CN111981918B - Connecting device for combined warhead - Google Patents
Connecting device for combined warhead Download PDFInfo
- Publication number
- CN111981918B CN111981918B CN202010863325.8A CN202010863325A CN111981918B CN 111981918 B CN111981918 B CN 111981918B CN 202010863325 A CN202010863325 A CN 202010863325A CN 111981918 B CN111981918 B CN 111981918B
- Authority
- CN
- China
- Prior art keywords
- connecting frame
- cover connecting
- circular
- upper cover
- circular plane
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B33/00—Manufacture of ammunition; Dismantling of ammunition; Apparatus therefor
Landscapes
- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- General Engineering & Computer Science (AREA)
- Joining Of Building Structures In Genera (AREA)
Abstract
The invention discloses a connecting device for a combined warhead, wherein a circle of second annular boss is arranged in the middle of a second upper end circular plane of an upper cover connecting frame, second circular through holes are circumferentially and uniformly distributed at the edge of the second lower end circular plane of the upper cover connecting frame, second circular blind holes are circumferentially and uniformly distributed in the middle of the second lower end circular plane of the upper cover connecting frame, and a second outer cylindrical surface is arranged on the side surface of the second circular boss of the upper cover connecting frame; according to the invention, after the upper warhead is connected with the upper cover connecting frame, the upper cover connecting frame and the lower end connecting frame are provided with large chamfers, when the upper cover connecting frame and the lower end connecting frame are combined, the chamfers automatically correct the position accuracy, and after the upper cover connecting frame and the lower end connecting frame are coaxial, the seventh sphere of the ball body jacks up the upper cover connecting frame, the upper warhead can freely rotate around the axis until the pin enters the pin hole, so that the circumferential angle position accuracy is ensured, and the time is saved.
Description
Technical Field
The invention belongs to the technical field of warheads, relates to a combined warhead, and particularly relates to a connecting device for the combined warhead.
Background
Blasting warheads is the simplest of the blasting warheads. It consists of a large number of high explosive charges in a metal shell, and the target is destroyed by the blasting effect generated when the main charge is exploded.
The state of application vast et al reports in the literature "the present situation and development of the warship warhead of conventional anti-ship missiles" (proceedings of war institute of war, sichuan university, 2006, page 14, 3): the damage power of the warhead is in proportion to the mass and the volume of the warhead, and the current warhead takes implosion type and great power as main research directions. However, with the increase of the size of the warhead, new problems are encountered, such as the increase of the processing difficulty of the shell, the increase of the charging difficulty, the increase of the transportation difficulty and the like.
The size of the warhead is affected by the above factors, and is difficult to increase after reaching a certain size. To meet the development requirements of larger-sized warheads, two warheads are typically connected in series prior to use. Before the experiment, one warhead is placed at the upper end of the other warhead, 2 warheads are superposed to form 1 warhead, the combined warheads are made, and then the warheads are detonated simultaneously to generate the explosion effect of the warheads with large explosive loads. However, the combined warhead has the following problems in the use process:
(1) the upper end warhead is placed on the terminal surface of lower end warhead, often no longer carries out mechanical connection, when the test field is windy or the terminal surface unevenness, in case the slope takes place, the easy landing of upper end warhead will take place dangerously.
(2) Because the size of the upper-end warhead is larger, when the upper-end warhead is placed towards the lower end face, a crane is usually used for moving in a matched mode, the stroke error of the crane is larger, after the upper-end warhead is placed, the coaxiality precision of the upper-end warhead and the axis of the lower-end warhead is poorer, the coaxiality error is larger, the axial symmetry is poor, and the power of the warhead after explosion is influenced.
(3) After the upper-end warhead is placed, the annular angle position precision of the upper-end warhead and the lower-end warhead is poor, and the annular angle error is large, so that the functional performance of the warhead is influenced, and the power of the warhead after explosion is influenced.
(4) Because the upper end of the warhead is heavy, when the upper end of the warhead moves through a crane, the moving distance is large each time, the position precision of each adjustment is poor, the adjustment needs to be repeated, the installation speed is slow, and the time is wasted.
