奥地利专利AT518877A4 Adjustment element for adjusting a sighting line of an optical sighting device, as well as a telesco

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专利摘要:
The invention relates to an adjusting element (10) for a telescopic sight, comprising a base (11), a rotary actuating element (12), a display element (14) having along its circumference at least one externally visible scale (15) with several scale markings (16). which are read in relation to a reference mark (17), wherein the display element (14) is used to display the current setting of the rotary actuating element (12). The individual scale markings (16) represent values of a main parameter (18), wherein at least two scale planes (24) are formed for displaying a first secondary parameter (20), which are arranged axially spaced from one another on the display element (14), wherein the same value of the main parameter (18) representing scale marks (16) of the individual scale levels (24) by a differential angle (25) are mutually shifted and by means of the individual scale levels (24), a first secondary parameter (20) is adjustable.
公开号:AT518877A4
申请号:T50157/2017
申请日:2017-02-27
公开日:2018-02-15
发明作者:Dr Zimmermann Andreas
申请人:Swarovski Optik Kg；
IPC主号:

专利说明:

Summary
The invention relates to an adjusting element (10) for a riflescope, with a base (11), a rotary actuating element (12), a display element (14), which has at least one scale (15) with a plurality of scale markings (16) visible from the outside along its circumference. which can be read in relation to a reference marking (17), the display element (14) being used to display the current setting of the rotary actuating element (12). The individual scale markings (16) represent values of a main parameter (18), at least two scale levels (24) being formed to display a first secondary parameter (20), which are arranged axially spaced apart on the display element (14), the same value of the main parameter (18) representing scale markings (16) of the individual scale levels (24) are shifted from one another by a difference angle (25) and a first secondary parameter (20) can be set by means of the individual scale levels (24).
Fig.2
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The invention relates to an adjusting element for adjusting a line of sight of an optical sighting device, in particular a telescopic sight, and a telescopic sight equipped with the adjusting element and a weapon equipped with the telescopic sight. The invention further relates to a method for adjusting a line of sight of an optical sighting device.
EP 2 848 887 A2 discloses a telescopic sight with a rotating tower, which has a rotary actuating element and a display element.
From AT 516 059 A4 a further riflescope with a rotating tower is known, which has a rotary actuating element and a display element.
Further riflescopes are known from EP 1 843 122 B1 and EP 2 684 005 B1.
In the riflescopes known from the prior art, the revolving tower is used to make a correction in the event of current shooting conditions which differ from the bullet conditions. The sight line, or line of sight, is tilted by an angle relative to the barrel of the rifle by means of the rotary actuating element. The rotary actuation element is coupled to a display element on which a scale is attached, as a result of which the current angle setting can be read. The resolution of the scale usually defines the smallest possible setting step. In addition, it is usually provided that the rotary actuating element is coupled to a latching ring, through which an acoustic or haptic feedback can be given to the user and, moreover, the rotary actuating element in its current position
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N2016 / 25400-AT-00 can be fixed against unwanted rotation. In most cases, the resolution of the locking ring is identical to the resolution of the scale. The rotation of the rotary actuating element by an incremental step of the locking ring, which is also called a click, causes the line of sight to tilt by a certain angle. The angle value is usually given in the form of an adjustment of the line of sight by a certain lateral displacement at a certain distance, such as 1cm / 100m or 0.5cm / 100m or in angular minutes, also minutes of angle or MOA, or a fraction of an MOA , Ballistic tables belonging to a rifle show how many clicks can be used to compensate for deviations from the bullet conditions.
The most important bullet conditions include the bullet distance, the air pressure prevailing during the bullet and the ambient temperature, the cartridge used (laboratory) including the nature of the projectile and the load, i.e. all factors relevant for external ballistics, such as the ballistic coefficient (BC) or the Projectile exit speed from the barrel (vO). Other entry conditions include the geographic location of the entry area and many other factors. Mostly, a target is only shot horizontally. The greatest impact of a deviation of the meeting point height brings with it a different distance from the bullet distance.
To compensate for the shifting of the meeting point due to a different shooting distance than the bullet distance, the shooter has to make corrections for a spot shot when aiming. In the case of a trained marksman and a shooting distance that does not deviate too much from the shooting range, these corrections can be carried out on the basis of empirical values by moving the turret by a few clicks or by moving the stopping point to the target. For example, an additional 5-10 clicks or 3-5 MOA for firing distances up to 200m are typically necessary at 100m range. For larger deviations in the distance, especially over 200m shooting distance at 100m shooting distance, pre-calculated simple ones
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Tables necessary, which e.g. be glued to the rifle stock for quick viewing.
If a second parameter value, such as the cross wind or a certain shot angle, for example when increasing the target to the horizontal, is also to be compensated for by taking the necessary correction into account based on the shooting distance, this usually leads to a problem, since empirical values apply to the additional correction value to be taken into account missing or corresponding and extensive ballistic tables are usually not at hand. Due to their complexity, extensive ballistics tables also have the disadvantage that they are difficult to read and therefore reading errors often occur in the field and under stress.
The object of the present invention was to overcome the disadvantages of the prior art and to provide an adjusting element for a riflescope or a riflescope equipped with the adjusting element, by means of which a second parameter can be easily taken into account and compensated.
This object is achieved by a device according to the claims.
