CN1147299A - Laser small arms transmitter - Google Patents
Laser small arms transmitter Download PDFInfo
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- CN1147299A CN1147299A CN95192856.2A CN95192856A CN1147299A CN 1147299 A CN1147299 A CN 1147299A CN 95192856 A CN95192856 A CN 95192856A CN 1147299 A CN1147299 A CN 1147299A
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- laser
- casing assembly
- optics
- wedge
- optics wedge
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
- F41A33/00—Adaptations for training; Gun simulators
- F41A33/02—Light- or radiation-emitting guns ; Light- or radiation-sensitive guns; Cartridges carrying light emitting sources, e.g. laser
Abstract
A laser small arms transmitter which may be affixed to the stock of a rifle such as an M16 used by a soldier in training with a multiple integrated laser engagement system. The transmitter includes a housing assembly having a forward end with a window through which the beam of a laser diode is emitted. A pair of optical wedges are positioned inside the housing assembly between the laser diode and the window. The optical wedges are supported for independent rotation about a common optical axis for steering the laser beam. An alignment head may be physically mated to the rearward end of the housing assembly for driving a pair of shafts to rotate the optical wedges in the alignment of the transmitter so that a soldier can accurately hit a target once he or she has located the target in the conventional sights of the rifle. The laser transmitter may also include a sensor for detecting the firing of a blank cartridge, a fire LED mounted inside the housing for producing an optical signal to indicate to the alignment head that the laser diode has been energized, and an inductive switch connected to a power circuit and actuable by an induction coil in the alignment head to energize the laser diode.
Description
The technical field of the invention
The present invention relates to military training equipment, what relate in particular to that a kind of soldier of army uses in military exercises is fixed on generating laser on the rifle.
Background technology of the present invention
For many years, armed Forces of the United States uses the soldier that trains troops of the belligerent system of multiple comprehensive laser (MILES).The rifle that a laser small arms transmitter (SAT) is fixed on rifle such as M16 is done, each soldier has detector on its helmet and bullet braces, be used for surveying and whether hit by laser " bullet ", the soldier pulls the trigger of its rifle, penetrate a gap bullet, the true shooting of simulation is live, and audio sensor triggers the laser small arms transmitter.
Must adjustment laser small arms transmitter, like this, in case within target in soldier's mission is positioned at conventional rifle gunsight the time, he or she is goal exactly just.In the past, old-fashioned laser small arms transmitter is done to rifle with bolting, and be adjusted to the iron sight of weapon consistent with laser beam.The shortcoming of this method is that this machinery weapon aiming tool must be through resetting, so that use rifle under situation under battle conditions, in order to overcome this defective, the conventional laser small arms transmitter that uses is equipped with the mechanical interlinked mechanism that is used to change laser light orientation now.
Form by the combination configuration of 144 detectors that are used to link to each other by the existing small arms adjustment positioner (SAAF) that is used to the belligerent system of multiple comprehensive laser small arms transmitter is harmonized that armed Forces of the United States uses, be used for determining the position of laser hit according to the target graticule with 35 printed circuit boards.Use the difficult problem of existing small arms adjustment positioner be the soldier without stabilized platform his or his weapon aiming be in 25 meters far away combination configuration, in many cases, the soldier makes his or his weapon-shooting with a kind of mode that causes aiming point not drop on desired locations.This combination configuration and soldier be at a distance of 25 meters far away, this with regard to having caused because snow, mist, wind and in sunrise or the visibility that the lighting condition difference occurs when dust is arranged limit.
Existing small arms adjustment positioner calculates the number that is positioned at orientation and elevation angle error " card is taken " sound, the clatter number that shows existing small arms adjustment positioner with four groups of electro-mechanical display indicators, the soldier then rotates the adjuster of its conventional small arms transmitter according to correct direction, calculate the respective number of clatter, then, he or she must make weapon aiming and shooting, the corresponding adjustment that adds again.This repetitive process is carried out continuously, till the soldier obtains the indication at zero point of existing laser small arms adjustment positioner.This is a kind of expending time in very much and dull process, because each soldier just has normal aiming error in the time of must regaining the target graticule and produces, reach the optimum state of its shooting ability as a soldier with harmonize his or his weapon of 15 fens clock times, but, still can not harmonize exactly, this is a common occurrence.
Alignment procedure with existing small arms adjustment positioner not only expends time in, and expense is also very expensive, because must use a large amount of empties, be not used in the gap bullet of igniting, the laser instrument of conventional small arms transmitter does not excite, and perhaps uses a kind of special mute emission rope of penetrating, and existing small arms adjustment positioner is not supported optical sighting device and dissimilar small arms, do not support night-vision devices yet, nor the coding that can check laser beam energy exactly and accept laser beam.