Disclosure of Invention
In order to overcome the defects and defects of the prior art, the invention provides a connecting device for a combined warhead, the connecting device for the combined warhead is characterized in that after the upper end warhead is connected with an upper cover connecting frame, although the position precision of each adjustment is poor when a crane is used for displacement, the upper cover connecting frame and a lower end connecting frame are both provided with large chamfers, when the upper cover connecting frame and the lower end connecting frame are combined, the position precision is automatically corrected by the chamfers, after the upper cover connecting frame and the lower end connecting frame are coaxial, the upper cover connecting frame can freely rotate around an axis because a seventh sphere of a ball body jacks up the upper cover connecting frame until a pin enters a pin hole, the circumferential angle position precision is ensured, the process is not repeatedly adjusted, the installation and the forming are carried out once, and the time is saved.
The invention provides a connecting device for a combined warhead, which comprises an upper end shell 1 and a lower end shell 5, and is characterized by further comprising an upper cover connecting frame 2, a lower cover connecting frame 3, a pin 4 and a spring 6;
the upper end shell 1 is a first cylinder, the first cylinder of the upper end shell 1 is a revolving body, the lower end surface of the first cylinder of the upper end shell 1 is a first lower end circular plane, and the side surface of the first cylinder of the upper end shell 1 is a first outer cylindrical surface;
the axis of the revolving body of the upper end shell 1 is vertical to the ground, and the upper end shell 1 is a warhead shell positioned at the upper end;
the upper cover connecting frame 2 is a second circular plate, the second circular plate of the upper cover connecting frame 2 is a revolving body, the upper end surface of the second circular plate of the upper cover connecting frame 2 is a second upper end circular plane, the lower end surface of the second circular plate of the upper cover connecting frame 2 is a second lower end circular plane, the middle part of the second upper end circular plane of the upper cover connecting frame 2 is provided with a circle of second annular boss, the inner side surface of the second annular boss of the upper cover connecting frame 2 is a second inner cylindrical surface, the second inner cylindrical surface of the upper cover connecting frame 2 is provided with a circle of second threaded holes, the edge of the second lower end circular plane of the upper cover connecting frame 2 is provided with second circular through holes which are uniformly distributed in the circumferential direction, the middle part of the second lower end circular plane of the upper cover connecting frame 2 is provided with second circular blind holes which are uniformly distributed in the circumferential direction, the center of the second lower end circular plane of the upper cover connecting frame 2 is provided with a second circular boss, the lower end surface of the second circular boss of the upper cover connecting frame 2 is a second lower end central circular plane, the side surface of a second circular boss of the upper cover connecting frame 2 is a second outer cylindrical surface, and a second chamfer is arranged at the joint of a second lower end central circular plane of the upper cover connecting frame 2 and the second outer cylindrical surface;
the revolving body axis of the upper cover connecting frame 2 coincides with the revolving body axis of the upper end shell 1, the upper cover connecting frame 2 is positioned at the lower end of the upper end shell 1, a first lower end circular plane of the upper end shell 1 is contacted with a second upper end circular plane of the upper cover connecting frame 2, a first outer cylindrical surface of the upper end shell 1 is contacted with a second inner cylindrical surface of the upper cover connecting frame 2, a second screw is arranged in a second threaded hole of the upper cover connecting frame 2 and is contacted with a first outer cylindrical surface of the upper end shell 1, and the upper end shell 1 is connected with the upper cover connecting frame 2 through the second screw;
the lower cover connecting frame 3 is a third circular plate, the third circular plate of the lower cover connecting frame 3 is a rotary body, the upper end surface of the third circular plate of the lower cover connecting frame 3 is a third upper end circular plane, the lower end surface of the third circular plate of the lower cover connecting frame 3 is a third lower end circular plane, the center of the third upper end circular plane of the lower cover connecting frame 3 is provided with a third central circular through hole, the inner side surface of the third central circular through hole of the lower cover connecting frame 3 is a third inner cylindrical surface, the joint of the third inner cylindrical surface and the third upper end circular plane of the lower cover connecting frame 3 is provided with a third chamfer, the middle part of the third upper end circular plane of the lower cover connecting frame 3 is provided with third circular blind holes which are uniformly distributed in the circumferential direction, the middle part of the third upper end circular plane of the lower cover connecting frame 3 is provided with third spherical holes which are uniformly distributed in the circumferential direction, the edge of the third upper end circular plane of the lower cover connecting frame 3 is provided with third circular through holes which are uniformly distributed in the circumferential direction, the middle part of the third lower cover connecting frame 3 is provided with a third annular boss in the middle part, the inner side surface of a third annular boss of the lower cover connecting frame 3 is a third lower end inner cylindrical surface, and a circle of third threaded hole is formed in the third lower end inner cylindrical surface of the lower cover connecting frame 3;