According to the invention, an adjusting element for a telescopic sight is formed with a base, a rotary actuating element which can be rotated about an axis of rotation relative to the base, and a display element. The display element can be rotated about the axis of rotation relative to the base and has along its circumference at least one externally visible scale with a plurality of scale markings which can be read in relation to a reference mark, the display element being coupled to the rotary actuation element and the reference mark being coupled to the base is and the display element is used to display the current setting of the rotary actuator. The individual scale markings represent values of a main parameter, at least two scale levels being formed to display a secondary parameter value, which are arranged axially spaced apart on the display element, the scale markings of the individual representing the same value of the main parameter
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Scale levels are shifted from each other by a difference angle and a first secondary parameter can be set by the individual scale levels.
The adjustment element according to the invention has the advantage that with a variable secondary parameter value, a further parameter can be taken into account, which influences the main parameter value. This has advantages in particular if the necessary setting of the main parameter, for example for changing the shooting distance, is carried out by the user on the basis of empirical values or simple tables. The secondary parameter, for example a shooting angle, can be set easily and without arithmetic using the scale of the secondary parameter.
In particular, it is provided that the main parameter represents MOA or a fraction of MOA or a specific adjustment, such as 1 cm / 100 m. It is therefore a purely incremental angular adjustment of the line of sight to the barrel when setting the main parameter. In order to be able to take into account differences from the margin conditions, the necessary correction of the main parameter must be calculated or read from a corresponding table.
The first secondary parameter usually represents the deviation of the line of sight under certain different conditions from the entry conditions. For example, the first secondary parameter can be used to correct a deviation of the shot angle relative to the horizontal. This is an absolute value that applies to the same conditions as for standard bullet conditions, apart from the shot angle. In other words, the first secondary parameter already contains the information from a multidimensional ballistics table. If a certain weapon / laboratory combination was not shot under standard bullet conditions, but, for example, at a distance different from the standard bullet distance, it may happen that the values of the first secondary parameter are no longer correct. However, these deviations are often so small that they are negligible and the representation of the first secondary parameter remains valid even in this case.
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A standard bullet condition is a bullet condition that is typical for a certain weapon with a certain amount of workmanship in a certain environmental condition, such as standard ICAO atmosphere. In order to be able to correctly take the secondary parameters into account, it may be necessary for the display element to be matched to a specific weapon under its typical bullet conditions.
The aspects discussed for the first secondary parameter can also apply to the second secondary parameter.
In particular, it can be provided that the first secondary parameter is used to correct a deviation of the shot angle relative to the horizontal with the height tower. As an alternative to this, it can be provided, for example, that the first secondary parameter serves to correct a cross wind with the side tower.
It can further be provided that the second secondary parameter serves to correct a deviation of the shot angle relative to the horizontal.
Of course, all parameters that influence the trajectory of the projectile and differ from the main parameter can also be shown in the secondary parameters.
Furthermore, it can be expedient if the display element is arranged directly on the rotary actuation element. The advantage here is that the adjustment element can have a simple structure through this measure. For example, it can be provided that the rotary actuating element is designed in the form of a rotary wheel with a cylindrical outer surface and that the display element is printed on the cylindrical outer surface, for example. It can also be provided that the display element is scratched, engraved, etched onto the cylindrical outer surface or applied to the rotary actuating element by any other shape. Furthermore, it can also be provided that the display element is in the form of a film which is glued to the rotary actuation element.
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It can further be provided that the scale markings are designed in the form of curved curves which extend over the individual scale planes. The advantage here is that the curved curves, which extend over the individual scale planes, connect the individual point values to one another. The readability of the display element can thereby be improved.
In addition, it can be provided that the relative angle between two scale markings of a first scale level is different in size from a relative angle between two scale markings of a second scale level. By means of this measure, it can be taken into account, for example, that a change in the shot angle when the bullet is removed has a different effect than a change in the shot angle at a distance that deviates from the bullet distance.
Alternatively, it can be provided that the relative angles between two scale markings in different scale planes are the same. It can thereby be achieved that the curved curves run parallel to one another. Such a scale marking can thus also be suitable for a rotary actuating element which is designed for multiple revolutions. Such an embodiment variant can be particularly advantageous when the necessary adjustments in the individual scale levels are negligible, so that high accuracy can nevertheless be achieved.
Also advantageous is a configuration according to which it can be provided that axially parallel auxiliary lines are arranged on the display element, which extend at least some of the scale markings from the different scale planes to the reference marking. The advantage here is that reading the display element is made easier by this measure. In particular, this makes it easier to read scale markings from scale planes removed from the reference marking.
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According to a further development, it is possible for the individual scale planes to be characterized by axially spaced, circumferentially extending secondary scale markings. The advantage here is that the individual scale levels can be made visible by the secondary scale markings.
Furthermore, it can be expedient if the scale markings and the axially parallel auxiliary lines and / or the secondary scale markings have a different color and / or a different line width. The advantage here is that this measure makes the display element clear and easy to read.
In addition, it can be provided that the reference mark has a second scale and a second secondary parameter can thereby be set, the second scale of the reference mark being used for shifting the zero point on the basis of the second secondary parameter. The advantage here is that not only one secondary parameter but also a second secondary parameter can be set by this measure.
