Riflescopes are mounted to rifles to assist a shooter, or user, in aiming the rifle to hit a desired target. Riflescopes may include reticles, which are markings or other indicators that appear in the field of view over the image of target through the riflescope. Reticles may include horizontal and vertical crosshairs with a central intersection point that can be calibrated to coincide with the point of impact of a projectile from the rifle. This central aiming point of the reticle may be zeroed-in at a particular zero range distance and then adjusted for different ranges and conditions using elevation and windage turrets to make slight adjustments to its vertical and horizontal position relative to the rifle. In this way, the user may always use the central intersection point of the crosshairs to aim the riflescope, and thus, the rifle. However, making mechanical adjustments to these elevation and windage turrets takes time, which may be disadvantageous in the field where a desired target could move at any time. Additionally, there are detailed reference charts the user must reference or memorize to correctly adjust these elevation and windage turrets.
As an alternative to the fine mechanical adjustments of elevation and windage turrets, some reticles are printed or formed with set holdover points, to use as aiming points instead of the central point. These holdover points save the user time in not having to make mechanical adjustments to dials, but still include complex charts to consult or memorize, which can cost the user time in the field and may result in mistake.
Embodiments of the invention address these and other limitations of the prior art.
Systems
As shown in
As illustrated in
Additionally or alternatively, the ballistic aiming system 300 may include all of the digital reticle riflescope 110, the rangefinder 140, the device 120 running the ballistics solution application 130, and peripheral sensors that provide additional input information used in calculating the ballistics solution, as shown in
Zeroing-In
As shown in
Through the zeroing-in process, the riflescope 110, and thus, the optical axis 240, becomes locked into a set position relative to the rifle bore line 230. This set position between the riflescope line of sight 240 and the rifle bore line 230 may be exploited by using holdover points or aiming adjustment points displayed on the reticle or in the field of view of the riflescope 110 to cause the user to make adjustments θ to the angle and position of the rifle bore line 230, which results in corresponding changes to the initial line of fire 220 of the selected projectile.
The zero range may be one of the pieces of ballistic data entered into the device 120 running the ballistics solution application 130.
Ballistics
The ballistic trajectory 220 for the selected projectile will vary with environmental conditions, such as crosswind, pressure, temperature, density altitude, humidity, angle of incline, etc. Additionally, the ballistic trajectory 220 of a projectile from the rifle 115 will vary with the projectile characteristics, such as caliber, bullet weight, ballistic coefficient, muzzle velocity, etc. and/or with the barrel length and twist rate.
As shown in
At the zero range, the ballistic trajectory 220 and correlated bullet drop have already been calibrated during the zeroing-in process, so that the optical axis 240 intersects the ballistic trajectory 220 at the point of impact 225, as illustrated in
For given environmental conditions, selected projectile, and other user input information, the ballistics solution application 130 may compute a new ballistic trajectory 220 for the selected projectile. The ballistics solution application 130 may use stored drag curves, such as the G1, G7 curves mentioned above, and custom drag curves, empirically measured data tables, the ballistics information described above, and/or algorithms for the selected projectile to calculate the amount of vertical bullet drop at any range.
The ballistics solution application 130 may use the computed ballistic trajectory 220 to calculate a ballistics solution θ for a given range. The ballistics solution θ may be given in terms of the amount of angular adjustment that should be made to the rifle 115 to hit the target at the determined range. The ballistics solution θ may be a set of both an elevation angle γ and an azimuth angle φ, i.e., a horizontal component and a vertical component. The amount of adjustment in the ballistics solution θ may be given in minutes of angle (MOA), milliradian (mil or MRAD), Bullet Drop Compensation (BDC), etc.
Because zeroing-in the riflescope 110 to the rifle 115 results in the riflescope 110 and its optical axis 240 being set at a constant angle relative to the rifle bore line 230, any angular adjustment θ to the riflescope 110 will result in the same angular adjustment θ to the rifle.
The ballistics solution θ will vary depending on the range to the target. Alternatively, if no range is input, the ballistics solution θ may be given as a set of angular adjustment values θ100 . . . θn for a series of incremental ranges. For example, if the zero range was 100 yards, the ballistics solution θ could include an angular adjustment value θ100 of 0 mil for 100 yards, since the ballistic trajectory 220 should already coincide with the optical axis 240 at the point of impact 225 for the zero range, and another angular adjustment value θ200 of 0.62 mil for 200 yards, etc. In some embodiments, the user may choose how many and which yardage targets will be displayed on the digital reticle riflescope 110. For instance, the user may operate the ballistics solution application 130 to elect to show holdover indicators for 3 distances, 100, 300, and 500 yards. In some embodiments the user may choose up to 8 or 10 different yardages. In operation, in some embodiments, the ballistics solution application 130 calculates different ballistic solutions θ for each of the selected yardages, and sends them to the digital reticle riflescope as separate solutions, where they are stored on the riflescope 100. The riflescope then calculates or otherwise determines which holdover solutions to select, such as by illuminating particular LEDs, as described in detail below.
