The present invention relates to a targeting system for firearms for munitions having a parabolic trajectory.
It is known from document EP 1 818 645 to superpose on a target a red dot that is movable to a target in order to improve the targeting of a parabolic shot. By parabolic shot, what is meant here is a ballistic shot for which the difference between the direct angle of sight and the angle of elevation of the weapon correcting for the effect of gravity is large, in particular, in excess of 5 to 10°. Document EP 2 221 571 proposes a similar solution in which a two-prism beamsplitter plays the role of reflective surface for steering the image of the red dot to the desired position. In these two documents, elevation is set by rotating a movable mirror.
It is sometimes necessary, besides superposition of a movable red dot, to designate or illuminate the target. These two documents have nothing to say on this subject.
A first aspect of the invention aims to provide a targeting system combining illumination and movable red dot into a single synchronous device.
A second aspect of the invention aims to provide a targeting system allowing the user to correct for 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 that is projected onto the reflective plate in order to materialize a red dot or reticle that is visible to the shooter in reflection from the reflective plate and the first beam being projected onto the reflective plate by way of a rotatable mirror the angle of inclination of which with respect to the first light beam is adjustable.
By parabolic shot, what is meant in the present description is a shot for which the difference between the angle of elevation of the target and the angle of elevation for the shot is larger than 10°.
According to preferred embodiments of the invention, the movable red dot sight of the invention includes at least one, or a suitable combination, of the following features:
The idea behind the invention consists in using one and the same movable part to define, on the one hand, the position of a movable red dot, and on the other hand, the angle between an illuminating/designating beam and the bore axis of the weapon.
This system comprises two separate sources 30, 36 that illuminate the same reflective movable plane 32 (mirror). These two separate sources are collimated and/or focused by optical means 31, 37 and the obtained beams are parallel to each other. These two sources are vertically fixed.
The light source 30 that serves for the movable red dot is steered by the movable mirror 32 toward a first semi-reflective surface 34, 53 that steers it toward the eye of the user 1. The semi-reflective surface then allows the movable red dot to be superposed on the target. The angle at which this red dot is seen is adjusted via the position of the movable mirror 32.
The light source 30 that serves for the movable red dot is a point-like source of low brightness. It may for example form part of a screen of good resolution, so as to allow other information to be displayed.
The light source 36 that serves for the illumination is steered by the same movable mirror 32 toward a second reflective surface 35, 54 that is perpendicular to the first, which steers it toward the target 2. The angle at which the illuminating beam is then emitted is parallel to the beam of the movable red dot, but, oriented at 180°. This second reflective surface may optionally be semi-reflective. Specifically, it may be sufficiently offset laterally in order not to obstruct the field of view of the user. Nevertheless, in order not to obstruct the field of view of the user, this surface is, preferably, semi-reflective.
The steering angle of the movable mirror may for example be modified by a piezoelectric, electromagnetic or electrical actuator, or any other suitable means.
The illuminating source is sufficiently bright to illuminate a distant target. It may furthermore have a wavelength outside of the visible, for example in the case of use of a night-vision device (IR).
So as to obtain beams of plane waves (collimated or parallel beam) the light sources are, for example, placed in the focal plane of an optical system 31, 37. In the case of certain types of laser pointers, the laser beam is already collimated and no additional optics are required.
Such as described in document EP 2 221 571, which is incorporated herein by reference, the fixed mirrors, or one thereof, may advantageously be replaced by prisms. In this case, specifically, refraction induces a decrease in the movement of the light beams over the reflective surfaces 53, 54, this allowing the length thereof, and therefore the bulk of the system, to be decreased. These prisms are preferably integrated into two beamsplitter cubes 51, 52 allowing the image of the target to be superposed on the reticle.
Lastly, when the Magnus effect is to be taken into consideration, the luminous red dot and the designating beam may advantageously be moved to correct the azimuthal direction by moving the corresponding light sources laterally in their respective focal planes. This movement may either be obtained by an actuator or by lateral movement of the reticle over a screen.
Another way of taking into account the Magnus effect is to take advantage of the azimuthal error introduced by a non-zero cant. Advantageously, the sighting scope of the invention then comprises an inclinometer that measures the cant of the weapon and an optical display projected from the focal plane of the lens 31 of the red dot. In this case, the light source of the red dot advantageously comprises a screen of good resolution, allowing both inclination (cant) information and the red dot to be displayed.
Preferably, depending on the distance of the target, a cant correcting for the Magnus effect is determined, the optical display indicating to the user when this cant is achieved. For example, the reticle may flash when the cant is achieved.
Number | Date | Country | Kind |
---|---|---|---|
BE2016/5594 | Jul 2016 | BE | national |
Filing Document | Filing Date | Country | Kind |
---|---|---|---|
PCT/EP2017/067429 | 7/11/2017 | WO | 00 |