The field of the present disclosure relates generally to rotating adjustment mechanisms, and in particular, to a rotatable assembly for actuating an optical or electrical element of a sighting device, such as a riflescope, a telescope, or other aimed optical device.
Sighting devices such as riflescopes have long been used in conjunction with weapons and firearms, such as rifles, handguns, and crossbows, to allow a shooter to accurately aim at a selected target. Because bullet and arrow trajectory, wind conditions, and distance to the target can vary depending upon shooting conditions, quality sighting devices typically provide compensation for variations in these conditions by allowing a shooter to make incremental adjustments to the optical characteristics or the aiming of the sighting device relative to the weapon surface on which it is mounted. These adjustments are known as elevation and windage adjustments, and are typically accomplished by lateral movement of an adjusting member, such as a reticle located within the riflescope, as shown in U.S. Pat. No. 3,058,391 of Leupold, or movement of one or more lenses within a housing of the riflescope, as shown in U.S. Pat. Nos. 3,297,389 and 4,408,842 of Gibson, and U.S. Pat. No. 7,827,723 of Zaderey et al.
The shooter typically makes such adjustments using rotatable adjustment knobs to actuate the adjustable member of the sighting device. Rotatable knobs may also be used to adjust other features of riflescopes, binoculars, spotting scopes, or other suitable optical devices, such as parallax, focus, illumination brightness, or other suitable features. Although the rotatable knobs are described in relation to use with sighting devices, rotatable knobs may be used to adjust an adjustable portion of other devices, and may include volume control knobs, channel selection knobs, radio station selection knobs, and other suitable knobs.
Some sighting devices with rotatable knobs may include a locking device to prevent inadvertent rotation of the knob. For example, one known locking device for a rotatable knob includes two buttons on opposite sides of the knob that must be squeezed together to unlock the knob for rotation and thereby enable a desired adjustment. When the buttons are released, the knob is immediately locked at its current rotational position. One drawback of this locking device is its relative complexity and attendant expense of manufacture. The squeezing pressure required to unlock the knob for rotation may also make it more difficult to effect multiple fine rotation adjustments in the course of an aiming operation, when inadvertent rotation of the knob is less of a concern.
The '636 patent describes a locking adjustment device that addresses at least some of the above drawbacks. Very briefly, this locking adjustment device may include a button or other lock-release. The button or other lock-release is operably associated with a guide tab and manually depressible to urge guide tab out of a locked position and thereby allow a knob to be manually rotated about the turret axis away from the locked position. Although the '636 patent is incorporated by reference herein, some of the information contained in the '636 patent is also repeated in the next eight paragraphs, with reference to
Referring now to
Plunger 122 extends into main tube 102 and is constrained from rotating so that rotation of spindle 116 (into which plunger 122 is threaded) about the turret axis is translated into linear motion of plunger 122 along the turret axis, thereby adjusting a position of the adjustable element within main tube 102.
Spindle 116 includes a lower base portion 134 and an upper neck portion 136, which may be is smaller in diameter than lower base portion 134. Retaining ring 114 surrounds spindle 116 and retains spindle 116 against seat 106 of the riflescope 138. Retaining ring 114 includes exterior threads 112 sized to mesh with threads 110 on bore 108. Thus, spindle 116 is captured against main tube 102 and allowed to rotate about the turret axis, but is constrained from traveling along the turret axis by retaining ring 114, which is threaded into bore 108 of main tube 102. Retaining ring 114 includes a pair of blind bores 142 sized to fit a spanner wrench for threading and tightening retaining ring 114 onto spindle 116 or into bore 108, or both.