In addition to the zero range, the ballistics solution application 130 may store environmental conditions present during zeroing-in. For example, the ballistics solution application 130 may store multiple rifle 115 and projectile profiles, for different ammunition, zero ranges, etc. The ballistics solution application 130 may store user-entered data observed from previous engagements (DOPE) and other information that may be correlated with a particular rifle 115 and projectile profile combination. The ballistics solution application 130 may use some or all of user-entered information and/or data automatically received from peripheral sensors within the ballistic aiming system 300, as shown in
Rangefinder
The rangefinder 140 may be a laser rangefinder, such as the KILO2400 available from SIG SAUER of Newington, N.H., USA, or other rangefinder. The rangefinder 140 may include a built-in ballistics solution calculator for determining a ballistics solution θ based on the determined range to the target, the selected projectile, the selected rifle, and the environmental conditions. In other words, as described above and shown in
Additionally or alternatively, as shown in
Digital Reticle
As shown in
The digital reticle riflescope 110 includes a mechanical reticle 400 within its field of view, such as is shown in
The digital reticle 500 may include a series of holdover indicators, such as individually addressable LEDs, that are selectively lit by a processor within the digital reticle riflescope 110. For example, the digital reticle 500 may include 25-200 individually addressable LEDs located along the horizontal and vertical crosshairs 402 and 404 of the mechanical reticle 400, as illustrated in
The LEDs may be non-transmissive OLEDs arranged atop the mechanical horizontal and vertical crosshairs 402 and 404. The OLEDs may be around 40 for example, with about a 30 μm dot size. The dot pitch for the OLEDs may be 0.056 mm, for example, and may vary depending on the location along the horizontal and vertical crosshairs 402 and 404 of the mechanical reticle 400. The OLEDs may have a very thin cathode deposition layer with a transparency of under 5%, for example. Additionally or alternatively, the LEDs may be TOLEDs with 60% transmission. Advantageously, however, the LEDs need not be transparent nor transmissive due to their arrangement atop the horizontal and vertical crosshairs 402 and 404 of the mechanical reticle 400. This allows for cost savings and less expensive manufacture of the digital reticle 500. Embodiments of the invention may work with any appropriate indicator or lighting technology, and is not limited to any particular technology.
The LEDs may be arranged on or adjacent the containing structure of the mechanical reticle 400, which may be located in the first and/or second focal plane, for example, near the objective and/or ocular lens of the riflescope 110. To enable the user to view the LEDs when lit, the LEDs may be located on the side of the mechanical reticle 400 closer to the ocular lens and oriented to illuminate in the direction of the ocular lens along the optical axis, as shown in
In operation of the digital reticle, the holdover indicator LEDs are lit to provide aiming adjustment points for the user. The particular holdover indicators that are energized may be selected by a processor 112 located on or in communication with the digital reticle riflescope 110 (
The digital reticle riflescope 110 may receive a ballistics solution θ from the rangefinder 140 or the device 120 running the ballistics solution application 130. The ballistics solution θ may include an aiming adjustment in the form of MOA, mil, etc. for adjusting the holdover point vertically, to compensate for gravitational bullet drop, for example. The ballistics solution θ may also include an aiming adjustment in the form of MOA, mil, etc. for adjusting the holdover point horizontally, such as for wind correction. The processor 112 determines which holdover indicators are selected based at least in part on the ballistics solution θ. In other words, different ballistics solutions θ may cause the processor 112 to select different holdover indicators. The processor 112 may calculate and select which holdover indicator to energize based on the received ballistics solution. The processor 112 may determine that a particular solution falls between two discrete holdover indicators and perform a rounding function to select the closest one. As described below, the processor 112 may take into account a magnification setting of the digital reticle riflescope 110. The processor 112 may then cause the selected holdover indicator to changes state, such as by causing electric current to flow through one or more of the selected LEDs. Aiming with the proper holdover indicator allows the shooter to properly aim at a target without making adjustments to the windage or elevation turrets, saving time and increasing efficiency and accuracy.
As shown in
As shown in
The digital reticle riflescope 110 may selectively illuminate LEDs atop the mechanical reticle 400 based on the ballistics solution θ received and the magnification level of the digital reticle riflescope 110.