Therefore, it is desirable to provide a kind of laser small arms transmitter that can cancel the function admirable of the configuration that must use general objective.This laser small arms transmitter preferably can carry out more rapidly the accurately automatic adjustment of aiming again.In addition, the output of the laser power of this modified laser small arms transmitter preferably has different energy and coding, so that the belligerent system of multiple comprehensive laser that makes manpower consume part can distinguish between the hit that is formed by small arms not of the same race.
Purpose of the present invention
Therefore, main purpose of the present invention provides a kind of laser small arms transmitter that is used for the function admirable of the belligerent system of multiple comprehensive laser.Technical scheme of the present invention
The invention provides a kind of generating laser that can be installed on the small arms.This generating laser have one can be substantially along the laser machine of the target excitation laser beam of weapon.The adjustment head of electro-mechanical alignment system can link to each other with generating laser, is used to adjust transmitter, so that according to orientation and elevation angle control laser beam, till the boresight of laser beam and weapon is in full accord.
In conjunction with Figure of description of the present invention,, can understand purpose of the present invention, advantage and feature more easily according to following detailed explanation.
Brief description of drawings
Figure 1A is that a soldier aims at it and is in the perspective view that automatic player discerns small arms laser alignment system rifle.
Figure 1B is the clear more side view that makes the alignment system after Figure 1A part is removed of signal.
Fig. 2 is Figure 1A and the display board of Figure 1B alignment system control device and the amplification front elevation of various keys.
Fig. 3 is one of a preferred embodiment exploded perspective illustration of amplifying that is installed in the laser small arms transmitter of the present invention on the rifle shown in Figure 1A and Figure 1B.
Fig. 4 carries out illustrating of laser beam control with the optics wedge.
Fig. 5 A and 5B are the side view and the front views of Figure 1A and 1B alignment system adjustment head.
Fig. 6 is that lens, spectroscope, target graticule and position sensing detector one of Figure 1A and 1B alignment system Optical devices illustrates.
Fig. 7 is a total calcspar of Figure 1A and Figure 1B alignment system.
Fig. 8 is the optical output power of Figure 1A and Figure 1B alignment system control device and the calcspar of the accurate checking circuit of coding.
Most preferred embodiment of the present invention
Referring to Figure 1A and 1B, adopt the mode of the laser small arms transmitter 12 that the rifle be bolted to the small arms 14 (as the M16 rifle) that used by the soldier of army in military exercises does that the preferred embodiments of the present invention are described.This small arms transmitter 12 is designed to an available alignment system 10 to be adjusted automatically, alignment system 10 comprises a rectangular hollow transition shell 16 that becomes horizontal alignment in use, the hinged end cap 18 of the lockable of shell 16 can rotate up, be fixed on its inner control device 20 so that show, soldier's 21 aimings are positioned at the weapon 14 of shell 16, soldier 21 wears a helmet 21a, carry a bullet braces 21b on the body, on helmet 21a and the braces 21b laser detector is housed all, is used for surveying the hit situation of military exercises laser " bullet ".Control device 20 comprises a box-type shell 22 (illustrating as Fig. 2) that has LCD display 24.Shell 22 also has a key plate that is the membrane keyboard shape.This keyboard is around display 24 and comprise push type key 26,28,30,32,34,36, reach 38.
A collapsible sliding rail 40 can stretch out from the rear end level of base component 42 (shown in Figure 1B), and base component 42 is fixed on the bottom surface of shell 16.The gun barrel 44 of rifle 14 firmly is supported on the last fulcrum of rigid triangle weapon support 46, and support 46 usefulness bolts are fixed firmly to the middle part of base component 42.The trigger control panel (not shown) of rifle 14 is fixed on the anchor clamps 48 that are arranged on the track 40, and anchor clamps 48 have knob 50 and 52, is respectively applied for the orientation and the elevation angle of the gun barrel 44 of adjusting rifle 14 movably.After rifle 14 being fixed on weapon support 46 and the anchor clamps 48, soldier 21 (Figure 1A) just aims at the video (Fig. 6) that is the target graticule 54 of uniformity projection with the weapon aiming tool, below will be elaborated to this.