the axis of the rotary body of the lower cover connecting frame 3 coincides with the axis of the rotary body of the upper cover connecting frame 2, the lower cover connecting frame 3 is positioned at the lower end of the upper cover connecting frame 2, the third inner cylindrical surface of the lower cover connecting frame 3 is contacted with the second outer cylindrical surface of the upper cover connecting frame 2, a third screw is arranged in a third circular through hole of the lower cover connecting frame 3, the third screw penetrates through the second circular through hole of the upper cover connecting frame 2, the head of the third screw is connected with a nut, and the lower cover connecting frame 3 is connected with the upper cover connecting frame 2 through the third screw;
the pin 4 is a fourth cylinder, and the fourth cylinder of the pin 4 is a revolving body;
the axis of the revolving body of the pin 4 is parallel to the axis of the revolving body of the upper end shell 1, the lower end of the pin 4 is positioned in the third circular blind hole of the lower cover connecting frame 3, and the upper end of the pin 4 is positioned in the second circular blind hole of the upper cover connecting frame 2;
the lower end shell 5 is a fifth cylinder, the fifth cylinder of the lower end shell 5 is a revolving body, the upper end surface of the fifth cylinder of the lower end shell 5 is a fifth upper end circular plane, and the side surface of the fifth cylinder of the lower end shell 5 is a fifth outer cylindrical surface;
the axis of the revolving body of the lower end shell 5 coincides with the axis of the revolving body of the upper end shell 1, the lower end shell 5 is a warhead shell positioned at the lower end, the lower end shell 5 is positioned at the lower end of the lower cover connecting frame 3, a fifth upper end circular plane of the lower end shell 5 is contacted with a third lower end circular plane of the lower cover connecting frame 3, a fifth outer cylindrical surface of the lower end shell 5 is contacted with a third lower end inner cylindrical surface of the lower cover connecting frame 3, a fifth screw is arranged in a third threaded hole of the lower cover connecting frame 3 and is contacted with a fifth outer cylindrical surface of the lower end shell 5, and the lower cover connecting frame 3 is connected with the lower end shell 5 by the fifth screw;
the spring 6 is a sixth spiral revolving body;
the spiral rotation axis of the spring 6 is parallel to the rotation body axis of the upper end shell 1, the spring 6 is positioned in the third circular blind hole of the lower cover connecting frame 3, and the spring 6 is positioned at the lower end of the pin 4;
the ball body 7 is a seventh sphere;
the ball body 7 is positioned in the third spherical hole of the lower cover connecting frame 3, and the uppermost end of the ball body 7 is in contact with the second lower end circular plane of the upper cover connecting frame 2;
the second lower end central circular plane of the upper cover connecting frame 2 is 2-3 mm higher than the third lower end circular plane of the lower cover connecting frame 3;
the uppermost end point of the seventh sphere of the ball body 7 is 0.7 mm-0.9 mm higher than the third upper end circular plane of the lower cover connecting frame 3;
the diameter of a second round blind hole of the upper cover connecting frame 2 is 0.5 mm-0.7 mm larger than that of a fourth cylinder of the pin 4;
the ratio of the axial length of the second chamfer of the upper cover connecting frame 2 to the height of the second circular boss of the upper cover connecting frame 2 is 1: 3-4;
the ratio of the axial length of the third chamfer of the lower cover connecting frame 3 to the height of the second circular boss of the upper cover connecting frame 2 is 1: 3 to 4.
Regarding the second lower end center circular plane of the upper cover link 2 is higher than the third lower end circular plane of the lower cover link 3 by a dimension, the seventh sphere uppermost end point of the ball body 7 is higher than the third upper end circular plane of the lower cover link 3 by a dimension, the second circular blind hole diameter of the upper cover link 2 is larger than the fourth cylinder diameter of the pin 4 by a dimension, the ratio of the axial length of the second chamfer of the upper cover link 2 to the second circular boss height of the upper cover link 2, and the ratio of the axial length of the third chamfer of the lower cover link 3 to the second circular boss height of the upper cover link 2, any one of the following 2 ways can be adopted:
implementation mode 1: the second lower end central circular plane of the upper cover connecting frame 2 is 2mm higher than the third lower end circular plane of the lower cover connecting frame 3;
the uppermost end point of the seventh sphere of the ball body 7 is 0.7mm higher than the third upper end circular plane of the lower cover connecting frame 3;
the diameter of a second round blind hole of the upper cover connecting frame 2 is 0.5mm larger than that of a fourth cylinder of the pin 4;
the ratio of the axial length of the second chamfer of the upper cover connecting frame 2 to the height of the second circular boss of the upper cover connecting frame 2 is 1: 3;
the ratio of the axial length of the third chamfer of the lower cover connecting frame 3 to the height of the second circular boss of the upper cover connecting frame 2 is 1: 3.
