The present disclosure generally relates to firearm bolts and, more particularly, to rotatable firearm bolts. Firearms including such bolts are also described.
The “Gatling gun” is a firearm that was originally developed in the mid-nineteenth century. In general, the Gatling gun is a multiple barrel firearm that includes a plurality of barrels (e.g., six). In operation, the Gatling gun fires projectiles in an automatic fashion as the plurality of barrels rotate in a circuit about an axis. As they rotate the barrels consecutively move to a single firing position that allows for the firing of a projectile. After a projectile is fired from one barrel, that barrel continues to rotate, bringing the next barrel to the firing position. Thus, each of the barrels fires only a portion of the projectiles that are shot by the firearm. Over time many improvements have been made to the original Gatling gun, advancing the design of the gun from a crank driven design to the design used in the modern M-134 “minigun.” Despite many improvements made over the years, the M-134 has retained the multiple rotating barrel design that is a hallmark of this type of firearm.
Like many firearms the M-134 utilizes cartridge ammunition. Cartridge ammunition generally includes a projectile (e.g., a bullet) that is mounted over an explosive charge. The bullet and charge are held together by a casing that includes an explosive primer. In many modern firearms the primer is designed to ignite in response to a force imparted from a firing pin, which may reside within a firearm bolt. Ignition of the primer is transferred to the charge, causing the charge to detonate and launch the bullet (e.g., through a barrel). In some cases, the bolt is also designed to eject spent cartridges from the firearm and chamber the next cartridge.
In firearms that include multiple rotating barrels such as the M-134, each barrel is typically associated with its own bolt. Such bolts often include a head and a body that is movable relative to the head. Common bolt designs that are used in the M-134 include the bolt described in U.S. Pat. No. 3,611,866 (hereinafter, the “GE bolt”) and the bolt described in U.S. Pat. No. 6,742,434 (hereinafter, the “Dillon bolt”). The structure and operation of the GE bolt and the Dillon bolt are described in detail in the '866 and '434 patents, the entire content of both of which are incorporated herein by reference. Since the operation of such bolts is essentially the same, a summary description of the construction and operation of only the Dillon bolt is provided herein in the interest of brevity.
In the Dillon bolt, the first and second cam assemblies are substantially identical but are located on opposite sides of the bolt. Each of the first and second cam assemblies is defined by a female helical cam slot formed in the bolt body 2 and a male helical cam arm formed by part of the bolt head 7. The first helical cam assembly is shown in
The first male helical cam arm 5 includes helical cam surfaces 14, 15, which interact with (e.g., slide against) corresponding helical cam surfaces 16, 17 of the first female helical cam slot 4, as shown in
In operation, six Dillon bolts are mounted to a respective one of six tracks in a rotor of a receiver of an M-134 via track slots 11 formed on either side of the bolt. Each track (and thus, each Dillon bolt) is associated with one of six rotating barrels of the firearm. To fire the M-134, each of the six barrels is rotated by a rotor in concert with its corresponding bolt. The bolts rotate and move towards and away from their respective barrel by the movement of a cam roller 10 within a helical path formed on the inside of the casing of the receiver. As the cam roller 10 travels along the helical path, the bolt acquires an ammunition cartridge (e.g., from an ammunition feeder such as a de-linker) and chambers the cartridge. Eventually the proximal end (not labeled) of the bolt head 7 abuts its corresponding barrel, such that the bolt head 7 and bolt body 2 are in an initial (pre-firing) position, but the helical path continues forward. As the cam roller 10 continues to move forward along the helical path, the bolt body 2 is compressed against the bolt head 7. This causes a compressive force to be exerted by the helical cam surfaces 16, 16′ of the female helical cam slots 4, 9 against the helical cam surfaces 14, 14′ of the male helical cam arms 5, 8. That compressive force causes the helical cam surfaces 16, 16′ of the first and second female cam slots 4, 9 to interact with the helical cam surfaces 14, 14′ of the male helical cam arms 5, 8. Such interaction causes the bolt head 7 to twist in a first direction relative to the bolt body 2 while simultaneously compressing the firing pin spring 6 and cocking the firing pin 3.