Box-shaped Optical devices 56 (Figure 1A and 1B) are rigidly fixed in the front portion (Figure 1B) of base component 42, Optical devices 56 comprise convex lens 58 (Fig. 6) and a spectroscope 60, spectroscope 60 sees through the infrared light from laser small arms transmitter 12, but reflect visible light.Target graticule 54 (Fig. 6) is fixed within the Optical devices 56 that are positioned at below the laser beam axis, spectroscope 60 is positioned at the front of convex lens 58, and makes its angle at 45, so that with the projection of target graticule video, pass convex lens 58 to the infinity.The position sensing detector 62 that is arranged in Optical devices 56 is accepted laser beam L2, and produces a kind of error signal that occurs displacement between laser beam receiving position and target graticule video and represent.Then adjust laser small arms transmitter 12, hit up to laser beam L2 till the center of detector 62.
The control circuit that will be positioned at control device 20 (Fig. 1) is connected to be harmonized on 64, and this adjustment 64 links to each other with the rear robot of laser small arms transmitter 12 on being fixed by bolts to rifle 14.Control circuit causes 64 laser that repeatedly inspire in the laser small arms transmitter 12 of harmonizing.Utilize error signal, control circuit will make the head of harmonizing rotate a pair of prism wedge 66 and 68 (Fig. 3) that is positioned at small arms transmitter 12 independently, each prism wedge all comprises one around spur gear, so that adjust the orientation and the elevation angle of laser beam, till the bore sight of laser beam and weapon trajectory 44 is harmonized fully.
Alignment system 10 of the present invention can carry out automatic boresight with oppose all u.s.a. military affairs specialty small arms and machine gun to be harmonized, and modern weapons is had full applicability.The automatic operation of this alignment system can guarantee to make after 21 pairs of weapons of soldier 14 carry out single once initial aiming laser small arms transmitter 12 to obtain (in 1 minute), accurate and conforming boresight rapidly.The optical sighting device and the night-vision devices that use aiming anchor clamps 48 can guarantee to be contained on the weapon 14 can not influence the boresight process.All alignment systems 10 all are placed in the firm transition shell 16, and this shell 16 also helps sunshade and the rainy day gas of becalming, this alignment system 10 in alignment procedure without empty, so, can be in all case as this system of use on the indoor table top.Initial this alignment system 10 of assembling comprises three easy steps, and they are that battery is installed in the control device shell 22 (Fig. 1), presses control (BIT) key 30 (Fig. 2) and presses the weapon kind that key 34 selections will be harmonized.Display 24 can provide next step suitable operational order to the operator, so that carry out next step operation.In case carry out after the adjustment preparation when alignment system 10, just according to harmonize his or his weapon of the instruction on the display 24, general operation sequence is as follows for soldier 21:
(a) soldier will harmonize and 64 be fixed on the laser small arms transmitter 12;
(b) soldier with his or his weapon put into aiming anchor clamps 48 and weapon fore-stock 46;
(c) soldier utilizes aiming anchor clamps orientation and the elevation angle to adjust knob 50 and 52, makes the image of the illumination target graticule 54 that can see in his or his the weapon aiming Optical devices;
(d) soldier presses and proceeds key 28 (Fig. 2), operates according to the instruction on the display 24.Carve in due course,, just can select weapon type by pressing key 34 according to the inquiry that provides on the display;
(e) soldier backs out, and presses the adjusting key 26 that is installed on the control device shell 22;
(f) soldier waits on the display 24 and provides " harmonize and finish " instruction (ALIGNMENTCOMPLETE), and this instruction meeting provided with interior at 1 minute; And
(g) soldier removes weapon according to the instruction that finishes of harmonizing from alignment system.
In alignment procedure, even alignment system 10 is run into any problem, for example low energy, mistake laser code or control problem, this alignment system will be informed the soldier, the laser small arms transmitter 12 of this weapon breaks down need be to its place under repair.
Whole operating process of the calcspar explanation alignment system 10 of Fig. 7.Weapon 14 is fixed on has in 64 the aiming anchor clamps 48 harmonized.Harmonize and 64 to be connected on the laser small arms transmitter 12.Optical devices 56 comprise the gunsight that the makes weapon illumination target graticule 54 to its aiming.When pressing adjusting key 26 (Fig. 2), control device 20 causes laser small arms transmitter 12 repeat its transmission, monitors the shooting light-emitting diode display (not shown) of the laser small arms transmitter that is fixed on indicator form 70 (Fig. 3) back simultaneously, so that proper handling.Optical devices 56 sensing laser positions also send the data of these positions to control device 20.Like this, control device 20 will be determined required correcting value.Control device 20 causes the necessary adjustment of adjustment 64 dos that is fixed on the laser small arms transmitter 12 again.This process is carried out incessantly continuously, till laser small arms transmitter 12 is accurately harmonized.Control device 20 is checked laser energy size and laser code with Optical devices 56, thereby can carry out the adjustment of laser small arms transmitter as requested.Below further describe five part primary clusterings of alignment system 10 in detail.