Furthermore, it can be provided that the resolution of the first secondary parameter is selected such that the difference angle between two scale markings from adjacent scale levels, which represent the same value of the main parameter, is the same size or by an integer multiplication as the resolution of the scale marking of the main parameter. The advantage here is that this measure means that the scale markings from different scale levels lie one above the other on an axis-parallel line, and this makes it easier to read the set scale value. In addition, it can be achieved in this way that the scale markings in each scale plane correspond to a latching position of the rotary actuating element. In order to achieve this, it may be necessary, for example, that unconventional values, such as a firing angle of 7.4 °, in the individual scale levels
14.8 °, etc. are shown.
According to a special design, it is possible for a transparent reading aid to be formed which is coupled to the base and is located outside
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N2016 / 25400-AT-00 of the display element extends over the individual scale levels of the display element, the reference marking being in the form of an axially parallel line applied to the reading aid. The advantage here is that such a reading aid makes it easy to read the individual values of the different scale levels.
According to an advantageous further development, it can be provided that the secondary scale markings of the individual scale levels are formed on the reading aid.
In particular, it can be advantageous if the reading aid is arranged on a rotating ring which can be rotated relative to the base, as a result of which the second secondary parameter can be set. This means that a second parameter value can be set even when using the reading aid.
It can further be provided that the display element is formed from an at least partially transparent material, on which the individual scale markings are applied, and that the reference mark is designed in the form of an axially parallel line arranged behind the display element, which extends over the individual scale levels of the display element.
In addition, it can be provided that the display element is interchangeable and that various display elements with different scale levels can be attached to the adjustment element. The advantage here is that this measure allows the display element to be adapted to the weapon used in each case with a certain amount of workmanship, and thus the telescopic sight can be used for different weapons or when changing the workout.
Furthermore, it can be provided that an at least partially transparent hollow cylinder is formed, on which the reference marking is formed, the hollow cylinder being coupled to the base and not rotatable relative to the base, and that with the rotary actuating element an inside the hollow cylinder
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N2016 / 25400-AT-00 horizontal display cylinder is rotatably coupled, on which the display element is arranged, wherein the display element of the display cylinder can be read together with the reference mark of the hollow cylinder.
Alternatively, it can be provided that an at least partially transparent hollow cylinder is formed, on which the display element is formed, the hollow cylinder being rotationally coupled to the rotary actuation element, and that a reference component is arranged inside the hollow cylinder, on which the reference mark is arranged, the Reference component is coupled to the base.
According to the invention, a rifle scope is provided, on which the adjustment element according to the invention is arranged, for example as a height tower for vertical or as a side tower for horizontal adjustment of the sight line.
Furthermore, a weapon, in particular a rifle, is provided, on which the telescopic sight according to the invention is arranged with the adjusting element according to the invention.
Furthermore, it can be expedient if the difference angle between the individual scale levels and / or the relative angle between two scale markings of a scale level is selected in accordance with the standard bullet conditions typical for the rifle.
According to the invention, a method for adjusting a line of sight of an optical sighting device, in particular a telescopic sight, is also provided by means of the adjusting element according to the invention. The process comprises the following process steps:
- Determining the current shooting conditions deviating from the shooting conditions, in particular the shooting distance;
- Determining a necessary correction value of a main parameter, in particular by reading from a table or a diagram or directly from a display element;
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- Rotation of the rotary actuator relative to the base to set a certain value of the main parameter necessary for correction, the current position of the rotary actuator can be read using the display element;
- determining the secondary parameter applicable under the current shooting conditions;
- Determining a necessary correction value of the main parameter according to the first secondary parameter by reading the correction value from the display element;
- Adjusting the rotational angle position of the rotary actuating element in order to correct the main parameter after the first secondary parameter.
Instead of reading the necessary correction value from a table or a diagram, experienced shooters can also know or estimate the necessary correction value by heart.
The step - "Adjusting the rotational angle position of the rotary actuating element in order to correct the main parameter after the first secondary parameter" can also be carried out simultaneously with the step - "Rotating the rotary actuating element relative to the base in order to set a specific value of the main parameter necessary for correction" , In addition, the end position of the rotary actuation element to be reached can be read from the display element and thus determined before the rotation of the rotary actuation element, taking into account both the main parameter and the first secondary parameter. Thus, both the main parameter and the first secondary parameter can be taken into account with only one adjustment process of the rotary actuating element.
Furthermore, it is also conceivable that, as a first method step, a weapon, on which the optical sighting device is arranged, is shot under certain shooting conditions.
A necessary correction value of the main parameter can also be determined by means of calculations using a ballistics program.
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For a better understanding of the invention, this will be explained in more detail with reference to the following figures.
Each show in a highly simplified, schematic representation:
Figure 1 shows an embodiment of a telescopic sight in a longitudinal section parallel to the line of sight axis.
2 shows a first exemplary embodiment of an adjusting element with the possibility of setting a main parameter and a first secondary parameter;