When the cam roller 10 reaches the forward most position of the helical path (i.e., the bolt assembly 1 is in the “firing position”) the firing pin spring 6 is released, causing the firing pin 3 to strike the primer of a cartridge that is chambered in the bolt. As noted above, the firing pin 3 is also coupled to the bolt head 7 by a release pin that moves within an L-shaped slot (shown in
Subsequently the cam roller 10 is moved backwards along the helical path. That movement causes a compression force to be exerted by helical cam surfaces 17, 17′ of the female came slots 4, 9 against the helical cam surfaces 15, 15′ of the male helical cam arms 5, 8. That compressive force causes the helical cam surfaces 17, 17′ of the female cam slots 4, 9 to interact with the helical cam surfaces 15, 15′ of the male helical cam arms 5, 8—causing the bolt head 2 to twist in a second direction relative to the bolt body 7 as the bolt head 2 is retracted away from the bolt head 7. Ultimately such interaction causes the bolt head 2 to realign with the bolt head 7 and causes the release pin to move back into the vertical leg of the L-shaped slot—resetting the bolt assembly 1 for another firing cycle.
Although it is functionally quite like the Dillon bolt, the GE bolt includes a single cam assembly formed by a single male cam arm on the bolt head and a single female cam slot in the bolt body. One issue with the GE bolt design is that rotation of the bolt head relative to the bolt body is caused by interaction of the single male cam arm and single female cam slot during both compression and retraction of the bolt assembly. As a result, asymmetrical loads are placed on the single cam assembly and, more specifically, at the point at which the male cam arm meets the rest of the cam head (hereinafter, the “neck” of the male cam arm). Over time such loads can fatigue and eventually break the male cam arm, resulting in a bolt failure. The Dillon bolt addressed that problem by utilizing two cam assemblies on opposite sides of the bolt as discussed above. The use of two cam assemblies balanced the load across the bolt assembly during use, resulting in fewer bolt failures than the GE bolt.
While the Dillon bolt did improve upon the GE bolt, as noted above the Dillon bolt utilizes two cam assemblies that each includes two pairs of helical cam surfaces. Specifically, the Dillon bolt includes a first cam assembly that includes a first pair of helical cam surfaces 14, 16 that interact as the bolt assembly is compressed from an initial position to a firing position, and a second pair of helical cam surfaces 15, 17 that interact as the bolt assembly is retracted from the firing position to the initial position. Likewise, the second cam assembly includes a first pair of helical cam surfaces 14′, 16′ that interact as the bolt assembly is compressed, and a second pair of helical cam surfaces 15′, 17′ that interact as the bolt assembly is retracted. Both cam assemblies also include a male cam arm that has a relatively thin neck. This is illustrated in
Interaction of surfaces 14, 16 and 14′, 16′ can impose a significant load on the neck of their respective male cam arm 5, 8 during compression of the bolt assembly 1 (i.e., movement between an initial and firing position). Likewise, interaction of surfaces 15, 17 and 15′ 17′ can impose a significant load on the neck of their respective male cam arm 5, 8 during retraction of the bolt assembly 1 (i.e., movement between the firing position and initial position). Thus, the neck of each of the male cam arms in the Dillon bolt may be subject to significant loads as the bolt is compressed and retracted during a firing cycle. Over time, such loads can lead to failure of one or both male cam arms 5, 8, potentially leading to failure of the entire bolt assembly. This issue may be exacerbated by the exceptionally high firing rate of rotatable firearms such as the M-134, which may be as high as 4,000-6,000 rounds per minute or more.
Thus, there remains a need in the art for a firearm bolt assembly that reduces or eliminates loads placed on weaker areas of the bolt, while remaining compatible with existing firearm designs such as the M-134.