As shown in
The digital reticle 500 provides an advantage over Bullet Drop Compensator (BDC) reticles in that because the holdover points used in embodiments of the invention are dynamic, the user is not limited to only a few projectile types of similar caliber and bullet weight that match the subtension of the predefined holdover reticle markings. Rather, the digital reticle 500 may provide aiming adjustment points for any projectile types because the ballistic aiming system adapts which LEDs are illuminated based on the particular projectile profile selected or programmed. Additionally, the user need not make a custom reference chart for his rifle 115 and projectile profile, as is done with BDC reticles, because the digital reticle riflescope 110 will illuminate the exact aiming adjustment points to use for the selected profile. This feature of the digital reticle riflescope 110 enables it to be used across a variety of firearms, rather than the user having multiple riflescopes with differing BDC reticles matched to each firearm.
Magnification
In some embodiments, the digital reticle riflescope 110 may be a variable power riflescope with a second or rear focal plane reticle. The digital reticle riflescope 110 may further selectively illuminate LEDs based at least in part on the magnification power level of the riflescope 110. The magnification power level may be determined using an encoder, sensors, mechanical position indicators, etc. as the user increases or decreases the magnification power. In this way, even if the digital reticle 500 is in the second focal plane, it may dynamically display the ballistic solution θ as a function of the magnified target view over the mechanical reticle 400 that remains the same size throughout the magnification levels. In operation, the digital reticle riflescope 110 operates as described above, by receiving a ballistics solution θ and then calculating which holdover indicator should be illuminated. In embodiments of the invention that include magnification compensation, the processor 112 takes the present magnification setting into account when calculating which holdover indicator to illuminate. As described above, the magnification power level may be determined using an encoder or sensor, etc., and the determined power level is then communicated to the processor 112.
As shown in
Power Selector Ring
As shown in
The power selector ring 150 may include an encoder, a zoom sensor, or other method of determining the selected magnification power level for the riflescope 110 at any given time. The encoder may send a magnification signal to a processor within the riflescope 110. The magnification signal may include data about the selected and/or last magnification power level of the riflescope 110 and/or power selector ring 150. Based on the magnification signal, the processor may determine which LEDs to selectively illuminate on the digital reticle 500 to compensate for the new and/or changed magnification power level.
For example, as shown in
The power selector ring 150 may include an LED or other indicator 155 that is oriented to illuminate in the direction of the user, as shown in
Illustrative example embodiments of the technologies disclosed herein are provided below. An embodiment of the technologies may include any one ore more, and any combination of, the example embodiments described below.
Example 1 includes a reticle for an aiming device, comprising a plurality of holdover indicators on the reticle that may be individually selected; an input for receiving ballistics data; and a processor configured to, based at least in part on the received ballistics data, select one or more of the holdover indicators, and cause the selected holdover indicator or indicators to visibly change state on the reticle.
Example 2 includes aspects of Example 1, in which the ballistics data is received from a rangefinder, in which the input is also structured to receive range data, and in which the processor is configured to select the one or more of the holdover indicators based at least in part of the received ballistics data and received range data.
Example 3 includes aspects of Example 1, in which the ballistics data is received from a device running a ballistics computer application.
Example 4 includes aspects of Examples 1-3, in which the input is structured to receive additional data from one or more of the group consisting of: a wind sensor, an inclinometer, a Global Positioning System, a thermometer, an altimeter, a barometer, and a motion sensor, and in which the processor is configured to select the one or more of the holdover indicators based at least in part of the received ballistics data and the additional data.
Example 5 includes aspects of Examples 1-4, further including a primary crosshair having a vertical portion and a horizontal portion, and in which the plurality of holdover indicators are disposed only on one the vertical portion or the horizontal portion of the primary crosshair.
Example 6 includes aspects of Examples 1-5, further including a primary crosshair having a vertical portion and a horizontal portion, and in which the plurality of holdover indicators are disposed only on both of the vertical portion and the horizontal portion of the primary crosshair.
Example 7 includes aspects of Examples 1-6, further comprising a cant indicator that provides an indication of a degree of rotation of the reticle.
Example 8 includes aspects of Examples 1-7, in which the plurality of holdover indicators includes Light Emitting Diodes (LEDs), and in which the processor is configured to illuminate the selected LEDs.
Example 9 includes aspects of Examples 1-8, in which the plurality of holdover indicators are not visible when not illuminated.
Example 10 includes aspects of Examples 1-9, in which the input additionally receives magnification data of a riflescope supporting the reticle, and in which the processor is configured to select one or more of the holdover indicators based at least in part on the magnification data.
Example 11 includes a method for operating a reticle for an aiming device, the reticle including a plurality of holdover indicators that may be individually selected, the method comprising receiving ballistics data from a ballistics computing device; selecting one or more of the holdover indicators based at least in part on the ballistics data; and causing the selected holdover indicator or indicators to visibly change state on the reticle.
Example 12 includes aspects of Example 11, further comprising receiving range data from a rangefinder; and selecting the one or more of the holdover indicators based at least in part on the ballistics data and on the range data.
