to a target to improve the aim of a shot bell.
• bell shooting we mean here a ballistic fire for which the difference between the direct angle of view and the elevation angle of the weapon correcting the effect of gravity is high, in particular, beyond 5 at 10 °.
• EP 2 221 571 proposes a similar solution in which a double separation prism acts as a reflective surface to return the image of the red dot to the desired position.
• the elevation is determined by the rotation of a moving mirror.
• a first aspect of the invention is to provide a sighting system combining the illumination and the mobile red dot in a single synchronous device.
• a second aspect of the invention is to provide a sighting system allowing the user to correct the azimuthal drift of a munition due to the Magnus effect.
• the present invention relates to a movable red dot sight comprising a first fixed light source and a first reflective plate, the light source generating a first collimated light beam which is projected on the reflective plate to materialize a red dot or reticle visible to the shooter by the reflection on the reflecting plate and the first beam being projected onto the reflecting plate via a rotating mirror whose angle of inclination with respect to the first light beam is adjustable.
• the movable red dot viewfinder of the invention comprises at least one or a suitable combination of the following features:
• the viewfinder comprises an illuminator / designator in which said viewfinder comprises a second fixed light source generating a second collimated light beam initially parallel to the first light beam returned by said rotating mirror to a second reflecting plate disposed at a 90 ° angle of the first reflective strip for illuminating / designating a target;
• the first and / or the second reflecting plate is a semi-transparent separating plate
• the viewfinder comprises a device for adjusting the angle of inclination of the rotating mirror with respect to the light beams, allowing adjustment of the angle of the mirror as a function of the distance from the target and / or the type of munition;
• the adjustment device is equipped with a graduation representing the distance of the target
• the adjustment device is equipped with several graduations suitable for different types of ammunition
• the adjustment device comprises a motor or mechanical actuator for adjusting the angle of the rotating mirror and a ballistic computer which controls said motor / actuator and which makes it possible to calculate and set the required angle of the mirror according to the distance from target and type of ammunition used;
• the ballistic computer is equipped with a rangefinder that automatically communicates the distance of the target when the shooter triggers the measurement;
• the first and / or second light source comprises a collimator with a convergent lens and a light source placed at the focus of the collimator lens;
• the diameter of the generated light beam is reduced, preferably of the order of 15 mm or smaller;
• the light source of the beam of the red dot is quasi-point, preferably with a diameter of the order of one tenth of a millimeter or millimeter;
• the light source of the red dot is formed by an LED placed behind a mask located at the focus of the collimator lens and pierced with a hole at the location of the optical axis of the generated light beam;
• the lateral position of the reticle is automatically moved laterally by a device controlled by the ballistic computer according to the type of ammunition used and the distance from the target, so as to correct the trajectory deviation of the ammunition due to the Magnus effect ;
• the viewfinder includes a ballistic computer equipped with an inclinometer which measures the angle of tilt of the weapon, the calculator determining the angle of tilt of the weapon correcting the Magnus effect, indications in the viewfinder indicating when this tilt is reached.
• Figure 1 shows the general parameters of a bell shooting.
• Figures 2 and 3 show a side view of a sighting system according to the invention.
• Figure 4 shows a top view of a sighting system according to the invention.
• FIG. 5 represents an exemplary display of a sighting system according to the invention.
• the basic idea of the invention is to use a single mobile part to define on the one hand the position of a red mobile point, and secondly, the angle between an illumination beam / designation and the firing axis of the weapon.
• This system comprises two separate sources 30,36 illuminating the same reflective movable plane 32 (mirror). These two distinct sources are collimated and / or focused by optical means 31, 37 and the beams obtained are parallel to each other. These two sources are vertically fixed.
• the light source 30 serving the mobile red point is returned by the movable mirror 32 to a first semi-reflecting surface 34,53 which returns to the eye of the user 1.
• the semi-reflective surface then allows to superimpose the moving red dot to the target.
• the angle at which this red dot is viewed is regulated by the position of the moving mirror 32.
• the light source 30 serving the mobile red dot is a quasi-point source of low intensity. It can for example be part of a screen of good resolution, so as to allow the display of other information.
• the light source 36 for illumination is returned by the same movable mirror 32 to a second reflecting surface 35,54 perpendicular to the first which returns to the target 2.
• the angle under which is then emitted beam illumination is parallel to the beam of the moving red dot, but oriented at 180 °.
• This second reflecting surface may be semi-reflective or not. Indeed, it can be sufficiently offset laterally to not interfere with the user's field of vision. Nevertheless, in order not to hinder the user's field of vision, this surface is preferably semi-reflective.
• the return angle of the movable mirror may for example be modified by an electric actuator, electromagnetic, piezoelectric, or any other suitable means.
• the illumination source is intense enough to illuminate a distant target. It can also have a wavelength out of the visible, for example in the case of use of night vision device (IR).
• the light sources are, for example, placed in the focal plane of an optical system 31, 37.
• the laser beam is already collimated and does not require additional optics.
• the fixed mirrors can be advantageously replaced by prisms.
• the refraction induces a reduction in the displacement of the light beams on the reflective surfaces 53, 54, which makes it possible to reduce the length of these, and therefore the overall size of the system.
• These prisms are preferably integrated with two separator cubes 51, 52 for superimposing the image of the target to the reticle.
• the bright red dot and the designation beam can advantageously be moved to correct the azimuth direction by laterally displacing the corresponding light sources in their respective focal planes. This displacement can be obtained by an actuator or by the lateral displacement of the reticle on a screen.
• the telescope of the invention then comprises an inclinometer measuring the angle of cant of the weapon and an optical display projected from the focal plane of the lens 31 of the red dot.
• the light source of the red dot advantageously comprises a screen of good resolution, allowing both to display the tilt information (tilt) and the red dot.
• a cant angle correcting the Magnus effect is determined, the optical display indicating to the user when this cant angle is reached.
• the crosshair may flash when the tilt angle is reached.
• FIG. 5 shows a display including tilt angle indications.
• visual cues 21 define the ideal angle
• a line segment 20 indicates the actual inclination of the weapon.
• FIG. 5 (a) represents the situation where a zero tilt angle is sought, for example in the case where the azimuthal correction is obtained by displacement of the reticle.
• Figure 5 (b) shows the situation in which visual cues have been tilted to give information the shooter must tilt the weapon to correct the Magnus effect.
• FIG. 5 (c) the inclination has been corrected and the weapon is in the firing position (ie, the inclination mark 20 is aligned with the visual cues 21).
• This aspect of the invention can be used in combination with the simultaneous use of an illuminator, or independently of it.