Features and advantages of embodiments of the claimed subject matter will become apparent as the following Detailed Description proceeds, and upon reference to the Drawings, wherein like numerals depict like parts, and in which:
As noted previously the Dillon bolt improved upon the GE bolt in part through the inclusion of two cam assemblies on opposites sides of a firearm bolt assembly. However, the two cam assemblies in the Dillon bolt are each defined by a male cam arm and a female cam slot, both of which include two helical cam surfaces. Thus, in the Dillon bolt, each of the cam assemblies each include two pairs of cam surfaces—one pair that interact during compression of the bolt, and another pair that interact during retraction of the bolt. Due to the geometry of the cam assemblies in the Dillon bolt, loads generated during compression and retraction of the bolt during a firing cycle may be concentrated at the neck of each cam arm. Over time such loads can lead to the failure of one or both cam arms, and potentially to failure of the entire firearm bolt assembly. Thus, while the Dillon bolt has proven to be more durable than the GE bolt, there remains a need and desire in the art for firearm bolt assemblies that are even more durable than the Dillon bolt and yet remain compatible with existing firearm designs—particularly rotary firearm designs such as the M-134.
The present disclosure generally relates to firearm bolt assemblies that differ from the Dillon and GE bolts, yet remain compatible with existing firearm designs such as the M-134. As will be described in detail, the firearm bolt assemblies presented herein include a first side, a second side, a proximal end, and a distal end, wherein the first side is substantially opposite the second side. The firearm bolt assemblies further include a bolt body, a bolt that is movable relative to the bolt body, a first cam system, and a second cam system. The first cam system is defined by only a pair of single first complementary cam surfaces that are each proximate the first side of the firearm bolt assembly, wherein the bolt head comprises one of the pair of single first complementary cam surfaces, and the bolt body comprises another of the pair of single first complementary cam surfaces. The second cam system is defined by only a pair of single second complementary cam surfaces that are each proximate the second side of the firearm bolt assembly, wherein the bolt head comprises one of the pair of single second complementary cam surfaces, and the bold body comprises another of the pair of single second complementary cam surfaces.
In embodiments, the firearm bolt assemblies described herein can transition from an initial position to a firing position by compression of the bolt body towards to the proximal end of the bolt assembly, during which a predominant compression force is born by (e.g., born only by) the first cam system. In such embodiments the firearm bolt assemblies may transition from the firing position to the initial position by retraction of the bolt body away from the proximal end of the firearm bolt assembly, during which a predominant compression force is born by (e.g., born only by) the second cam system. In some embodiments, the predominant compression force during compression of the bolt body towards the proximal end is a pushing force that is directed towards the proximal end of the firearm bolt assembly. In contrast the predominant compression force during retraction of the bolt body away from the proximal end is a pulling force that is directed towards the distal end of the firearm bolt assembly.
In embodiments one of the pair of single first complementary cam surfaces is a first helical cam surface and the other of the pair of single first complementary cam surfaces is a second helical cam surface that is complementary to the first helical cam surface. When the firearm bolt assembly is moved from the initial position to the firing position, interaction of the first and second helical cam surfaces causes the bolt head to twist, relative to the bolt body, in a first direction about an axis extending through the bolt head and the bolt body. In such instances, one of the pair of single second complementary cam surfaces is a third helical cam surface and the other of the pair of single second complementary cam surfaces is a fourth helical cam surface that is complementary to the third helical cam surface. When the firearm bolt assembly is moved from the firing position to the initial position, interaction of the third and fourth helical cam surfaces causes the bolt head to twist, relative to the bolt body, in a second direction about the axis extending through the bolt head and bolt body, wherein the second direction is substantially opposite the first direction.
In embodiments the first helical cam surface and second helical cam surfaces are disposed proximate the top of the firearm bolt assembly, and the third and fourth helical cam surfaces are disposed proximate the bottom of the firearm bolt assembly. The first and third helical cam surfaces are defined by part of the bolt head, and the second and fourth helical cam surfaces are defined by a part of the bolt body. Movement of the firearm bolt assembly from the initial position to the firing position imparts a predominant compression force (pushing force) in the direction of the proximal end of the firearm bolt assembly, which causes the second helical cam surface to urge (e.g., be pushed) against the first cam surface. In contrast, movement of the firearm bolt assembly from the firing position to the initial position imparts a predominant compression force (pulling force) in the direction of the distal end of the firearm bolt assembly, which causes the fourth helical cam surface to urge (e.g., be pulled against) the third helical cam surface.