Example 13 includes aspects of Examples 11-12, further comprising receiving additional data from one or more of the group consisting of: a wind sensor, an inclinometer, a Global Positioning System, a thermometer, an altimeter, a barometer, and a motion sensor, and selecting the one or more of the holdover indicators based at least in part on the ballistics data and on the additional data.
Example 14 includes aspects of Examples 11-13, further comprising providing an indication of a degree of rotation of the reticle
Example 15 includes aspects of Examples 11-14, in which causing the selected holdover indicator or indicators to visibly change state on the reticle comprises illuminating at least one LED.
Example 16 includes an aiming system for a projectile launching device, including a reticle including a plurality of holdover indicators; a rangefinder for providing range data; a ballistics calculator for providing ballistics data; a receiver for receiving the range data and the ballistics data; and a processor configured to, based at least in part on the received ballistics data, select one or more of the holdover indicators; and cause the selected holdover indicator or indicators to visibly change state on the reticle
Example 17 includes aspects of Example 16, further comprising one or more selected from the group of: a wind sensor, an inclinometer, a Global Positioning System, a thermometer, an altimeter, a barometer, and a motion sensor.
Example 18 includes aspects of Examples 16-17, in which the reticle is supported by a riflescope having selectable magnification, in which the receiver is structured to additionally receive magnification information, and in which the processor is configured to select one or more of the holdover indicators based at least in part on the magnification information.
The disclosed aspects may be implemented, in some cases, in hardware, firmware, software, or any combination thereof. The disclosed aspects may also be implemented as instructions carried by or stored on one or more or computer-readable storage media, which may be read and executed by one or more processors. Such instructions may be referred to as a computer program product. Computer-readable media, as discussed herein, means any media that can be accessed by a computing device. By way of example, and not limitation, computer-readable media may comprise computer storage media and communication media.
Although the reticle described herein was described with reference to a digital reticle riflescope 110, it is not strictly necessary that the reticle be mounted in or associated with a scope, and may instead be mounted in or associated with another type of aiming device.
All described embodiments and features of the disclosed invention may be combined with each other in any arbitrary manner, except where as described to be exclusive or known to those of skill in the art as technically unable to be combined. The above description is meant to be read broadly, and in a non-limiting manner, and the invention is limited only by the scope of the claims below.
This application is a non-provisional of and claims benefit from U.S. Provisional Application No. 62/571,173, filed Oct. 11, 2017, titled “BALLISTIC AIMING SYSTEM WITH DIGITAL RETICLE,” the disclosure of which is incorporated herein by reference in its entirety.
Number | Name | Date | Kind |
---|---|---|---|
1107163 | Grauheding | Aug 1914 | A |
1127230 | Grauheding | Feb 1915 | A |