3 shows a second exemplary embodiment of the adjusting element with setting options for the main parameter, the first secondary parameter and a second secondary parameter;
4 shows a third exemplary embodiment of the adjusting element with auxiliary lines;
5 shows a fourth embodiment of the adjusting element with lines of the main scale marking which are curved to different degrees;
6 shows a fifth exemplary embodiment of the adjusting element with a transparent hollow cylinder;
7 shows a sixth embodiment of the adjusting element with a transparent hollow cylinder;
8 shows a seventh exemplary embodiment of the adjusting element with a reading aid;
9 shows an eighth embodiment of the adjusting element with an adjustable reading aid;
10 shows a first exemplary embodiment of a processing of the display element;
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Fig. 11 shows a second embodiment of a processing of the display element.
In the introduction, it should be noted that in the differently described embodiments, the same parts are provided with the same reference numerals or the same component names, and the disclosures contained in the entire description can be applied analogously to the same parts with the same reference numerals or the same component names. The location information selected in the description, e.g. above, below, to the side, etc., referring to the figure described and illustrated immediately, and if the position is changed, these are to be applied accordingly to the new position.
1 shows a highly schematic representation of a rifle scope 1. The rifle scope 1 is preferably used as a target device on a rifle. For this purpose, the rifle scope 1 is arranged on the rifle.
The riflescope 1 comprises an outer housing 2, in which a reversing system 5 is arranged between an objective 3 and an eyepiece 4. The optical elements of the reversing system 5, e.g. two putty lenses, sit in an inner housing 6. The reversing system 5 is together with the inner housing 6 as a structural unit inside the outer housing 2 on a bearing 7, e.g. Ball seat, rotatable or tiltable. This unit is tilted by an adjustment by means of an adjustment unit 8. This also changes the direction of a line of sight 9, which can be specifically adjusted by the adjusting unit 8.
To adjust the reversing system 5 within the outer housing 2, an adjusting element 10 acting on the reversing system 5, in particular an adjusting tower 10, is provided.
In alternative configurations, the adjustment tower 10 can also interact with other optical components within the outer housing 2. For example, the lens 3 can be adjustably mounted within the outer housing 2 in order to achieve an adjustment of the line of sight 9. The adjustment tower could also be used
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N2016 / 25400-AT-00 can be set up to move a reticle. In yet another embodiment variant, it is also conceivable for the complete outer housing 2 to be adjusted relative to the rifle to which the riflescope 1 is attached by means of the adjustment tower 10.
The riflescope 1 comprises at least one adjustment tower 10. This can be, for example, a height adjustment tower for the vertical adjustment of the sight line 9. In addition, a second adjustment tower 10 for horizontal adjustment of the sight line 9 can be formed on the telescopic sight 1.
FIG. 2 shows a schematic representation of a possible embodiment variant of the adjustment tower 10. As can be seen from FIG. 2, it can be provided that a rotary actuating element 12 is arranged on a base 11, which can be rotated relative to the base 11 with respect to an axis of rotation 13. An adjustment, in particular an angular tilt, of the line of sight 9 can be carried out by means of the rotary actuating element 12.
As can be seen from FIG. 2, it can be provided that a display element 14 is arranged directly on the rotary actuating element 12, by means of which the current position of the rotary actuating element 12 can be read off. The display element 14 comprises a scale 15 with a plurality of scale markings 16. The scale markings 16 can be read in relation to a reference mark 17. As can be seen from FIG. 2, it can be provided that the rotary actuating element 12 is designed in the form of a cylinder, the scale 15 or the scale markings 16 being printed directly on the circumferential surface of the circular cylinder. The base 11 can also be designed in the form of a circular cylinder, and the reference mark 17 can be printed or attached directly to the base 11.
The individual scale markings 16 represent values of a main parameter 18. The main parameter 18 can, for example, be expressed in multiples of 1 cm / 100 m or MOA. This means that a rotation of the rotary actuating element 12 by an incremental value of a scale marking 16 causes the line of sight 9 to be tilted by a certain angular amount.
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A relative angle 26 between two scale markings 16 arranged next to one another is also referred to as the resolution of the main parameter 18. Since a locking ring is usually coupled to the rotary actuating element 12, by means of which the user is given haptic and acoustic feedback when the next scale marking 16 is reached, adjustment by a scale marking 16 is also referred to as a “click”.
Different riflescopes 1 can have different resolutions for the angular adjustment of the line of sight 9. Common resolutions are, for example, that a click corresponds to 1cm / 100m, 0.5cm / 100m, 1 MOA, 1/2 MOA, 1/4 MOA or 1/8 MOA. Of course, other values such as 1/1000 rad etc. can also be used as the resolution.
Furthermore, it can be provided that the resolution of the main parameter 18 is identified in a main parameter label 19.
Furthermore, it is provided that not only the main parameter 18 is shown on the display element 14, but also that a first secondary parameter 20 is shown and can therefore be set. For this purpose, a first sub-scale 21 can be provided, which has a plurality of first sub-scale markings 22. In addition, a first sub-scale inscription 23 can be provided, by means of which the sub-parameter 20 can also be read.
The adjustability of the first secondary parameter 20 can in particular be achieved in that a plurality of scale levels 24 are formed, which are arranged axially spaced apart on the display element 14. The scale markings 16 of the individual scale levels 24 representing the same value of the main parameter 18 are shifted between two mutually adjacent scale levels 24 by a difference angle 25 to one another. This is an angle, since the rotary actuation element 12, on which the display element 14 is arranged, has a circular cylindrical surface. A parameter can be selected as the first secondary parameter 20, which requires only a slight variation or a small setting range. A possible one
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The value that would be suitable, for example, as the first secondary parameter 20 is the shot angle.