Optical devices 56 (Figure 1B) are sub-assemblies, and it gives soldier 21 54 projections of illumination target graticule during boresight, and senses the position of weapon laser beam according to graticule.Illumination graticule 54 can be assisted soldier's 21 boresights at illumination condition when poor (as dusk or dawn).Fig. 6 illustrates the operating process of Optical devices 56 main elements, and single big convex lens 58 play laser beam and sight and focus on any effect on the sensor detector 62 of lengthwise position, and this point is positioned on the focus of convex lens 58.When with laser beam convex lens incidence angle (non-adjustment) out of square, that the position that is positioned on the detector 62 will be offset.The amount that detector 62 quantitatively is offset passively, and to 20 error signals of control device.This detector is a solid-state devices preferably, as four line detectors (quad-detetor), perhaps can be a line detector that has simulated power output.Spectroscope 60 is arranged in laser beam passway, its reflect visible light, simultaneously, it makes and passes from himself from the infrared light in the laser.Spectroscope is pressed 45 support, when arriving, make the video projection of target graticule 54, pass convex lens with convenient laser.With visible light source such as light-emitting diode display 72 illumination run-home graticules 54, and make its location, like this, projection image is just to drop on the zero point of position sensing detector 62 on same the optical axis.No longer need Optical devices 56 are adjusted, alignment system 10 also needn't contain except that detector 62 and as other any electronic component the light-emitting diode display light source 72 of illumination target graticule 54.
L-shape protection baffle plate 74 (Fig. 1) is rigidly fixed on the base component 42 between weapon gun barrel 44 tops and the Optical devices 56 with bolt, and this baffle plate can prevent that the soldier from striking the convex lens 58 of Optical devices unintentionally with gun barrel 44 when rifle 14 being installed on support 46 and the anchor clamps 48.Baffle plate has a hole of passing from it, is covered by a metal screen 76, is used to make laser to pass, and this bore dia can be 8 millimeters, so that make laser pass through its through Optical devices 56.Do not wish to cover this hole,, make laser beam scattering or refraction, will cause the inaccuracy of operation like this because this class material can be dirty with glass or some other solid transparent material.
64 (a Fig. 5 A and a 5B) that harmonize are electro-mechanical devices, with a cable 65 (Figure 1A) it are linked to each other with small arms transmitter 12, and according to the instruction that control device 20 sends, adjust the laser position of laser small arms transmitter automatically.Harmonize and 64 to contain an induction coil 78 (Fig. 5 A), inspire the laser of laser small arms transmitter with this induction coil 78, and, when needed, by key 30 (Fig. 2) with the identification of its transfer test person to the laser small arms transmitter, harmonizing 64 also has a detector 80, and its monitoring laser small arms transmitter shooting light-emitting diode display 70 is so that determine its mode of operation.Two miniature deceleration transmission motors 82 and 84 (Fig. 5 B) be positioned at 64 a related with it biased teeth wheels 86 and 87 of harmonizing and be used to be rotatably installed in non-slip coupling (not shown) on a pair of power transmission shaft 118 and 120, shaft coupling is assemblied on the end of adjustment spools 106 and 108 of laser small arms transmitter.The motor 82 and 84 of harmonizing is driven and is controlled by control device 20 in the boresight process, simultaneously, and the laser of Optical devices 56 sensing laser small arms transmitters, and provide real-time feedback information to control device 20.
The laser small arms emission is hit 12 (Fig. 3) and is comprised a casing assembly 88 and a dismountable closure assemblies 90, and this closure assemblies 90 forms the rearward end that the laser small arms emission is hit.Laser diode module 92 is installed in the casing assembly 88 and by a power supply circuits energy supply that is contained on the control panel 94, control panel 94 also is fixed in the casing assembly 88.Make power supply circuits work by the induction change-over switch 96 that is fixed in the rear case component 90, be laser diode module 92 energy supplies.Drive owing to the energy supply of induction coil 78 (Fig. 5 A) makes the induction change-over switch, induction coil 78 is overlapped on the top of casing assembly 88 (Fig. 3), and is consistent with induction change-over switch 96.
The front end of laser small arms launcher shell assembly 88 (Fig. 3) forms porose 98 and 100, and the audio frequency or the optical sensor (not shown) that are used to survey emission gap bullet are positioned at hole 100, and links to each other with circuit on the control panel 94.The transparent window 102 that is used to make the light beam from laser diode module 92 to pass is installed in another Windows 98.An optics collar 104 is fixed on form 102 back, optics wedge 66 and 68 is supported on form 102 back rotationally, make independent rotation by power transmission shaft 106 and 108 respectively, this power transmission shaft front end has pinion 106a and 108a, and what be respectively applied for engagement optics wedge 66 and 68 has tooth circumference (spur gear) part.Power transmission shaft 106 and 108 axle journals are supported on the bearing (as 110 and 112), and power transmission shaft 106 and 108 rear end put in the hole (not shown) that is arranged in rear case component 90, with O shape ring 114 and 116 with rear case component 90 sealing positions.The end of this power transmission shaft is protected with rigid flange 90a, and rigid flange 90a vertically stretches out from rear case component 90.