The firearm bolt assemblies described herein may further include a firing pin that is disposed within a bore formed in the bolt head and the bolt body. The firing pin may be biased by a firing pin spring. In such embodiments the firearm bolt assembly may be configured such that the spring is loaded (e.g., compressed) when the bolt body is compressed towards the bolt head as the firearm bolt assembly is moved from the initial position to the firing position. For example, the firearm bolt assembly may include a spring stop, a reset pin, a release pin, and a release channel. In embodiments the spring stop is positioned within the portion of the bore formed in the bolt body and includes a through hole through which the reset pin is disposed. The reset pin may extend into and/or through an opening formed in a sidewall of the bolt body. The release channel may be in the form of an L-shaped slot formed through a sidewall of the bolt head. The L-shaped slot may include a vertical leg and a longitudinal leg. In such embodiments a proximal portion of the release pin extends into the portion of the bore formed in bolt head, and a distal portion of the release pin extends into the L-shaped slot.
When the firearm bolt assembly is in the initial position, a portion of the release pin is present within the vertical leg of the L-shaped slot. As the firearm bolt assembly is moved from the initial position to the firing position, the bolt body is compressed towards the bolt head and the bolt head twists in a first direction relative to the bolt body due to the interaction of the pair of first single complementary cam surfaces. As the bolt body moves toward the bolt head but before the firing position is reached, the distal portion of the release pin is disposed within the vertical leg of the L-shaped slot. Consequently, movement of the bolt body towards the bolt head causes the spring stop to compress the firing pin spring and cock the firing pin. As the bolt head twists in the first direction relative to the bolt head, the distal end of the release pin moves within the vertical leg of the L-shaped slot towards the longitudinal leg. When firearm bolt assembly reaches the firing position, the bolt head is twisted enough in the first direction (relative to the bolt body) to cause the release pin to move into the longitudinal leg of the L-shaped slot. Movement of the release pin into the longitudinal leg releases the firing pin, causing the firing pin to strike the primer of a cartridge (if any) chambered in the firearm bolt assembly.
After the firearm bolt assembly reaches the firing position, the firearm bolt assembly may return from to the initial position by retracting the bolt body away from the bolt head. Immediately following the firing position, the release pin resides within the longitudinal leg of the L-shaped slot. As the bolt body is retracted away from the bolt head, the bolt head twists, relative to the bolt body, in a second direction about an axis extending through the bolt head and the bolt body, wherein the second direction is substantially opposite the first direction. As the bolt head twists in the second direction, the release pin moves within the longitudinal leg toward the vertical leg of the L-shaped slot. Eventually, retraction of the bolt body relative to the bolt head causes the release pin to move into the vertical leg of the L-shaped slot. At that or a later point, the bolt head is realigned with the bolt body, and the firearm bolt assembly is ready for another firing cycle.
As used herein, the phrases “only a pair of single first complementary cam surfaces” and “only a pair of single second complementary cam surfaces” are used in connection with first and second cam assemblies, respectively. In the context of the present disclosure, such phrases mean that the first cam system is made up of only two (i.e., two single) complementary cam surfaces, and the second cam system is made up of only two (i.e., two single) complementary cam surfaces. As will become apparent from the following description, in embodiments the first cam system is formed by only a single (first) cam surface on or formed by a bolt head, and a single (second) cam surface on or formed by a bolt body. Likewise, the second cam system is formed by only a single (third) cam surface on or formed by a bolt head, and only a single (fourth) cam surface on or formed by a bolt body. The first and second cam assemblies may be disposed on substantially opposite sides of a firearm bolt assembly.
As used herein, the term “substantially opposite” means opposite or nearly opposite (e.g., opposite within a +/−30% deviation tolerance, such as a +/−about 20%, +/−about 10%, or even +/−about 5% deviation tolerance). In some embodiments, “substantially opposite” means opposite or nearly opposite within a +/−5% deviation tolerance.