By designing the display element 14 according to the invention, a deviation from the main parameter 18 can be set in the first secondary parameter 20. As can be seen from FIG. 2, it can be provided that the scale markings 16 are designed in the form of curved curves which extend over the individual scale planes 24. This increases clarity and makes it easier to read. As can be seen in FIG. 2, the scale markings 16 can be arranged parallel to one another. In particular, it can be provided that the scale markings 16 are evenly distributed over the circumference of the rotary actuating element 12.
As an alternative to this, it can of course also be provided that the scale marking 16 is only shown in the form of points which are arranged in the individual scale levels 24.
Furthermore, it can be provided that the rotary actuating element 12 has a grip area 27, which is preferably spaced apart from the display element 14 and on which the rotary actuating element 12 can be gripped by the user.
FIG. 3 shows a further embodiment of the adjustment tower 10, which is possibly independent of its own, again using the same reference numerals or component designations for the same parts as in the previous FIG. 2. In order to avoid unnecessary repetition, reference is made to the detailed description in the previous FIG. 2.
As can be seen from FIG. 3, it can also be provided that the reference mark 17 does not comprise a single reference position, but that a second sub-scale 28 is formed on the base 11, which has a plurality of second sub-scale markings 29 and a second sub-scale label 30. A second secondary parameter 31 can thereby be set.
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The setting of the second secondary parameter 31 is achieved in that the second secondary scale markings 29 can be used to implement a zero point shift when reading the main parameter 18 or the main parameter 18 influenced by the first secondary parameter 20. A parameter can be selected as the second secondary parameter 31, which requires only a slight variation or a small setting range. For example, it is conceivable that the air pressure and therefore the visual height deviation compared to the bullet conditions or a cartridge different from the bullet conditions can be set as the second secondary parameter.
FIG. 4 shows a further embodiment of the adjustment tower 10, which is possibly independent of its own, again using the same reference numerals or component designations for the same parts as in the previous FIGS. 2 and 3. In order to avoid unnecessary repetition, reference is made to the detailed description in the preceding FIGS. 2 and 3.
As can be seen from FIG. 4, provision can be made for auxiliary lines 32 which are parallel to the axis and which extend the intersection points of the scale markings 16 from the different scale planes 24 to the reference mark 17. It makes sense here that the resolution of the first secondary parameter 20 is selected such that the difference angle 25 between two scale marks 16 from adjacent scale levels 24, which scale marks 16 represent the same value of the main parameter 18, is the same size or is an integer multiplication larger like the resolution of the scale marking 16 of the main parameter 18. In the present exemplary embodiment, the difference angle 25 and the relative angle 26 are the same size. As a result, the scale marking 16 representing the same value of the main parameter 18 is shifted exactly by one click from two adjacent scale levels 24. This not only increases the readability, but also contributes to the fact that each adjustable scale marking of the complete display element 14 coincides with a defined latching position.
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The reference marking 17 can of course also represent the second secondary parameter 31 in this and in all other exemplary embodiments, as in the exemplary embodiment according to FIG. 3.
In order to achieve a clear division of the auxiliary lines 32, as shown in FIG. 4, it may be necessary to select the values of the first secondary parameter 20 such that the shape described is obtained. As a result, odd or unusual values can also occur for the second secondary parameter 31.
FIG. 5 shows a further embodiment of the adjustment tower 10, which is possibly independent of its own, again using the same reference numerals or component designations for the same parts as in the preceding FIGS. 2 to 4. In order to avoid unnecessary repetition, reference is made to the detailed description in the preceding FIGS. 2 to 4 or reference.
As can be seen from FIG. 5, it can also be provided that the individual, curved curves of the scale markings 16 are not arranged running parallel to one another, but that the relative angle 26 between two adjacent scale markings 16 of a first scale plane 24 is different in size from the relative angle 26 between two adjacent scale markings 16 in a second scale plane 24. This takes into account, for example, that with a steeper firing angle, a firing distance different from the firing conditions only requires a slight adjustment of the tilt of the sight line 9 than would be necessary, for example, with a horizontal firing.
For the sake of clarity, only three scale markings 16 are shown in the present display element 14 according to FIG. 5. It goes without saying that, of course, this type of scale markings 16 can also be arranged distributed over the entire circumference, the curvature of the individual scale markings 16 becoming ever larger.
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FIG. 6 shows a further embodiment of the adjustment tower 10, which is possibly independent of its own, again using the same reference numerals or component designations for the same parts as in the preceding FIGS. 2 to 5. In order to avoid unnecessary repetitions, reference is made to the detailed description in the preceding FIGS. 2 to 5.
As can be seen from FIG. 6, it can be provided that a hollow cylinder 33 is formed which is transparent and which is not rotatably coupled to the base 11. The reference marking 17 can be printed or arranged on the surface of the hollow cylinder 33. Furthermore, the first secondary scale 21 with the corresponding first secondary scale markings 22 can be printed on the hollow cylinder 33. A display cylinder 34 can be arranged within the hollow cylinder 33, which is rotationally coupled to the rotary actuating element 12. The display element 14, in particular the scale markings 16, can be printed on the display cylinder 34.
This configuration makes it easy to read the individual scale levels 24.
The hollow cylinder 33 can be formed, for example, from a glass or a transparent plastic material.
Furthermore, it can be provided that the hollow cylinder 33 with the display element 14 arranged thereon can be rotated by a certain value relative to the base 11, as a result of which the reference marking 17 is shifted and the second secondary parameter 31 can also be set thereby.
FIG. 7 shows a further embodiment of the adjustment tower 10, which is possibly independent of its own, again using the same reference numerals or component designations for the same parts as in the preceding FIGS. 2 to 6. In order to avoid unnecessary repetitions, reference is made to the detailed description in the preceding FIGS. 2 to 6.
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The embodiment variant according to FIG. 7 is similar to the embodiment variant according to FIG.