Landscapes

• Engineering & Computer Science (AREA)
• General Engineering & Computer Science (AREA)
• Physics & Mathematics (AREA)
• Optics & Photonics (AREA)
• Telescopes (AREA)
• Illuminated Signs And Luminous Advertising (AREA)
• Eye Examination Apparatus (AREA)
• Stroboscope Apparatuses (AREA)

Applications Claiming Priority (2)

Publications (1)

Family

ID=56609634

Family Applications (2)

Family Applications Before (1)

Country Status (13)

Families Citing this family (6)

Family Cites Families (21)

• 2016
  • 2016-07-15 BE BE2016/5594A patent/BE1024403B1/fr not_active IP Right Cessation
• 2017
  • 2017-07-11 WO PCT/EP2017/067429 patent/WO2018011219A1/fr unknown
  • 2017-07-11 DK DK17739248.7T patent/DK3485218T3/da active
  • 2017-07-11 WO PCT/EP2017/067432 patent/WO2018011221A1/fr unknown
  • 2017-07-11 ES ES17739248T patent/ES2797983T3/es active Active
  • 2017-07-11 KR KR1020197003846A patent/KR20190039508A/ko active IP Right Grant
  • 2017-07-11 JP JP2019523174A patent/JP2019523387A/ja not_active Ceased
  • 2017-07-11 EP EP17739248.7A patent/EP3485218B1/fr active Active
  • 2017-07-11 SG SG11201811194RA patent/SG11201811194RA/en unknown
  • 2017-07-11 AU AU2017297740A patent/AU2017297740A1/en not_active Abandoned
  • 2017-07-11 KR KR1020197003912A patent/KR20190039511A/ko not_active Application Discontinuation
  • 2017-07-11 SG SG11201811134VA patent/SG11201811134VA/en unknown
  • 2017-07-11 AU AU2017297742A patent/AU2017297742A1/en not_active Abandoned
  • 2017-07-11 BR BR112019000556-0A patent/BR112019000556A2/pt not_active IP Right Cessation
  • 2017-07-11 US US16/317,278 patent/US10921092B2/en active Active
  • 2017-07-11 EP EP17739250.3A patent/EP3485219A1/fr not_active Withdrawn
  • 2017-07-11 PL PL17739248T patent/PL3485218T3/pl unknown
  • 2017-07-11 US US16/317,284 patent/US20200386517A1/en not_active Abandoned
  • 2017-07-11 BR BR112019000563-3A patent/BR112019000563A2/pt not_active Application Discontinuation
  • 2017-07-11 JP JP2019523176A patent/JP2019523388A/ja active Pending
• 2018
  • 2018-12-30 IL IL264018A patent/IL264018A/en unknown
  • 2018-12-30 IL IL264026A patent/IL264026A/en unknown

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