As used herein, the term “complementary” when used regarding two cam surfaces means that that the two cam surfaces define substantially opposite surface profiles that are designed to slide against one another during movement of a firearm bolt assembly from an initial position to a firing position, from the firing position to the initial position, or both.
As used herein, the term “predominant compressive force” when used regarding the compression of a firearm bolt assembly (e.g. as the bolt assembly is moved from the initial position to the firing position), means the (pushing) force directed towards the proximal end of the bolt assembly (i.e., towards the bolt head). In contrast the term “predominant compressive force” when used regarding retraction of firearm bolt assembly (e.g., as the bolt assembly is moved from the firing position to the initial position), means the (pulling) force directed towards the distal end of the firearm bolt assembly (i.e., towards the bolt body).
As discussed above the firearm assemblies presented herein utilize first and second cam systems that are each defined only by a pair of single complementary cam surfaces. The cam systems are configured such that the first cam system bears the predominant compressive forces that are imparted during movement of the firearm bolt assembly from an initial position to the firing position to a first side of the firearm bolt, whereas the second cam system bears the predominant compressive forces that are imparted during movement of the firearm bolt assembly from the firing position to the initial position to a second side of the bolt. In other words, the cam systems are configured such that the predominant compressive forces imparted during movement from the initial position to the firing position are localized to one portion (e.g., side) of the firearm bolt assembly, whereas the predominant compressive forces imparted during movement from the firing position to the initial position are localized to another portion (e.g., another side) of the firearm bolt assembly.
The predominant compressive forces imparted during movement from the initial position to the firing position may be greater than the predominant compressive forces imposed during movement from the firing position to the initial position. This is because during movement from the initial to the firing position, the compression force needs to overcome the expansion spring force of the firing pin spring. In contrast, movement of the firearm bolt assembly from the firing position to the initial position may be aided by the spring force of the firing pin spring. Consequently, the first and second cam assemblies may be configured such that the first cam system may withstand a greater applied compression force than the second cam system.
Put in other terms, in embodiments the firearm bolt assemblies described herein include first and second cam assemblies, wherein the first and second cam assemblies are configured such that only the first cam system bears the predominant compressive forces imparted during compression of the bolt body towards to the bolt head, whereas only the second cam system bears the predominant compressive forces imparted during retraction of the bolt body away from the bolt head. Because the predominant compressive forces applied during compression of the bolt body towards the bolt head compress a firing pin spring, such forces are larger than the compressive forces that are applied during retraction of the bolt body away from the bolt head. Consequently, the first cam system may have a wider/thicker neck, relative to a neck of the second cam system. As such, the first cam system may be able to withstand a larger amount of compression force relative to the second cam system.
As best shown in
The third cam surface 517 is designed to slide against the first cam surface 513 as the firearm bolt assembly 500 is moved from an initial position to a firing position. Thus, the first and third cam surfaces 513, 517 should each be understood to be one of a pair of first single complementary cam surfaces. Similarly, the fourth cam surface 519 is designed to slide against the second cam surface 515 as the firearm bolt assembly is moved from the firing position to the initial position. Thus, such surfaces may should also be understood to be one of a pair of second complementary cam surfaces. Accordingly, the first cam system is defined by only a pair of single first complementary cam surfaces (513, 517), and the second cam system is defined by only a pair of single second complementary cam surfaces (515, 519)
The first and second cam systems are rotation imparting structures that cause the bolt head 503 to rotate (twist) relative to the bolt body 501 as the firearm bolt assembly 500 is moved from an initial position to a firing position, and vice versa. In that regard, the first and third cam surfaces 513, 517 making up the first cam system may be in the form of first complementary helical cam surfaces, and the second and fourth cam surfaces 515, 519 may be in the form of second complementary helical cam surfaces. The first complementary helical cam surfaces may be the same or different from the second complementary helical cam surfaces. In embodiments, the second complementary helical cam surfaces are substantial opposites of the first complementary helical cam surfaces. Of course, the use of helical cam surfaces is not required and cam surfaces having any other suitable shape that causes bolt head 503 to twist relative to bolt body 501 as the bolt body 501 is compressed or retracted from bolt head 503 may also be used.