1190121 | Critchett | Jul 1916 | A |
1708389 | Karnes | Apr 1929 | A |
1724093 | Kauch et al. | Aug 1929 | A |
1803939 | Karnes | May 1931 | A |
1989697 | Knisley | Feb 1935 | A |
2154454 | Joyce | Apr 1939 | A |
2162723 | Karnes | Jun 1939 | A |
2171571 | Karnes | Sep 1939 | A |
2250179 | Brown | Jul 1941 | A |
2253948 | Brown | Aug 1941 | A |
2355920 | Marston | Aug 1944 | A |
2363523 | Greenblatt, Jr. et al. | Nov 1944 | A |
2372613 | Antonin | Mar 1945 | A |
2404302 | Land et al. | Jul 1946 | A |
2420252 | Land | May 1947 | A |
2433843 | Hammond et al. | Jan 1948 | A |
2450712 | Brown | Oct 1948 | A |
2455963 | Roed | Dec 1948 | A |
2464195 | Burley et al. | Mar 1949 | A |
2504168 | Rood | Apr 1950 | A |
2534225 | Brown | Dec 1950 | A |
2538253 | Emory et al. | Jan 1951 | A |
2586807 | Fowler | Feb 1952 | A |
2596522 | Bethke | May 1952 | A |
2609606 | Draper et al. | Sep 1952 | A |
2690014 | Draper et al. | Sep 1954 | A |
2734273 | Blindenbacher et al. | Feb 1956 | A |
2737652 | White et al. | Mar 1956 | A |
2806287 | Sullivan | Sep 1957 | A |
2811894 | Braker | Nov 1957 | A |
2878466 | Shank et al. | Mar 1959 | A |
2949816 | Weaver | Aug 1960 | A |
2963788 | Luboshez | Dec 1960 | A |
2964991 | Coeytaux et al. | Dec 1960 | A |
3059338 | Coeytaux | Oct 1962 | A |
3097432 | Shaw | Jul 1963 | A |
3121134 | Heinzel | Feb 1964 | A |
3169726 | Jackson | Feb 1965 | A |
3190003 | O'brien | Jun 1965 | A |
3199197 | Macleod et al. | Aug 1965 | A |
3286352 | Schray | Nov 1966 | A |
3340614 | Leatherwood | Sep 1967 | A |
3381380 | Thomas | May 1968 | A |
3383987 | Macmillan | May 1968 | A |
3392450 | Herter et al. | Jul 1968 | A |
3431652 | Leatherwood | Mar 1969 | A |
3492733 | Leatherwood | Feb 1970 | A |
3682552 | Hartman | Aug 1972 | A |
3744133 | Fukushima et al. | Jul 1973 | A |
3782822 | Spence | Jan 1974 | A |
3948587 | Rubbert | Apr 1976 | A |
4205916 | Vogl et al. | Jun 1980 | A |
4263719 | Murdoch | Apr 1981 | A |
4285137 | Jennie | Aug 1981 | A |
4312262 | Tye | Jan 1982 | A |
4403421 | Shepherd | Sep 1983 | A |
4497548 | Burris | Feb 1985 | A |
4531052 | Moore | Jul 1985 | A |
4561204 | Binion | Dec 1985 | A |
4584776 | Shepherd | Apr 1986 | A |
4618221 | Thomas | Oct 1986 | A |
4671165 | Heidmann et al. | Jun 1987 | A |
4720804 | Moore | Jan 1988 | A |
4743765 | Ekstrand | May 1988 | A |
4777352 | Moore | Oct 1988 | A |
4777861 | Lecuyer et al. | Oct 1988 | A |
4787739 | Gregory | Nov 1988 | A |
4806007 | Bindon | Feb 1989 | A |
4912853 | McDonnell et al. | Apr 1990 | A |
4945646 | Ekstrand | Aug 1990 | A |
4965439 | Moore | Oct 1990 | A |
5026158 | Golubic | Jun 1991 | A |
5068969 | Siebert | Dec 1991 | A |
5181323 | Cooper | Jan 1993 | A |
5355224 | Wallace | Oct 1994 | A |
5375072 | Cohen | Dec 1994 | A |
5413029 | Gent et al. | May 1995 | A |
5456157 | Lougheed et al. | Oct 1995 | A |
5491546 | Wascher et al. | Feb 1996 | A |
RE35409 | Moore | Dec 1996 | E |
5783825 | Wiese | Jul 1998 | A |
5822713 | Profeta | Oct 1998 | A |
5901452 | Clarkson | May 1999 | A |
5920995 | Sammut | Jul 1999 | A |
5973315 | Saldana et al. | Oct 1999 | A |
6032374 | Sammut | Mar 2000 | A |
6111692 | Sauter | Aug 2000 | A |
6247259 | Tsadka et al. | Jun 2001 | B1 |
6269581 | Groh | Aug 2001 | B1 |
6357158 | Smith, III | Mar 2002 | B1 |
6453595 | Sammut | Sep 2002 | B1 |
6516551 | Gaber | Feb 2003 | B2 |
6516699 | Sammut et al. | Feb 2003 | B2 |
6591537 | Smith | Jul 2003 | B2 |
6681512 | Sammut | Jan 2004 | B2 |