The locking adjustment device may include a click mechanism 146 to provide tactile and/or audible feedback to the user when a knob 174 is rotated. Click mechanism 146 may include a click ring 148 interposed between a shoulder of the lower base portion 134 of spindle 116 and retaining ring 114. Click ring 148 includes a grooved surface 152 facing spindle 116. Grooved surface 152 includes regularly spaced apart features, which may include splines or a series of evenly spaced vertical grooves or ridges. Other engagement features may include a series of detents, indentations, apertures, or other suitable features. Click mechanism 146 further includes a click pin 154 with a ramped surface 156 configured to engage the regularly spaced apart features of grooved surface 152. Click pin 154 is housed within a bore 158 in spindle 116 that has an open end facing grooved surface 152. A spring 160, or other biasing element, urges click pin 154 to extend outwardly from within bore 158 and engage grooved surface 152 of click ring 148. In operation, rotational movement of knob 174 about the turret axis causes click pin 154 to move out of contact with one groove and into a neighboring groove, thereby producing a click that is either audible, tactile, or both. Each click may coincide with an adjustment amount to alert the user about the extent of an adjustment being made. Click mechanism 146 continues clicking as long as knob 174 is rotated.
Locking adjustment device may further include a guide ring 168 attached along a stepped portion of an upper necked portion 172 of retaining ring 114. Guide ring 168 may be press fit around retaining ring 114 such that it rests flush against stepped portion and upper necked portion 172. In some embodiments, guide ring 168 may be welded, threaded, or adhered by an adhesive substance to retaining ring 114. In other embodiments, guide ring 168 may be integrated with or formed in retaining ring 114 or main tube 102.
The locking adjustment device may include a knob 174 mountable over guide ring 168 and spindle 116 for rotation about the turret axis when locking adjustment device is installed on riflescope 138. Knob 174 may include a retaining cap and a dial. Retaining cap may include a cylindrical gripping surface that may be notched, fluted, knurled, or otherwise textured to provide a surface for the user to grip when manually rotating knob 174. Dial may be supplied with a fine scale composed of parallel longitudinal indicia spaced apart around the circumference of dial to facilitate fine adjustments. Retaining cap and dial may be fabricated as a single unitary part or may be formed from two separate components that are coupled together, such as via mating threads.
The knob 174 may include a threaded bore sized to receive a threaded set screw. It should be understood that any number of bores, with a corresponding number of set screws, may be provided on knob 174. The set screw may rigidly couple knob 174 to a collar 188 that is press-fit onto upper neck portion 136 of spindle 116 so that knob 174 and spindle 116 rotate together as a unit. In other embodiments (not shown), collar 188 may be omitted and knob 174 may be directly coupled to spindle 116 by set screws or otherwise. A tool, such as a hex key, can be used to tighten set screw such that set screw bears against collar 188. Similarly, the tool can be used to loosen a set screw so that knob 174 and/or dial can be rotated relative to spindle 116 about the turret axis or removed and replaced with a different knob 174, if desired. In other embodiments (not shown), knob 174 is coupled or releasably coupled to spindle 116 in a manner other than by set screws. The combination of collar 188 and set screws, in conjunction with a flanged portion on collar 188, help prevent knob 174 from lifting upward in a direction along the turret axis.
The knob 174 may include a button 194 and an indicator unit 196 for rotation therewith. Slot 144 is sized and dimensioned to slidably receive indicator unit 196 such that at least a portion of indicator unit 196 is visible on a top surface of knob 174. Button 194 is operably associated with a guide tab 198 and manually depressible to urge guide tab 198 out of a locked position and thereby allow knob 174 to be manually rotated about the turret axis away from the locked position.
The accompanying drawings, wherein like reference numerals represent like elements, are incorporated in and constitute a part of this specification and, together with the description, explain the advantages and principles of the presently disclosed technology.
With reference to the drawings, this section describes particular embodiments and their detailed construction and operation. Throughout the specification, reference to “one embodiment.” “an embodiment,” or “some embodiments” means that a particular described feature, structure, or characteristic may be included in at least one embodiment. Thus appearances of the phrases “in one embodiment.” “in an embodiment,” or “in some embodiments” in various places throughout this specification are not necessarily all referring to the same embodiment. Furthermore, the described features, structures, and characteristics may be combined in any suitable manner in one or more embodiments. In view of the disclosure herein, those skilled in the art will recognize that the various embodiments can be practiced without one or more of the specific details or with other methods, components, materials, or the like. In some instances, well-known structures, materials, or operations are not shown or not described in detail to avoid obscuring aspects of the embodiments.