implementation mode 2: the second lower end central circular plane of the upper cover connecting frame 2 is 3mm higher than the third lower end circular plane of the lower cover connecting frame 3;
the uppermost end point of the seventh sphere of the ball body 7 is 0.9mm higher than the third upper end circular plane of the lower cover connecting frame 3;
the diameter of a second round blind hole of the upper cover connecting frame 2 is 0.7mm larger than that of a fourth cylinder of the pin 4;
the ratio of the axial length of the second chamfer of the upper cover connecting frame 2 to the height of the second circular boss of the upper cover connecting frame 2 is 1: 4;
the ratio of the axial length of the third chamfer of the lower cover connecting frame 3 to the height of the second circular boss of the upper cover connecting frame 2 is 1: 4.
the connecting device for the combined warhead brings the following technical effects:
(1) the device and the upper end warhead are mechanically connected into a whole, and the device and the lower end warhead are also mechanically connected into a whole, so that the upper end warhead and the lower end warhead are integrated, and even if wind or inclination occurs, as long as the lower end warhead is reliably connected with the base, the upper end warhead and the lower end warhead are kept in a tightly connected state, and the upper end warhead cannot slide off, so that the safety is ensured.
(2) The upper end warhead is coaxial after being connected with the upper cover link, and the lower end warhead is coaxial after being connected with the lower cover link, and the circular boss of second of upper cover link contacts the back with the circular through-hole in third center of lower cover link, and the upper cover link is coaxial with the lower cover link, and consequently, the upper end warhead after the assembly is higher with lower extreme warhead axiality precision, has guaranteed the axial symmetry nature of combination warhead, has guaranteed the power after the warhead explosion.
(3) The annular angle position precision is higher after upper end warhead and upper cover link joint, and the annular angle position precision is higher after lower extreme warhead and lower cover link joint, and upper end warhead passes through pin accurate control annular position precision with lower extreme warhead, and upper end warhead and lower extreme warhead annular angle position precision are higher promptly, guarantee that functional part works at predetermined angle on the warhead, have guaranteed the power after the warhead explosion.
(4) After the upper warhead is connected with the upper cover connecting frame, although when the upper warhead is displaced through a crane, the moving distance is large each time, the position precision of each adjustment is poor, the upper cover connecting frame and the lower end connecting frame are both provided with large chamfers, when the upper cover connecting frame and the lower end connecting frame are combined, the chamfers automatically correct the axis coincidence precision, after the upper cover connecting frame and the lower end connecting frame are coaxial, the seventh sphere of the ball body jacks up the upper cover connecting frame, the upper warhead can freely rotate around the axis until the pin enters the pin hole, the circumferential angle position precision is guaranteed, the process is not repeatedly adjusted, the installation and forming are carried out once, and the time is saved.
Drawings
Fig. 1 is a schematic view showing a structure of a coupling device for a combo warhead. 1. The device comprises an upper end shell, 2 an upper cover connecting frame, 3 a lower cover connecting frame, 4 a pin, 5 a lower end shell, 6 a spring, 7 and a ball body.
Detailed Description
The present invention is further described in detail with reference to the drawings and examples, it should be noted that the present invention is not limited to the following examples, and equivalent modifications based on the technical scheme of the present invention are within the scope of the present invention.