Like the Dillon and GE bolts the firearm bolt assemblies of the present disclosure are designed to move between an initial position to a firing position as the firearm bolt assembly is used to fire cartridge ammunition, discharge spent cartridges, and chamber a next cartridge. And like the Dillon and GE bolts, the firearm bolt assembly 500 includes track slots 520, 520′ that are designed to allow the firearm bolt assembly 500 to ride within a track of a rotor of a rotary firearm, e.g., a machine gun such as the M-134. That concept is best shown in
Although not shown in
After the proximal end 509 is positioned against the end of the barrel 605, the cam roller continues to ride forward in the helical path. With reference to
When firearm bolt assembly 500 is in the initial position a distal portion of the release pin 525 is present within the vertical leg of release channel 523, as best shown in
After the firearm bolt assembly 500 reaches the firing position the cam roller 505 moves rearwardly within the helical track to return the firearm bolt assembly 500 to the initial position. More specifically and with reference to
More specifically, after the firearm bolt assembly 500 reaches the firing position, the cam roller 505 may move rearward in the helical track within the housing of the firearm. The rearward movement of the cam roller 505 imposes a force on the bolt body 501 in a direction towards the distal end 511. Immediately after the firearm bolt assembly 500 achieves the firing position, the release pin 525 resides within the longitudinal leg of the L-shaped slot 523, as shown in
In different terms and with reference to
The second wedge W2 has a first side that extends from a tip 560 of the bolt head 503 towards a second interface point 565 along an edge 569 of track slot 520′, such that the first side of W2 is generally oriented towards the distal end 511 of the firearm bolt assembly 500. The second interface point 565 may be understood as the point at which the first side (e.g., the hypotenuse) of the wedge W2 meets the edge of track slot 520′. A second side of the second wedge W2 extends along a line that extends perpendicularly (relative to axis A) from the second interface point 565 along the top surface of the firearm bolt head 503 towards an edge point 567 on an edge of track slot 520 in bolt head 503. The second side of wedge W2 may have a curvilinear component proximate the edge point 565 that transitions to a linear component as it extends perpendicular to the axis A and away from the edge point 565. In embodiments the edge point 567 is substantially opposite the edge point 559. The third side of the second wedge W2 extends along a line from the tip 560 to a point intersecting the line defining the second side of wedge W2, such that wedge W2 is in the form of a right triangle. Cam surface 513 is defined generally along the first side of the second wedge W2.
In contrast and with reference to
The second inverse wedge IW2 has a first side that extends from a tip 580 of the bolt head 503 towards a fourth interface point 585, such that the first side of IW2 is generally oriented toward the proximal end 509. The fourth interface point 585 may be understood as the point at which the first side (e.g., the hypotenuse) of the second inverse wedge IW2 meets a shoulder 588 of the bolt head 503. A second side of the second inverse wedge IW2 extends along a line that extends perpendicularly (relative to axis A) from the fourth interface point 585 along the shoulder 588 towards track slot 520 in bolt head 503. The third side of the second inverse wedge IW2 extends along a line from the tip 580 to a point intersecting the line defining the second side of inverse wedge IW2, such that inverse wedge IW2 is in the form of a right triangle. Cam surface 513 is defined generally along the first side of the second wedge W2.
Referring again to
Similarly, and with reference to
As further shown in
Example 1: In this example there is provided a firearm bolt assembly, including: a first side, a second side, a proximal end, and a distal end, the first side being substantially opposite the second side; a bolt head; a bolt body; a first cam system defined by only a pair of single first complementary cam surfaces proximate the first side of the firearm bolt assembly, the bolt head including one of the pair of single first complementary cam surfaces, the bolt body including another of the pair of single first complementary cam surfaces; and a second cam system defined by only a pair of single second complementary cam surfaces proximate the second side of the firearm bolt assembly, the bolt head including one of the pair of single second complementary cam surfaces, the bolt body including another of the pair of single second complementary cam surfaces.