6. In this exemplary embodiment, however, the display element 14, in particular the scale markings 16, is printed on the hollow cylinder 33, the hollow cylinder 33 being rotationally coupled to the rotary actuating element 12. The reference mark 17 is located on a reference component 35, which is non-rotatably coupled to the base 11. The individual scale levels 24 can also be marked on the reference component 35.
FIG. 8 shows a further embodiment of the adjustment tower 10, which is possibly independent of its own, again using the same reference numerals or component designations for the same parts as in the preceding FIGS. 2 to 7. In order to avoid unnecessary repetitions, reference is made to the detailed description in the preceding FIGS. 2 to 7.
The adjustment tower 10 is shown in a side view in FIG. 8a. 8b shows the adjustment tower 10 in the associated front view.
In the exemplary embodiment according to FIG. 8, a reading aid 36 is formed, which is arranged directly on the base 11. The reading aid 36 is preferably formed from a transparent material. The reference marking 17 or optionally also the first secondary scale markings 22 are arranged on the reading aid 36.
The reading aid 36 extends over the individual scale levels 24, which simplifies the reading of all scale levels 24.
FIG. 9 shows a further embodiment of the adjustment tower 10, which is possibly independent of its own, again using the same reference numerals or component designations for the same parts as in the preceding FIGS. 2 to 8. In order to avoid unnecessary repetitions, reference is made to the detailed description in the preceding FIGS. 2 to 8.
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The adjustment tower 10 is shown in a side view in FIG. 9a. 9b shows the adjustment tower 10 in the associated front view.
The embodiment according to FIG. 9 is configured similarly to the embodiment according to FIG. 8, wherein in this embodiment the reading aid 36 is not arranged directly on the base 11, but is arranged on a rotating ring 37 which can be rotated relative to the base 11. The second secondary parameter 31 can thereby be set.
To illustrate the scale marking according to the invention, the following example shows how the firing angle affects the correction for a spot shot necessary for different firing ranges. The calculations were carried out using commercially available ballistic software, such as QuickTARGET, under the following assumption: Standard ICAO atmosphere; Spot shot distance: 100m; Height of the line of sight above the barrel: 5cm; 1 click: 1 cm / 100m; Laboration: SAKO .308 WIN 141A Racehead, vO = 820 m / s, BC = 0.480
On the basis of this data, the necessary correction for different shooting angles, in the following for uphill strikes for a spot shot, can be calculated.
The display element 14 could in this case be designed, as shown in a development in FIG. 10.
The correction values in clicks for the above parameters may be necessary as shown in the table, whereby different shot angles are given in the first row of the table and different shot distances are given in the first column of the table:
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0 ° 10 ° 20 ° 30 ° 100m 0 0 0 -1 150m 3 2 2 1 200m 6 6 5 4 250m 10 10 9 7 300m 15 14 13 11 350m 20 19 18 16 400m 25 25 23 20 450m 31 30 28 25 500m 37 36 34 31
If the spot shot distance is used as the main parameter 18 and the shot angle as the first secondary parameter 20 according to Table 1, then four scale levels 24 result, which clearly visualize the scale markings 16 shown as curved lines in FIG. 10. The flat development of the cylindrical display element 14 is shown, the numbers, 1 ″,, 2 ″, ... ’5’ assigning the spot marks distances 100m, 200m, ... 500m associated with the scale markings. The dashed lines represent the corresponding intermediate distances 150m, 250m to 450m. The horizontal lines correspond to the secondary parameters 10 °, 20 ° and 30 ° shot angle. On the lowest scale level, the number of clicks is shown for better understanding, as they correspond to the actual incremental rotation of the tower. In order to correct the main parameter 18 in accordance with the first secondary parameter 20, the shooter follows the scale marking corresponding to the shooting distance along the different scale levels 24 until the scale level 24 corresponds to the current shooting angle and adjusts the rotary actuating element 12 accordingly.
10 shows a necessary correction for a shot at 450 m at an angle of 30 °, which correspond to the point in reference number 38. This is compared with a shot at 450m at an angle of 0 °, which corresponds to the point in reference number 39.
The curvature of the corresponding scale marking 16 thus results in a correction of 6 clicks by which the tower closes again for a spot shot
N2016 / 25400-AT-00 must be turned back. Conversely, it can also be seen from this example that, without this correction, a shooting shot of 1cm / 100m / click x 450m x 6 click = 27cm would have resulted without correction, which would no longer be tolerated from a hunting perspective. If the values of the main and secondary parameters to be corrected are not on or in the immediate vicinity of a scale marking 16, the shooter must visually interpolate the values.
Another example is intended to show how the scale marking 16 according to the invention can be applied to the side tower. As is well known among marksmen, a cross wind has a considerable influence on the hit position at the target. Experienced shooters take this into account through experience-based lateral compensation. Less experienced shooters often find it difficult to estimate the necessary correction, since both the distance to the target and the strength of the crosswind have to be taken into account. Assuming the laboratory parameters listed in Table 1, the influence of the cross wind can be calculated using a ballistic program.
The display element 14 could in this case be designed as shown in a development in FIG. 11.
The correction values in clicks for the above parameters may be necessary as shown in the table, with different wind speeds in the first row of the table and different shooting distances in the first column of the table:
2 m / s 5 m / s 8 m / s 100m 1 2 4 200m 2 5 8th 300m 3 8th 13 400m 4 11 18 500m 6 15 23
In this exemplary embodiment, the spot shot distance corresponds to the main parameter 18 and the cross wind represents the first secondary parameter 20, here three scale levels 24 for the first secondary parameter 20 with three under 23/42
N2016 / 25400-AT-00 different wind speeds have been taken into account. In this example, the three wind strengths were chosen such that a connection of the correction values for a certain distance results in a straight scale markings 16. Since a cross wind is possible from both sides, that is from the right or from the left to the firing direction, an adjustment via the side tower is usually provided symmetrically about a zero position.
This can be seen in FIG. 11 since the scale markings 16 are reflected around the zero position. Positive values mean that the rotary actuating element 12 must be rotated counterclockwise in this example, which corresponds to a tilting of the line of sight to the right and is necessary for compensation of cross winds from the right. Negative values correspond exactly to the opposite for compensation of cross winds from the left.