When handle is harmonized 64 (a Fig. 5 A and a 5B) when being connected to the rear case component 90 of laser small arms transmitter 12, the non-slip coupling (not shown) of harmonizing on 64 the power transmission shaft 118 and 120 (Fig. 5 B) just links to each other with the end of power transmission shaft 106 and 108, is connected so that provide with the driving of motor 82 and 84.
Fig. 4 illustrates by 64 the motor 82 and 84 of harmonizing and controls the situation of laser beam B by the independent rotation of optics wedge 66 and 68.Can be with the optics wedge as the beam-control element in the photosystem.Passing the minimum deflection smallest offset that occurs when drift angle is the thin slice wedge of θ w by light or light beam can draw with formula θ d=(n-1) θ w is approximate, and wherein n is a reflectance factor.Prism " magnifying power " (Δ) is measured by prismoptric, determines prismoptric according to the amount of whenever leaving 1 centimetre of skew of 1 meter distance generation of prism, like this, and Δ=100tan (θ d)
Two thin wedges by will having identical magnifying power (etc. deviation) are near combination, and make its around with the axis independent rotation of the normal almost parallel of their adjacently situated surfaces, just can make the laser beam B of passing two thin slice wedge bound fractions around the zero deflection beam channel, in narrow bullet, control along all directions.The radius of curvature of this narrow bullet is approximately θ d.In to the wedge process, drift angle is controlled in the extremely strict permissible variation scope, owing to decompose coefficient (melt-to-melt index) permissible variation that decomposes again, the angle of deviation (function of wavelength) is limited to atomic little amount.
The supposition vertical with vertical surface according to input beam limits misalignment angle, input angle difference, deviation just has difference certainly, the misalignment angle when determining the identical but wavelength shift of input direction, and computing formula is: θ d=arcsin (n sin θ w)-θ w '.
Wherein θ d is a misalignment angle, and θ w is the wedge angle, and n then is the typical coefficient of certain wavelength.The optics wedge can obtain with multiple material, for example synthetic fused silica, and optics wedge-shape and size also can be different.
Control device 20 (Figure 1A) is equipped with LCD display 24 (Fig. 2) and the controlling organization that is beneficial to use, and they constantly inform the state of weapon that the user uses, and sends instruction to the user continuously simultaneously in alignment procedure.Control device 20 is fixed in the transition shell capping 18.When transition shell capping 18 is shown in an open position, can read LCD display 24 at an easy rate.As previously discussed, control device 20 provides whole control operations, and all activities of monitoring Optical devices and adjustment head unit 56 and 64.Have combination 4 * 20LCD display 24 user interface is housed.Each key function below is described:
(a) adjusting key (26): after the soldier is with weapon aiming tool aiming Optical devices target graticule, start this key by this soldier.
(b) proceed key (28): want any moment of the instruction carrying out next alignment step or wonder demonstration the soldier, just can press this key.
(c) block key (30): during alignment system is tentatively determined, press this key, so that check its ready state.
(d) circuit and instrument are arranged memory (D1D LEADN) key (32): be transformed on the laser small arms transmitter device 12 with the test circuit and the instrument layout of this key with alignment system, so that check each translation function controller.Use this key to choose wantonly, promptly available can, only when certain requires, just use, for example, the laser small arms transmitter of belt bracket weapon can be accepted other circuit and instrument and arrange.
(e) weapon options button (34): this key uses with two band arrow keys 36 and 38, is used to select the type (M16A2, M2, M240 etc.) that will harmonize weapon.This selects to determine that much transmitting powers and which kind of coding will be by the alignment system verifications.
(f) arrow mark key (36 and 38): these two keys are used for selecting the type of different weapons.
Aiming anchor clamps 48 (Figure 1B) are a kind of firm mechanisms, be used at the fixing weapon 14 and aim at of alignment procedure with it, it allows the soldier to use any mark deviation of taking aim at that produces because of its method of sight to carry out boresight, and eliminating any weapon that leaves aiming point floats, anchor clamps 48 are fixed on the sliding rail 40, sliding rail 40 can indentation transition package header parts 42 in, so that admit the weapon of different length, aiming anchor clamps 48 have the elevation angle and orientation adjustment knob, can allow soldier's its weapon aiming tool that takes accurate aim, the video of the graticule 54 that aims at the mark.The gun barrel 44 of weapon leans against on the weapon support 46 that is positioned at transition shell 16, and transition shell 46 is installed on the transition package header parts 42.