Example 2: This example includes any or all of the features of example 1, wherein: the firearm bolt assembly is movable from an initial position to a firing position by compression of the bolt body towards the proximal end, during which a predominant compression force is born by the first cam system; and the firearm bolt assembly is movable from the firing position to the initial position by retraction of the bolt body away from the proximal end, during which a predominant compression force is born by the second cam system.
Example 3: This example includes any or all of the features of example 1, wherein: one of the pair of single first complementary cam surfaces includes a first helical cam surface and the other of the pair of single first complementary cam surfaces includes second helical cam surface that is complementary to the first helical cam surface, such that when the firearm bolt assembly is moved from the initial position to the firing position interaction of the first and second helical cam surfaces causes the bolt head to twist, relative to the bolt body, in a first direction about an axis extending through the bolt head and the bolt body.
Example 4: This example includes any or all of the features of example 3, wherein: one of the pair of single second complementary cam surfaces includes a third helical cam surface and the other of the pair of single second complementary cam surfaces includes a fourth helical cam surface complementary to the third helical cam surface, such that when the firearm bolt assembly is moved from the firing position to the initial position, interaction of the third and fourth helical cam surfaces causes the bolt head to twist, relative to the bolt body, in a second direction about the axis extending through the bolt head and the bolt body, the second direction being substantially opposite the first direction.
Example 5: This example includes any or all the features of example 2, wherein when the firearm bolt assembly is moved from the initial position to the firing position, the predominant compressive force is directed towards the proximal end.
Example 6: This example includes any or all the features of example 2, wherein when the firearm bolt assembly is moved from the firing position to the initial position, the predominant compressive force is directed towards the distal end.
Example 7: According to this example there is provided a machine gun, including: a rotationally driven rotor; a plurality of barrels, wherein each of the plurality barrels is disposed in the rotor; at least one firearm bolt assembly aligned within a respective one of the plurality of barrels, wherein the at least one firearm bolt assembly includes: a first side, a second side, a proximal end, and a distal end, the first side being substantially opposite the second side; a bolt head; a bolt body; a first cam system defined by only a pair of single first complementary cam surfaces proximate the first side of the firearm bolt assembly, the bolt head including one of the pair of single first complementary cam surfaces, the bolt body including another of the pair of single first complementary cam surfaces; and a second cam system defined by only a pair of single second complementary cam surfaces proximate the second side of the firearm bolt assembly, the bolt head including one of the pair of single second complementary cam surfaces, the bolt body including another of the pair of single second complementary cam surfaces.
Example 8: This example includes any or all of the features of example 7, wherein: the firearm bolt assembly is movable from an initial position to a firing position by compression of the bolt body towards the proximal end, during which a predominant compression force is born by the first cam system; and the firearm bolt assembly is movable from the firing position to the initial position by retraction of the bolt body away from the proximal end, during which a predominant compression force is born by the second cam system.
Example 9: This example includes any or all of the features of example 7, wherein: one of the pair of single first complementary cam surfaces includes a first helical cam surface and the other of the pair of single first complementary cam surfaces includes second helical cam surface that is complementary to the first helical cam surface, such that when the firearm bolt assembly is moved from the initial position to the firing position interaction of the first and second helical cam surfaces causes the bolt head to twist, relative to the bolt body, in a first direction about an axis extending through the bolt head and the bolt body.
Example 10: This example includes any or all of the features of example 7, wherein: one of the pair of single second complementary cam surfaces includes a third helical cam surface and the other of the pair of single second complementary cam surfaces includes a fourth helical cam surface complementary to the third helical cam surface, such that when the firearm bolt assembly is moved from the firing position to the initial position, interaction of the third and fourth helical cam surfaces causes the bolt head to twist, relative to the bolt body, in a second direction about the axis extending through the bolt head and the bolt body, the second direction being substantially opposite the first direction.
Example 11: This example includes any or all the features of example 8, wherein when the firearm bolt assembly is moved from the initial position to the firing position, the predominant compressive force is directed towards the proximal end.
Example 12: This example includes any or all the features of example 8, wherein when the firearm bolt assembly is moved from the firing position to the initial position, the predominant compressive force is directed towards the distal end.