11, similar to FIG. 10, shows the development of the cylindrical display element 14, the scale markings 16 being based on the values from the table above. The numbers, 1 ‘,, 2’ ..... 5 ’correspond to the spot mark distances of 100 m, 200 m, ... 500 m belonging to the scale markings 16. The labeling of the three scale levels with, 2 ',, 5' and, 8 'corresponds to a cross wind of 2m / s, 5m / s and 8m / s. The actual click values are shown on the X axis for better understanding.
To compensate for cross winds from the right at 8 m / s at a shooting range of 500 m, reference numeral 40 - as can be seen in FIG. 11, a rotation of the rotary actuating element 12 of 23 clicks counter-clockwise is necessary.
In the event of a cross wind from the left at 5 m / s with a shooting distance of 350 m - reference number 41 - a twist of the rotary actuating element 12 of -8 clicks, ie clockwise, is necessary.
On the basis of these values, it can also be easily calculated that without a corresponding lateral correction, the target is 1 cm / 1 OOm / click x 500m x 23 click = 115cm in the case of a wind of 8m / s and 500m firing range or 1cm at 5m / s and 350m / 100m / click x 350m x 8 click = 28cm would have been missed.
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As can be seen particularly well from FIGS. 10 and 11, it is conceivable for all exemplary embodiments that the scale markings 16 or their distance from one another does not correspond to the clicks, therefore the resolution of the adjustment possibility of the rotary actuating element 12, but rather that values already predefined in the scale markings 16 are represented. Resolution of the clicks of the rotary actuating element 12 can therefore be specified in a separate label, which can be different from the main parameter label 19.
The exemplary embodiments show possible design variants, it being noted at this point that the invention is not limited to the specially illustrated design variants of the same, but rather also various combinations of the individual design variants with one another are possible and this variation possibility is based on the teaching of technical action through the present invention Ability of the specialist working in this technical field.
The scope of protection is determined by the claims. However, the description and drawings are to be used to interpret the claims. Individual features or combinations of features from the different exemplary embodiments shown and described can represent independent inventive solutions. The object on which the independent inventive solutions are based can be found in the description.
All information on value ranges in the objective description is to be understood so that it includes any and all sub-areas, e.g. the information 1 to 10 is to be understood so that all sub-areas, starting from the lower limit 1 and the upper limit 10, are included, i.e. all sections start with a lower limit of 1 or greater and end with an upper limit of 10 or less, e.g. 1 to 1.7, or 3.2 to 8.1, or
5.5 to 10.
For the sake of order, it should finally be pointed out that, for a better understanding of the structure, elements have sometimes been shown to scale and / or enlarged and / or reduced.
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N2016 / 25400 AT-00
LIST OF REFERENCE NUMBERS
Scope 28 second sub-scale outer housing 29 second subscale markie lens tion eyepiece 30 second sub scale description reversing system tung Inner housing 31 second secondary parameter camp 32 ledger line adjustment 33 hollow cylinder line of sight 34 display cylinders Verstellturm 35 reference component Base 36 viewing aid Rotary actuator 37 rotating ring axis of rotation 38 450m - 30 ° display element 39 450m - 0 ° scale 40 500m - 8m / s scale mark 41 350m - 5m / s
Reference marking main parameters Main parameter labeling of first secondary parameters first secondary scale first secondary scale marking first secondary scale labeling
Scale plane Difference angle Relative angle between two adjacent scale marks grip area
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权利要求:
Claims (22)
[1]
claims
1. adjusting element (10) for adjusting a line of sight (9) of an optical sighting device, in particular a telescopic sight (1), with a base (11), a rotary actuating element (12) which is relative to the base (11) about an axis of rotation (13) is rotatable, a display element (14) which is rotatable relative to the base (11) about the axis of rotation (13) and along its circumference has at least one scale (15) visible from the outside with a plurality of scale markings (16) which are related to a Reference mark (17) can be read, the display element (14) being coupled to the rotary actuation element (12) and the reference mark (17) being coupled to the base (11) and the display element (14) for displaying the current setting of the rotary actuation element (12 ), characterized in that the individual scale markings (16) represent values of a main parameter (18), with at least two scale levels () taking into account a first secondary parameter (20). 24) are formed, the scale markings (16) of the individual scale levels (24) representing the same value of the main parameter (18) being shifted by a difference angle (25) from one another and by means of the individual scale levels (24) of the main parameters (18) after a first Secondary parameters (20) can be corrected.
[2]
2. Adjustment tower according to claim 1, characterized in that the individual scale planes (24) on the display element (14) are arranged axially spaced apart.
[3]
3. Adjusting element according to claim 1 or 2, characterized in that the display element (14) is arranged directly on the rotary actuating element (12).
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N2016 / 25400 AT-00
[4]
4. Adjusting element according to one of the preceding claims, characterized in that the secondary parameters (20) and the main parameters (18) represent different parameters.
[5]
5. Adjusting element according to one of the preceding claims, characterized in that the scale markings (16) are designed in the form of continuous lines which extend over the individual scale planes (24) and can be rectilinear or curved.
[6]
6. Adjusting element according to one of the preceding claims, characterized in that the relative angle (26) between two scale markings (16) of a first scale plane (24) is different in size from a relative angle (26) between two scale markings (16) of a second scale plane (24) is.
[7]
7. Adjusting element according to one of the preceding claims, characterized in that axially parallel auxiliary lines (32) are arranged on the display element (14), which extend at least some of the scale markings (16) from the different scale planes (24) to the reference marking (17).
[8]
8. Adjusting element according to one of the preceding claims, characterized in that the individual scale planes (24) are characterized by axially spaced circumferentially extending secondary scale markings (22).
[9]
9. Adjusting element according to one of claims 5 to 8, characterized in that the scale markings (16) and the axially parallel auxiliary lines (32) and / or the secondary scale markings (22) have a different color and / or a different line width.