The critical piece combination of alignment system 10 is installed on the transition shell 16, firm and stable environment in transportation and operating process is provided like this.Shell 16 also can sunshade and is avoided windy influence, so that carry out alignment procedure according to any desired condition.Base component 42 is fixed on the shell bottom surface Optical devices 56, weapon support 46, and the aiming anchor clamps track 40 and linking to each other of sliding for the battery pack (not shown) of alignment system energy supply.Alignment system is housed in the base component 42, and control device 20 is installed on the inboard of protecgulum 18A.
Fig. 8 is the calcspar of control device 20 optical output powers and the correct checking circuit of encoding, and with serial data bus 124 coding circuit 122 and a microcomputer (not shown) is linked.The megabit amplifier 126 that is arranged in laser beam passway is to coded electronic instrument output signal.
Below having described according to laser small arms transmitter of the present invention and with alignment system makes it carry out self-adjusting preferred embodiment.Clearly, for those of ordinary skill in the art, can change on arrangement of components and details for the present invention, therefore, protection scope of the present invention can only limit according to claims.
Claims (20)
1. generating laser that is installed in simulated gunnery live telecast on the small arms is characterized in that comprising:
Casing assembly with front end, described front end have a form;
One is installed in the laser diode that is used to launch the laser beam that passes described form in the described casing assembly;
One is installed in the described casing assembly and the power circuit that links to each other with described laser diode, is used to described laser diode energy supply so that make described laser diode emission laser beam; Be fixed on first and second optics wedge between described laser diode and the described form; Support the device of described first and second optics wedge, be used to make described first and second optics wedge to make independent rotation so that control described laser beam around a common light axis; And the transmission device that links to each other with described optics wedge bracing or strutting arrangement, described optics wedge bracing or strutting arrangement has the part that runs through described casing assembly, is used for being connected with described adjustment head.
2. generating laser according to claim 1, wherein said optics wedge have the basic deviation that equates.
3. generating laser according to claim 1, wherein said each optics wedge all have with the first surface of common light axis normal and with respect to the angled second surface that stretches out of described common light axis.
4. generating laser according to claim 3, wherein said first and second optics wedge supports and close contact with their first vertical surface.
5. generating laser according to claim 1, the wherein said device that is used to support first and second optics wedge comprises first and second spur gear, each spur gear is around a corresponding optics wedge.
6. generating laser according to claim 5, wherein said transmission device comprises first and second adjustment axle and is fixed on corresponding one adjusts first and second pinion that is used to engage corresponding spur gear on the axle, described adjustment axle has the end, and this end is passed the hole and the described adjustment head that are positioned at described casing assembly rear end and is in transmission connection.
7. generating laser according to claim 6 comprises a flange that stretches out from the casing assembly adjacent with described hole, be used to protect the end of the adjustment axle that passes.
8. generating laser according to claim 1, the shooting light-emitting diode display that wherein said casing assembly rear end has second form and is installed in the described second form back.
9. generating laser according to claim 1 also comprises a sensor that is used to survey the empty emission.
10. generating laser according to claim 1 comprises that also one links to each other with described power circuit and can order about action so that the induction change-over switch of excitation laser diode by the induction coil in the described head of harmonizing.
11. a generating laser that is installed in simulated gunnery live telecast on the small arms is characterized in that comprising:
Casing assembly with front end, this front end has first form;
One is installed in the laser diode that is used to launch the laser beam that passes described first form in the described casing assembly;
One is installed in the described casing assembly and the power circuit that links to each other with described laser instrument, is used to described laser instrument energy supply, so that make laser instrument launch laser beam;
Be used to control the drive unit of described laser beam;
The device that is used for transmission control device; And
One is connected on the described power circuit and orders about action so that give the induction change-over switch of described laser instrument energy supply by the induction coil that is positioned at the adjustment head that is installed on the described casing assembly.
12. according to claim 11 described generating laser, the wherein said device that is used to control laser beam comprises first and second optics wedge between the described laser instrument and first form, also comprise being used to support described first and second optics wedge device, so that make described first and second optics wedge make independent rotation around a common axis line with described transmission device.
Be installed in and be positioned at described casing assembly but 13. generating laser according to claim 11, wherein said casing assembly have a rear end that has second form and one at the shooting light-emitting diode display of the described second form back.