Example 13: According to this example there is provided a firearm bolt assembly that is movable between an initial position and a firing position, including: a first side, a second side, a proximal end, and a distal end, the first side being substantially opposite the second side; a bolt body including a first wedge proximate the first side of the firearm bolt assembly and a first inverse wedge proximate the second side of the firearm bolt assembly; a bolt head including a second wedge proximate the first side of the firearm bolt assembly and a second inverse wedge proximate the second side of the firearm bolt assembly; wherein: the first and second wedges define a first cam system, the first cam system including a first cam surface on the first wedge that is oriented towards the proximal end of the firearm bolt assembly, and a second cam surface on the second wedge that is oriented towards the distal end of the firearm assembly; and the first and second inverse wedges define a second cam system, the second cam system including a third cam surface on the first inverse wedge that is oriented towards the distal end of the firearm bolt assembly, and a fourth cam surface of the second inverse wedge that is oriented towards the proximate end of the firearm bolt assembly.
Example 14: This example includes any or all of the features of example 13, wherein: the firearm bolt assembly is movable from an initial position to a firing position by compression of the bolt body towards the proximal end, during which a predominant compression force is born by the first cam system; and the firearm bolt assembly is movable from the firing position to the initial position by retraction of the bolt body away from the proximal end, during which a predominant compression force is born by the second cam system.
Example 15: This example includes any or all of the features of example 14, wherein: the first cam surface is a first helical cam surface and the second cam surface is a second helical cam surface that is complementary to the first helical cam surface; the third cam surface is a third helical cam surface and the fourth cam surface is a fourth helical cam surface that is complementary to the third helical cam surface, the third and fourth helical cam surfaces being substantial opposites of the first and second helical cam surfaces, respectively.
Example 16: This example includes any or all of the features of example 14, wherein when the firearm bolt assembly is moved from the initial position to the firing position, the first and second helical cam surfaces interact and cause the bolt head to twist, relative to the bolt body, in a first direction about an axis extending through the bolt head and the bolt body.
Example 17: This example includes any or all of the features of example 16, wherein when the firearm bolt assembly is moved from the firing position to the initial position the third and fourth helical cam surfaces interact and cause the bolt head to twist, relative to the bolt body, in a second direction about the axis extending through the bolt head and the bolt body, the second direction being substantially opposite the first direction.
Example 18: This example includes any or all the features of example 14, wherein when the firearm bolt assembly is moved from the initial position to the firing position, the predominant compressive force is directed towards the proximal end.
Example 19: This example includes any or all the features of example 14, wherein when the firearm bolt assembly is moved from the firing position to the initial position, the predominant compressive force is directed towards the distal end.
As may be appreciated from the foregoing, the firearm bolt assemblies described herein may be configured to localize compressive forces applied during a transition from an initial position to a firing position to a first cam system on one side of the firearm bolt assembly, and to localize compressive forces applied during a transition from the firing position to the initial position to a second cam system another side of the firearm bolt assembly. Localizing the forces in that manner enables the use of a first cam system that is relatively robust compared to the second cam system. Such designs may exhibit improved durability relative to the GE and Dillon bolts of the prior art.
The terms and expressions which have been employed herein are used as terms of description and not of limitation, and there is no intention, in the use of such terms and expressions, of excluding any equivalents of the features shown and described (or portions thereof), and it is recognized that various modifications are possible within the scope of the claims. Accordingly, the claims are intended to cover all such equivalents.
This application is a Continuation of U.S. patent application Ser. No. 17/343,916 filed Jun. 10, 2021, which is a Continuation of U.S. patent application Ser. No. 16/279,211 filed Feb. 19, 2019, now U.S. Pat. No. 11,143,488, issued Oct. 12, 2021; U.S. patent application Ser. No. 17/343,916 is incorporated herein by reference in its entirety, and U.S. patent application Ser. No. 16/279,211, now U.S. Pat. No. 11,143,488, is incorporated herein by reference in its entirety.
Number | Date | Country | |
---|---|---|---|
Parent | 17343916 | Jun 2021 | US |
Child | 18210645 | US | |
Parent | 16279211 | Feb 2019 | US |
Child | 17343916 | US |