[10]
10. Adjusting element according to one of the preceding claims, characterized in that the reference marking (17) has a second secondary scale (28)
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N2016 / 25400-AT-00 and a second secondary parameter (31) can thereby be set, the second secondary scale (28) of the reference marking (17) being used for shifting the zero point on the basis (11) of the second secondary parameter (31).
[11]
11. Adjusting element according to one of the preceding claims, characterized in that the resolution of the first secondary parameter (20) is selected such that the difference angle (25) between two scale markings (16) from mutually adjacent scale planes (24), which scale markings (16) represent the same value of the main parameter (18), the same size or an integer multiplication greater than the relative angle (26) of the scale marking (16) of the main parameter (18).
[12]
12. Adjusting element according to one of the preceding claims, characterized in that a transparent reading aid (36) is formed, which is coupled to the base (11) and located outside the display element (14) over the individual scale levels (24) of the display element (14 ), the reference marking (17) being in the form of an axially parallel line applied to the reading aid (36).
[13]
13. Adjusting element according to claim 12, characterized in that the secondary scale markings (22) of the individual scale levels (24) are formed on the reading aid (36).
[14]
14. Adjusting element according to claim 12 or 13, characterized in that the reading aid (36) is arranged on a rotating ring (37) which can be rotated relative to the base (11), as a result of which the second secondary parameter (31) can be set.
[15]
15. Adjusting element according to one of claims 1 to 11, characterized in that the display element (14) is formed from an at least partially transparent material on which the individual scale markings (18, 20)
29/42
N2016 / 25400-AT-00 are applied and that the reference marking (17) is designed in the form of an axially parallel line arranged behind the display element (14), which extends across the individual scale levels (24) of the display element (14).
[16]
16. Adjusting element according to one of the preceding claims, characterized in that the display element (14) is interchangeable and different display elements (14) with differently pronounced scale levels (24) can be attached to the adjusting element (10).
[17]
17. Adjusting element according to one of the preceding claims, characterized in that an at least partially transparent hollow cylinder (33) is formed, on which the reference marking (17) is formed, the hollow cylinder (33) being coupled to the base (11) and not is rotatable relative to the latter, and that with the rotary actuating element (12) a display cylinder (34) lying within the hollow cylinder (33) is rotatably coupled, on which the display element (14) is arranged, the display element (14) of the display cylinder (34) can be read together with the reference mark (17) of the hollow cylinder (33).
[18]
18. Adjusting element according to one of claims 1 to 16, characterized in that an at least partially transparent hollow cylinder (33) is formed, on which the display element (14) is formed, the hollow cylinder (33) being rotationally coupled to the rotary actuating element (12) , and that a reference component (35), on which the reference mark (17) is arranged, is arranged within the hollow cylinder (33), the reference component (35) being coupled to the base (11).
[19]
19. Riflescope (1) with at least one adjusting element (10) for adjusting the line of sight by adjusting at least one optical component within the riflescope (1), characterized in that the adjusting element (10) is designed according to one of the preceding claims.
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N2016 / 25400 AT-00
[20]
20. Gun with a barrel, a barrel and a rifle scope (1) arranged on the barrel or barrel, characterized in that the rifle scope (1) is designed according to one of the preceding claims.
[21]
21. Weapon according to claim 20, characterized in that the difference angle (25) between the individual scale planes (24) and / or the relative angle (26) between two scale markings (16) of a scale plane (24) is selected in accordance with the standard bullet conditions typical for the rifle becomes.
[22]
22. A method for adjusting a line of sight of an optical sighting device, in particular a telescopic sight (1), by means of an adjusting element (10) according to one of claims 1 to 18, characterized in that the method comprises the following method steps:
- Determining the current shooting conditions deviating from the shooting conditions, in particular the shooting distance;
- Determining a necessary correction value of a main parameter (18), in particular by reading from a table or a diagram or directly from a display element (14);
- Rotating the rotary actuating element (12) relative to the base (11) in order to set a certain value of the main parameter (18) necessary for correction, the current position of the rotary actuating element (12) being able to be read using the display element (14);
- Determining the secondary parameter (20) that applies to the current shooting conditions;
- Setting a necessary correction value of the main parameter (18) after the first secondary parameter (20) by reading the correction value from the display element (14);
- Adjusting the rotational angle position of the rotary actuating element (12) in order to correct the main parameter (18) after the first secondary parameter (20).
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N2016 / 25400 AT-00
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2424

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同族专利:

公开号 | 公开日

EP3367044B1|2020-06-24|

AT518877B1|2018-02-15|

EP3367044A1|2018-08-29|

US20180252498A1|2018-09-06|

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引用文献:

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法律状态:

优先权:

申请号 | 申请日 | 专利标题

ATA50157/2017A|AT518877B1|2017-02-27|2017-02-27|Adjustment element for adjusting a sighting line of an optical sighting device, as well as a telescopic sight with the adjusting element and weapon with the telescopic sight, and method for adjusting the sighting line|ATA50157/2017A| AT518877B1|2017-02-27|2017-02-27|Adjustment element for adjusting a sighting line of an optical sighting device, as well as a telescopic sight with the adjusting element and weapon with the telescopic sight, and method for adjusting the sighting line|

EP18158750.2A| EP3367044B1|2017-02-27|2018-02-27|Adjusting element for adjusting a line of sight of an optical sighting device, and telescopic sight with the adjusting element and weapon with the telescopic sight, as well as method of positioning the line of sight|

US15/906,519| US11143490B2|2017-02-27|2018-02-27|Adjusting element for adjustment of a line of sight of an optical sighting mechanism, and telescopic sight with the adjusting element and weapon with the telescopic sight, and method for adjusting the line of sight|

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