6729062 | Thomas et al. | May 2004 | B2 |
6802131 | Scholz et al. | Oct 2004 | B1 |
6886287 | Bell et al. | May 2005 | B1 |
7069684 | Smith, III | Jul 2006 | B2 |
7171775 | LaCorte | Feb 2007 | B1 |
7171776 | Staley, III | Feb 2007 | B2 |
7185455 | Zaderey | Mar 2007 | B2 |
7194838 | Smith, III | Mar 2007 | B2 |
D542879 | Zaderey | May 2007 | S |
7222452 | Smith, III | May 2007 | B2 |
7225578 | Tai | Jun 2007 | B2 |
7237355 | Smith, III | Jul 2007 | B2 |
7269920 | Staley, III | Sep 2007 | B2 |
7292262 | Towery et al. | Nov 2007 | B2 |
7296358 | Murphy et al. | Nov 2007 | B1 |
7325353 | Cole et al. | Feb 2008 | B2 |
7325354 | Grauslys et al. | Feb 2008 | B2 |
7328531 | Dietz | Feb 2008 | B2 |
7343707 | Smith, III | Mar 2008 | B2 |
7350329 | Bell et al. | Apr 2008 | B1 |
7386953 | Ball | Jun 2008 | B2 |
7421816 | Conescu | Sep 2008 | B2 |
7490430 | Staley, III | Feb 2009 | B2 |
7516571 | Scrogin et al. | Apr 2009 | B2 |
7530192 | Grauslys et al. | May 2009 | B2 |
7584570 | Smith | Sep 2009 | B2 |
7603804 | Zaderey et al. | Oct 2009 | B2 |
7624528 | Bell et al. | Dec 2009 | B1 |
7654029 | Peters et al. | Feb 2010 | B2 |
7658031 | Cross et al. | Feb 2010 | B2 |
7690145 | Peters et al. | Apr 2010 | B2 |
7703679 | Bennetts et al. | Apr 2010 | B1 |
7703719 | Bell et al. | Apr 2010 | B1 |
7705975 | Farris | Apr 2010 | B1 |
7738082 | Peters | Jun 2010 | B1 |
7748155 | Cole | Jul 2010 | B2 |
7764434 | Håkansson et al. | Jul 2010 | B2 |
7793456 | LaCorte | Sep 2010 | B1 |
7806331 | Windauer et al. | Oct 2010 | B2 |
7832137 | Sammut et al. | Nov 2010 | B2 |
7836626 | Shepherd | Nov 2010 | B2 |
7856750 | Sammut et al. | Dec 2010 | B2 |
7877886 | Hamilton | Feb 2011 | B1 |
7905046 | Smith, III | Mar 2011 | B2 |
7937878 | Sammut et al. | May 2011 | B2 |
8001714 | Davidson | Aug 2011 | B2 |
8006429 | Windauer | Aug 2011 | B2 |
8033464 | Windauer et al. | Oct 2011 | B2 |
8046951 | Peters et al. | Nov 2011 | B2 |
8051597 | D'Souza et al. | Nov 2011 | B1 |
8056281 | Staley, III | Nov 2011 | B2 |
8074394 | Lowrey | Dec 2011 | B2 |
8081298 | Cross | Dec 2011 | B1 |
8091268 | York | Jan 2012 | B2 |
8109029 | Sammut et al. | Feb 2012 | B1 |
8172139 | McDonald et al. | May 2012 | B1 |
8196828 | Kelly | Jun 2012 | B2 |
8201741 | Bennetts et al. | Jun 2012 | B2 |
8230635 | Sammut et al. | Jul 2012 | B2 |
8281995 | Bay | Oct 2012 | B2 |
8282493 | Román et al. | Oct 2012 | B2 |
8286384 | Zaderey et al. | Oct 2012 | B2 |
8314923 | York et al. | Nov 2012 | B2 |
8317100 | Windauer et al. | Nov 2012 | B2 |
8336776 | Horvath et al. | Dec 2012 | B2 |
8353454 | Sammut et al. | Jan 2013 | B2 |
8365455 | Davidson | Feb 2013 | B2 |
8375620 | Staley, III | Feb 2013 | B2 |
8408460 | Schneider et al. | Apr 2013 | B2 |
8414298 | D'Souza et al. | Apr 2013 | B2 |
8448372 | Peters et al. | May 2013 | B2 |
8453368 | Bockmon | Jun 2013 | B2 |
8468930 | Bell | Jun 2013 | B1 |
8500563 | Román et al. | Aug 2013 | B2 |
8516736 | Windauer | Aug 2013 | B2 |
8584944 | White et al. | Nov 2013 | B2 |
8608069 | Bay | Dec 2013 | B1 |
8656630 | Sammut | Feb 2014 | B2 |
8701330 | Tubb | Apr 2014 | B2 |
8705173 | Peters et al. | Apr 2014 | B2 |
8707608 | Sammut et al. | Apr 2014 | B2 |
D709588 | Silvers et al. | Jul 2014 | S |
8807430 | Millett | Aug 2014 | B2 |
8833655 | McCarty et al. | Sep 2014 | B2 |
8881981 | Millett | Nov 2014 | B2 |
8893423 | Tubb | Nov 2014 | B2 |
8893971 | Sammut et al. | Nov 2014 | B1 |
8905307 | Sammut et al. | Dec 2014 | B2 |