14. generating laser according to claim 11, wherein said casing assembly comprise a rectangular hollow case, the rear end of this casing assembly is a removable closure assemblies.
15. generating laser according to claim 12, each the optics wedge in wherein said two optics wedges all have one with the first surface of common light axis normal and one with respect to the angled second surface that stretches out of common axis line.
16. generating laser according to claim 15, wherein said first and second optics wedge supports and close contact with their first vertical surface.
17. generating laser according to claim 12, the wherein said device that is used to support first and second optics wedge comprises first and second spur gear, and each spur gear is around a corresponding optics wedge.
18. generating laser according to claim 17, wherein said transmission device comprises first and second adjustment axle and is fixed on corresponding one adjusts first and second pinion that is used to mesh a corresponding spur gear on the axle, described adjustment axle has the end, and the rear end that casing assembly is passed in this end is used for being in transmission connection with described adjustment head.
19. according to 11 described generating lasers of claim, wherein said casing assembly front end comprises one second form, this generating laser also comprises a sensor after being installed in this second form, is used to survey blank firing.
20. a generating laser that is installed in simulated gunnery live telecast on the small arms is characterized in that comprising: a casing assembly, described casing assembly have with the front end of first form and second form with the rear end of the 3rd form;
One is installed in the laser diode that is used to launch the laser beam that passes described first form in the described casing assembly; One is installed in the described casing assembly and the power circuit that links to each other with laser diode, is used to described laser diode energy supply so that make the laser diode emission pass the laser beam of described first form; The action that links to each other with described power circuit and can be ordered about by the induction coil in the adjustment head that is installed on the described casing assembly is so that excite the induction change-over switch of described laser diode; A sensor that is installed in the casing assembly that is positioned at the described second form back and is used to survey blank firing; A shooting light-emitting diode display that is installed in the casing assembly that is positioned at described the 3rd form back is used to produce optical signalling, so that be excited to the described laser diode of described adjustment head indication; Be fixed on first and second optics wedge in the described casing assembly between described laser diode and described first form; Support the device of described first and second optics wedge, this bracing or strutting arrangement is used to make described first and second optics wedge to make independent rotation around a common light axis, so that control described laser beam; And with the adjacent transmission device of described optics wedge bracing or strutting arrangement, described optics wedge bracing or strutting arrangement has the part that runs through described casing assembly rear end, is used for being connected with described adjustment head.
Applications Claiming Priority (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US08/237,717 | 1994-04-29 | ||
| US08/237,717 US5410815A (en) | 1994-04-29 | 1994-04-29 | Automatic player identification small arms laser alignment system |
| US08/415,595 | 1995-04-03 | ||
| US08/415,595 US5476385A (en) | 1994-04-29 | 1995-04-03 | Laser small arms transmitter |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN1147299A true CN1147299A (en) | 1997-04-09 |
| CN1071016C CN1071016C (en) | 2001-09-12 |
Family
ID=26930952
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN95192856A Expired - Fee Related CN1071016C (en) | 1994-04-29 | 1995-04-28 | Laser small arms transmitter |
Country Status (14)
| Country | Link |
|---|---|
| EP (1) | EP0760084B1 (en) |
| JP (1) | JP3005694B2 (en) |
| CN (1) | CN1071016C (en) |
| AT (1) | ATE190715T1 (en) |
| AU (1) | AU682110B2 (en) |
| BR (1) | BR9507525A (en) |
| CA (1) | CA2188554C (en) |
| DE (1) | DE69515659D1 (en) |
| FI (1) | FI110284B (en) |
| MX (1) | MX9605216A (en) |