Referring to
Mounted over the spindle assembly 216 is the adjustment assembly including the catch assembly 269 and the knob assembly 274 (in particular, the catch assembly 269 may be mounted onto the retaining ring 214 of the spindle assembly 216 whereas the knob assembly 274 may be mounted to the spindle 215 of the spindle assembly 216). The catch assembly 269 may include a ring 268 mountable onto the retaining ring 214 of the spindle assembly 216 (e.g., a ring opening of the ring 268 may receive an upper necked portion of the retaining ring 214 of the spindle assembly 216). In some embodiments, in addition to carrying the button 294 or other lock-release, the ring 268 may function as a guide ring-performing any of the functions as guide ring 168 (
One or more surfaces of the ring 268 may include recesses to mate with locking assembly components. For example, in this embodiment an outer surface of the ring 268 defines an opening 248 (e.g., an aperture) in which a button 294 or other lock-release is located. In this embodiment, the opening 248 is similar to the aperture defined by the knob 174 (
The knob assembly 274 may be similar in any respect to the rotatable knob 174 described in the '636 patent. For example, in some embodiments the knob assembly 274 may include a retaining cap and dial (e.g., similar to the retaining cap and dial described in the description of FIG. 1 of the '636 patent), which may be fabricated as a single unitary part or may be formed from two separate components that are coupled together, such as via mating threads.
The knob assembly 274 may include a threaded bore 284 for a set screw (not shown), similar to the corresponding threaded bore described in the '636 patent. The set screw (not shown) insertable in the threaded bore 284 may be tightened so that knob assembly 274 and the spindle assembly 216 rotate together as a unit, or loosened so that the knob assembly 274 can be rotated relative to the spindle assembly 216. However, the set screw is not required—in other embodiments any knob assembly described herein may include any toolless actuation device usable by an operator to control whether the knob assembly 274 and the spindle assembly 216 rotate together (or not). In other embodiments, a knob assembly may include any rotatable knob, now known or later developed.
When the adjustable assembly is mounted to a sighting device (e.g., the riflescope 238 in this embodiment), the knob assembly 274 is rotatable relative to the sighting device (in the unlocked state, e.g., when the button 294 is depressed in this embodiment). In contrast, when the adjustable assembly is mounted to a sighting device, the catch assembly 269 is not rotatable relative to the sighting device (e.g., is rotationally fixed relative to the sighting device). Given the fixed rotation position of the catch assembly 269 when the adjustable assembly is mounted to a sighting device, it should be appreciated that travel of the button 294 or other lock-release may be constrained to a linear path (e.g., the button 294 or other lock-release travels along a linear path to and away from the turret axis, but does not rotate with the knob assembly 274). In other words, a rotational position of the button 294 or other lock-release is fixed relative to the sighting device. A fixed rotation position for the button 294 or other lock-release may allow some sighting device operators to lock or unlock rotation of the knob assembly 274 more easily.
The riflescope 238 is shown with a windage adjustment turret 374 having a knob similar to the knob 174 (
In various embodiments, any spindle assembly or adjustment assembly described herein may include other components shown in
Referring now to
The guideway 502 (
In some embodiments, catch device 298 may be fixably attached (e.g., by press fit), or otherwise coupled to, the button 294 or other lock-release via the fastening portion 518 (e.g., tubular portion). A length of the fastening portion 518 (e.g., the tubular portion) of the catch device 298 may extend through a via defined at least in part by the top of the ring 268. Fastening portion 518 may be inserted into an opening 528 on button 294 having dimensions corresponding to fastening portion 518 and secured therein, such as by a press fit, using an adhesive, or the like. Alternatively, fastening portion 518 and opening 528 may both be threaded so that catch device 298 is threadably coupled to button 294 or other lock-release. In other embodiments, the catch device 298 and the button 294 or other lock-release may instead be formed as a single unitary piece.