8910412 | Mikroulis | Dec 2014 | B2 |
8919647 | Chen et al. | Dec 2014 | B2 |
8959823 | Peters et al. | Feb 2015 | B2 |
8959824 | Sammut et al. | Feb 2015 | B2 |
8966806 | Sammut et al. | Mar 2015 | B2 |
8991702 | Sammut et al. | Mar 2015 | B1 |
9004358 | Bay | Apr 2015 | B2 |
9033232 | Bockmon | May 2015 | B2 |
9038307 | Silvers et al. | May 2015 | B2 |
9038901 | Paterson et al. | May 2015 | B2 |
9057587 | Roman et al. | Jun 2015 | B2 |
9068794 | Sammut | Jun 2015 | B1 |
9068795 | Roman et al. | Jun 2015 | B2 |
9074845 | Wiklund | Jul 2015 | B2 |
9091507 | Paterson et al. | Jul 2015 | B2 |
9110295 | Lupher et al. | Aug 2015 | B2 |
9115956 | Hakanson et al. | Aug 2015 | B2 |
9115958 | Crispin | Aug 2015 | B2 |
9121672 | Tubb | Sep 2015 | B2 |
9127907 | Lupher et al. | Sep 2015 | B2 |
9127909 | Ehrlich | Sep 2015 | B2 |
9127910 | Volfson | Sep 2015 | B2 |
9127911 | Varshneya et al. | Sep 2015 | B2 |
9140521 | Millett | Sep 2015 | B2 |
9151574 | Lowrey | Oct 2015 | B2 |
9157701 | Varshneya et al. | Oct 2015 | B2 |
9175927 | Tubb | Nov 2015 | B2 |
9194880 | Kremer | Nov 2015 | B2 |
9212868 | Roman et al. | Dec 2015 | B2 |
9239213 | Chen et al. | Jan 2016 | B2 |
9250035 | Sullivan et al. | Feb 2016 | B2 |
9250036 | Farca et al. | Feb 2016 | B2 |
9250038 | Sammut et al. | Feb 2016 | B2 |
9255771 | Sammut et al. | Feb 2016 | B2 |
9292034 | Windauer | Mar 2016 | B2 |
D753785 | Silvers et al. | Apr 2016 | S |
9310163 | Bay | Apr 2016 | B2 |
9310165 | Bell et al. | Apr 2016 | B2 |
9335120 | Roman et al. | May 2016 | B2 |
9335123 | Sammut | May 2016 | B2 |
9347742 | Varshneya et al. | May 2016 | B2 |
9395155 | Bockmon | Jul 2016 | B1 |
9429653 | Volfson | Aug 2016 | B2 |
9429745 | Brumfield | Aug 2016 | B2 |
9435610 | Silvers et al. | Sep 2016 | B2 |
9459077 | Sammut et al. | Oct 2016 | B2 |
9464871 | Bay | Oct 2016 | B2 |
9466120 | Maryfield et al. | Oct 2016 | B2 |
9482488 | Moyle | Nov 2016 | B2 |
9482489 | Peters et al. | Nov 2016 | B2 |
9482516 | McCarthy et al. | Nov 2016 | B2 |
9500444 | Sammut et al. | Nov 2016 | B2 |
9518804 | Hamilton | Dec 2016 | B2 |
9557142 | Tubb | Jan 2017 | B2 |
9568277 | Crispin | Feb 2017 | B2 |
9568279 | Maryfield et al. | Feb 2017 | B2 |
9574849 | Hakanson et al. | Feb 2017 | B2 |
9574850 | Sammut et al. | Feb 2017 | B2 |
9581415 | Tubb | Feb 2017 | B2 |
9593907 | Regan et al. | Mar 2017 | B2 |
9612086 | Sammut et al. | Apr 2017 | B2 |
9651338 | Theisinger | May 2017 | B2 |
9665120 | Windauer | May 2017 | B2 |
9678099 | Maryfield et al. | Jun 2017 | B2 |
9678208 | Volfson | Jun 2017 | B2 |
9689643 | Farca et al. | Jun 2017 | B2 |
20050241207 | Staley, III | Nov 2005 | A1 |
20050257414 | Zaderey et al. | Nov 2005 | A1 |
20070097351 | York et al. | May 2007 | A1 |
20070137088 | Peters | Jun 2007 | A1 |
20070144052 | Smith, III | Jun 2007 | A1 |
20080098640 | Sammut et al. | May 2008 | A1 |
20090183417 | Smith, III | Jul 2009 | A1 |
20090199451 | Zaderey et al. | Aug 2009 | A1 |
20090199453 | Cross et al. | Aug 2009 | A1 |
20110021293 | York | Jan 2011 | A1 |
20110271577 | Davidson | Nov 2011 | A1 |
20110296733 | York | Dec 2011 | A1 |
20120132709 | Lowrey | May 2012 | A1 |
20120145785 | Scrogin et al. | Jun 2012 | A1 |
20120217300 | McDonald et al. | Aug 2012 | A1 |
20130014421 | Sammut et al. | Jan 2013 | A1 |
20140000146 | Davidson | Jan 2014 | A1 |
20140041277 | Hamilton | Feb 2014 | A1 |
20140063261 | Betensky et al. | Mar 2014 | A1 |
20140123534 | Hodnett | May 2014 | A1 |