| NO (1) | NO312217B1 (en) |
| NZ (1) | NZ284974A (en) |
| PL (1) | PL176681B1 (en) |
| WO (1) | WO1995030124A1 (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102494556A (en) * | 2011-12-14 | 2012-06-13 | 中国人民解放军总参谋部第六十研究所 | Stable image transmitter |
| CN104635240A (en) * | 2010-05-11 | 2015-05-20 | 上海聚然智能科技有限公司 | Mixedly-using target transmitting system for radio radar and laser radar |
| CN105091663A (en) * | 2015-07-20 | 2015-11-25 | 中国人民解放军总参谋部第六十研究所 | Visible light auxiliary calibration type laser transmitter and calibration method thereof |
| CN109307936A (en) * | 2018-11-28 | 2019-02-05 | 湖北华中光电科技有限公司 | A kind of auxiliary device for accelerating astro tracker pointing velocity |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1998019128A1 (en) * | 1996-10-25 | 1998-05-07 | Mentrex Ag | Device for adapting a weapon for simulated firing |
| SE514050C2 (en) | 1999-03-10 | 2000-12-18 | Saab Training Systems Ab | A simulator created for simulation of firing and a method for firing a simulator mounted on a weapon |
| WO2021145804A1 (en) * | 2020-01-15 | 2021-07-22 | Saab Ab | Simulation system with alignment device for aligning simulation axis with line of sight for a small arms transmitter |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0057304A1 (en) * | 1981-02-04 | 1982-08-11 | El-Op Electro-Optics Industries Limited | A gun sighting and fire control system |
| US4488369A (en) * | 1983-05-25 | 1984-12-18 | Todd Van Note | Marksmanship training apparatus |
-
1995
- 1995-04-28 EP EP95917730A patent/EP0760084B1/en not_active Expired - Lifetime
- 1995-04-28 DE DE69515659T patent/DE69515659D1/en not_active Expired - Lifetime
- 1995-04-28 PL PL95317129A patent/PL176681B1/en not_active IP Right Cessation
- 1995-04-28 AU AU23678/95A patent/AU682110B2/en not_active Ceased
- 1995-04-28 WO PCT/US1995/005253 patent/WO1995030124A1/en not_active Application Discontinuation
- 1995-04-28 JP JP7528388A patent/JP3005694B2/en not_active Expired - Lifetime
- 1995-04-28 NZ NZ284974A patent/NZ284974A/en not_active IP Right Cessation
- 1995-04-28 MX MX9605216A patent/MX9605216A/en unknown
- 1995-04-28 AT AT95917730T patent/ATE190715T1/en not_active IP Right Cessation
- 1995-04-28 CN CN95192856A patent/CN1071016C/en not_active Expired - Fee Related
- 1995-04-28 CA CA002188554A patent/CA2188554C/en not_active Expired - Fee Related
- 1995-04-28 BR BR9507525A patent/BR9507525A/en not_active IP Right Cessation
-
1996
- 1996-10-28 NO NO19964571A patent/NO312217B1/en unknown
- 1996-10-28 FI FI964325A patent/FI110284B/en not_active IP Right Cessation
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104635240A (en) * | 2010-05-11 | 2015-05-20 | 上海聚然智能科技有限公司 | Mixedly-using target transmitting system for radio radar and laser radar |
| CN104635240B (en) * | 2010-05-11 | 2017-05-10 | 上海聚然智能科技有限公司 | Mixedly-using target transmitting system for electromagnetic wave radar and laser radar |
| CN102494556A (en) * | 2011-12-14 | 2012-06-13 | 中国人民解放军总参谋部第六十研究所 | Stable image transmitter |
| CN102494556B (en) * | 2011-12-14 | 2014-02-19 | 中国人民解放军总参谋部第六十研究所 | Stable image transmitter |
| CN105091663A (en) * | 2015-07-20 | 2015-11-25 | 中国人民解放军总参谋部第六十研究所 | Visible light auxiliary calibration type laser transmitter and calibration method thereof |
| CN109307936A (en) * | 2018-11-28 | 2019-02-05 | 湖北华中光电科技有限公司 | A kind of auxiliary device for accelerating astro tracker pointing velocity |
| CN109307936B (en) * | 2018-11-28 | 2020-11-20 | 湖北华中光电科技有限公司 | Accelerate auxiliary device of astronomical director speed of aiming |
Also Published As
| Publication number | Publication date |
|---|---|
| EP0760084B1 (en) | 2000-03-15 |
| AU682110B2 (en) | 1997-09-18 |
| FI964325A0 (en) | 1996-10-28 |
| CN1071016C (en) | 2001-09-12 |
| ATE190715T1 (en) | 2000-04-15 |
| MX9605216A (en) | 1997-12-31 |
| NZ284974A (en) | 1997-03-24 |
| EP0760084A1 (en) | 1997-03-05 |
| PL176681B1 (en) | 1999-07-30 |
| WO1995030124A1 (en) | 1995-11-09 |
| PL317129A1 (en) | 1997-03-17 |
| FI964325A (en) | 1996-12-23 |
| BR9507525A (en) | 1997-09-16 |
| CA2188554A1 (en) | 1995-11-09 |
| NO312217B1 (en) | 2002-04-08 |
| JP3005694B2 (en) | 2000-01-31 |
| NO964571L (en) | 1996-10-29 |
| CA2188554C (en) | 1999-09-21 |
| JPH09512625A (en) | 1997-12-16 |
| NO964571D0 (en) | 1996-10-28 |
| DE69515659D1 (en) | 2000-04-20 |
| FI110284B (en) | 2002-12-31 |
| AU2367895A (en) | 1995-11-29 |
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