A rear of the button 294 or other lock-release may define a pair of openings (not shown) to each receive a biasing element 232 (e.g., to receive a pair of springs). To unlock knob assembly 274, button 294 or other lock-release is depressed inwardly toward turret axis to urge catch member 524 out of a catch opening or recess (such as by a notch 506 defined by a bottom of the knob assembly 274—shown in
In the illustrated embodiment, the adjustment assembly is a single revolution adjustment assembly, so the ramp at the end of the first turn may act as a stop. In other embodiments in which an adjustment assembly is arranged to make more than one revolution (e.g., a second revolution), an additional curved slide surface similar to the second curved slide surface described in the '636 patent may be provided on the bottom of the knob assembly similar to the second slide surface of the top of the guide ring described in the '636 patent. Briefly, in such an embodiment, once a knob has completed a rotation around the turret axis, the catch device (e.g., guide tab) may automatically transition onto the ramped transition section (defined by the bottom surface of the knob assembly) and continue on second curved surface to accommodate a second rotation of the knob. Depending on the shape of the transition section, the user may or may not feel a minor stop, bump, or other tactile sensation when catch device transitions between the curved slide curve and the additional curved slide surface. The user can continue turning knob until catch device hits a stop along the second end of the additional curved slide surface. At that point, in some embodiments the stop blocks catch device from moving beyond the second end, thereby limiting further rotation of the knob in this direction. The knob may still be rotated in an opposite direction for further fine adjustment and/or to return the knob assembly to its home position where it automatically locks.
In the illustrated embodiment, the retaining ring 214 (
In other embodiments, any components described herein that rotate relative to each (or which do not rotate) may be fabricated as a single unitary structure. In another example of this, instead of providing a separable guide ring 268, in various embodiments guide ring features (e.g., any features defined by an upper section of the guide ring 268) may be integrally formed on the sighting device (e.g., machine into a main tube of a riflescope).
As the button is depressed, the catch member travels inwardly toward the turret axis, which urges the catch member out of the slot defined by the knob assembly. In this state, the adjustment assembly can be rotated in the counterclockwise.
In some embodiments, any knob assembly described herein may be rotatable from a home position in more than one direction (e.g., in clockwise and counterclockwise directions), when unlocked. In other embodiments, it may be possible and practical to restrict rotation of any knob assembly described herein to rotation from the home position in a single direction, when unlocked.
Any assembly described herein may be formed from a set of parts including a single unitary part or more than one part. For sets containing more than one part, the parts may be fixably coupled together (e.g., press fit), releasably coupled together, or the like, or combinations thereof. As one example, as described earlier, a knob assembly may include a retaining cap and a dial coupled together, or may include a single unitary part (such as a knob having an upper section similar in any respect to the retaining cap and a lower section similar in any respect to the dial).
In the illustrated embodiment, the button or other lock-release is part of the adjustment assembly. In other embodiments, any of the principles described herein may be used to locate a button or other lock-release on some other part of a sighting device. For example, in some embodiments, a seat of the sighting device may define an opening to receive a fixed rotational position button or other lock-release. In various embodiments, any components of any catch assembly described herein may be part of a sighting device (e.g., located below the turret).
In still other embodiments, a button or other lock-release may be carried by the knob assembly. For example, in such an embodiment an axis of the button or other lock-release may coincide with the turret axis (co-axial axes). In such an embodiment, while the button or other lock-release may rotate about its axis, its lateral and longitudinal location relative to the sighting device does not change (e.g., the button or other lock-release has a fixed lateral and longitudinal location). In various embodiments, the button or other lock-release may be arranged to travel inwardly along a linear path.
It will be obvious to those having skill in the art that many changes may be made to the details of the above-described embodiments without departing from the underlying principles of the invention. The scope of the present invention should, therefore, be determined only by the following claims.
The subject matter described in this application is related to U.S. patent application Ser. No. 17/651,789, filed Feb. 18, 2022 and entitled “LOCKING ADJUSTMENT DEVICE,” which is a continuation of U.S. patent application filed Ser. No. 16/807,051, filed Mar. 2, 2020 (now U.S. Pat. No. 11,255,636) and entitled “LOCKING ADJUSTMENT DEVICE,” which is a continuation of U.S. patent application Ser. No. 14/923,158, filed Oct. 26, 2015 (now U.S. Pat. No. 10,578,399) and entitled “LOCKING ADJUSTMENT DEVICE,” which is a continuation of U.S. patent application Ser. No. 13/343,656 filed Jan. 4, 2012 (now U.S. Pat. No. 9,170,068) and entitled “LOCKING ADJUSTMENT DEVICE,” the disclosures of which are incorporated by reference herein in their entireties.