20140166750 | Chen et al. | Jun 2014 | A1 |
20140166751 | Sammut et al. | Jun 2014 | A1 |
20140231014 | Davidson | Aug 2014 | A1 |
20140339307 | Sammut et al. | Nov 2014 | A1 |
20150153139 | Davidson | Jun 2015 | A1 |
20150276346 | Hamilton et al. | Oct 2015 | A1 |
20150323780 | Hamilton | Nov 2015 | A1 |
20160010950 | Sammut et al. | Jan 2016 | A1 |
20160025455 | Paterson et al. | Jan 2016 | A1 |
20160091282 | Baker et al. | Mar 2016 | A1 |
20160109210 | Lupher et al. | Apr 2016 | A1 |
20160138890 | Hofmann et al. | May 2016 | A1 |
20160163080 | Baker et al. | Jun 2016 | A1 |
20160169625 | Richards | Jun 2016 | A1 |
20160202021 | Roman et al. | Jul 2016 | A1 |
20160202960 | Le et al. | Jul 2016 | A1 |
20160252325 | Sammut et al. | Sep 2016 | A1 |
20160265880 | Maryfield et al. | Sep 2016 | A1 |
20160327367 | Porter et al. | Nov 2016 | A1 |
20160377379 | Roman et al. | Dec 2016 | A1 |
20160377380 | Sammut | Dec 2016 | A1 |
20170108376 | Maryfield et al. | Apr 2017 | A1 |
20170343317 | VanBecelaere | Nov 2017 | A1 |
20190072364 | VanBecelaere | Mar 2019 | A1 |
Number | Date | Country |
---|---|---|
2589391 | Feb 2010 | CA |
2773537 | Nov 2011 | CA |
2784280 | Nov 2011 | CA |
2743103 | Oct 2013 | CA |
2904485 | Aug 2014 | CA |
2847309 | Sep 2014 | CA |
2767420 | Dec 2014 | CA |
2660897 | Jun 2015 | CA |
2858582 | Jun 2015 | CA |
726699 | Oct 1942 | DE |
2000614 | Jul 1971 | DE |
2736598 | Feb 1978 | DE |
2652120 | May 1978 | DE |
3219940 | Dec 1983 | DE |
3622901 | Jan 1988 | DE |
19846655 | Apr 1999 | DE |
102004034267 | Feb 2006 | DE |
202005017276 | Mar 2006 | DE |
112007000314 | Jan 2009 | DE |
102008053948 | May 2009 | DE |
102013217240 | Mar 2014 | DE |
102013012257 | Jan 2015 | DE |
0359950 | May 1994 | EP |
0605290 | Jan 1997 | EP |
0844457 | May 1998 | EP |
1007995 | Jun 2000 | EP |
1057201 | Dec 2000 | EP |
1436568 | Jul 2004 | EP |
1443354 | Aug 2004 | EP |
1690060 | Aug 2006 | EP |
1725890 | Nov 2006 | EP |
1748273 | Jan 2007 | EP |
1801614 | Jun 2007 | EP |
1804017 | Jul 2007 | EP |
1943681 | Jul 2008 | EP |
1969302 | Sep 2008 | EP |
1723382 | Nov 2008 | EP |
2008049 | Dec 2008 | EP |
1723383 | Sep 2009 | EP |
2148165 | Jan 2010 | EP |
2276050 | Jan 2011 | EP |
2276050 | Jan 2011 | EP |
2339286 | Jun 2011 | EP |
2402704 | Jan 2012 | EP |
1516151 | Jun 2012 | EP |
2475950 | Jul 2012 | EP |
1817538 | Mar 2013 | EP |
2659218 | Nov 2013 | EP |
2513591 | Feb 2014 | EP |
2694908 | Feb 2014 | EP |
2739933 | Jun 2014 | EP |
1646837 | Aug 2014 | EP |
2778739 | Sep 2014 | EP |
2781875 | Sep 2014 | EP |
2802837 | Nov 2014 | EP |
2452151 | Mar 2015 | EP |
2943735 | Nov 2015 | EP |
2956733 | Dec 2015 | EP |
2676098 | Feb 2016 | EP |
1038149 | Apr 2016 | EP |
3036504 | Jun 2016 | EP |
3084338 | Oct 2016 | EP |
3102905 | Dec 2016 | EP |
2811252 | Jan 2017 | EP |
3111155 | Jan 2017 | EP |
2536995 | Oct 2017 | EP |
1388007 | Feb 1965 | FR |
2699658 | Jun 1994 | FR |
2700840 | Apr 1996 | FR |
2094950 | Sep 1982 | GB |
2420867 | Feb 2008 | GB |
S5536823 | Mar 1980 | JP |
I485630B | May 2015 | TW |
2006060007 | Jun 2006 | WO |
2015095614 | Jun 2015 | WO |
2015156899 | Oct 2015 | WO |
2016018478 | Feb 2016 | WO |
2016018478 | Mar 2016 | WO |
2016145122 | Sep 2016 | WO |
2016145123 | Sep 2016 | WO |
2016145124 | Sep 2016 | WO |
2016145124 | Nov 2016 | WO |
Number | Date | Country | |
---|---|---|---|
20190128643 A1 | May 2019 | US |
Number | Date | Country | |
---|---|---|---|
62571173 | Oct 2017 | US |