Example 1:
as shown in fig. 1, the connecting device for a combined warhead in the embodiment comprises an upper end shell 1 and a lower end shell 5, and is characterized by further comprising an upper cover connecting frame 2, a lower cover connecting frame 3, a pin 4 and a spring 6;
the upper end shell 1 is a first cylinder, the first cylinder of the upper end shell 1 is a revolving body, the lower end surface of the first cylinder of the upper end shell 1 is a first lower end circular plane, and the side surface of the first cylinder of the upper end shell 1 is a first outer cylindrical surface;
the axis of the revolving body of the upper end shell 1 is vertical to the ground, and the upper end shell 1 is a warhead shell positioned at the upper end;
the upper cover connecting frame 2 is a second circular plate, the second circular plate of the upper cover connecting frame 2 is a revolving body, the upper end surface of the second circular plate of the upper cover connecting frame 2 is a second upper end circular plane, the lower end surface of the second circular plate of the upper cover connecting frame 2 is a second lower end circular plane, the middle part of the second upper end circular plane of the upper cover connecting frame 2 is provided with a circle of second annular boss, the inner side surface of the second annular boss of the upper cover connecting frame 2 is a second inner cylindrical surface, the second inner cylindrical surface of the upper cover connecting frame 2 is provided with a circle of second threaded holes, the edge of the second lower end circular plane of the upper cover connecting frame 2 is provided with second circular through holes which are uniformly distributed in the circumferential direction, the middle part of the second lower end circular plane of the upper cover connecting frame 2 is provided with second circular blind holes which are uniformly distributed in the circumferential direction, the center of the second lower end circular plane of the upper cover connecting frame 2 is provided with a second circular boss, the lower end surface of the second circular boss of the upper cover connecting frame 2 is a second lower end central circular plane, the side surface of a second circular boss of the upper cover connecting frame 2 is a second outer cylindrical surface, and a second chamfer is arranged at the joint of a second lower end central circular plane of the upper cover connecting frame 2 and the second outer cylindrical surface;
the axis of a revolving body of the upper cover connecting frame 2 is coincident with the axis of a revolving body of the upper end shell 1, the upper cover connecting frame 2 is positioned at the lower end of the upper end shell 1, a first lower end circular plane of the upper end shell 1 is contacted with a second upper end circular plane of the upper cover connecting frame 2, a first outer cylindrical surface of the upper end shell 1 is contacted with a second inner cylindrical surface of the upper cover connecting frame 2, a second screw is arranged in a second threaded hole of the upper cover connecting frame 2 and is contacted with a first outer cylindrical surface of the upper end shell 1, and the upper end shell 1 is connected with the upper cover connecting frame 2 through the second screw;
the lower cover connecting frame 3 is a third circular plate, the third circular plate of the lower cover connecting frame 3 is a revolving body, the upper end surface of the third circular plate of the lower cover connecting frame 3 is a third upper end circular plane, the lower end surface of the third circular plate of the lower cover connecting frame 3 is a third lower end circular plane, the center of the third upper end circular plane of the lower cover connecting frame 3 is provided with a third central circular through hole, the inner side surface of the third central circular through hole of the lower cover connecting frame 3 is a third inner cylindrical surface, the joint of the third inner cylindrical surface and the third upper end circular plane of the lower cover connecting frame 3 is provided with a third chamfer, the middle part of the third upper end circular plane of the lower cover connecting frame 3 is provided with third circular blind holes which are uniformly distributed in the circumferential direction, the middle part of the third upper end circular plane of the lower cover connecting frame 3 is provided with third spherical holes which are uniformly distributed in the circumferential direction, the middle part of the third lower end circular plane of the lower cover connecting frame 3 is provided with a third annular boss in the circumferential direction, the inner side surface of a third annular boss of the lower cover connecting frame 3 is a third lower end inner cylindrical surface, and a circle of third threaded hole is formed in the third lower end inner cylindrical surface of the lower cover connecting frame 3;
the axis of the rotary body of the lower cover connecting frame 3 coincides with the axis of the rotary body of the upper cover connecting frame 2, the lower cover connecting frame 3 is positioned at the lower end of the upper cover connecting frame 2, the third inner cylindrical surface of the lower cover connecting frame 3 is contacted with the second outer cylindrical surface of the upper cover connecting frame 2, a third screw is arranged in a third circular through hole of the lower cover connecting frame 3, the third screw penetrates through the second circular through hole of the upper cover connecting frame 2, the head of the third screw is connected with a nut, and the lower cover connecting frame 3 is connected with the upper cover connecting frame 2 through the third screw;
the pin 4 is a fourth cylinder, and the fourth cylinder of the pin 4 is a revolving body;
the axis of the revolving body of the pin 4 is parallel to the axis of the revolving body of the upper end shell 1, the lower end of the pin 4 is positioned in the third circular blind hole of the lower cover connecting frame 3, and the upper end of the pin 4 is positioned in the second circular blind hole of the upper cover connecting frame 2;
the lower end shell 5 is a fifth cylinder, the fifth cylinder of the lower end shell 5 is a revolving body, the upper end surface of the fifth cylinder of the lower end shell 5 is a fifth upper end circular plane, and the side surface of the fifth cylinder of the lower end shell 5 is a fifth outer cylindrical surface;
the axis of the revolving body of the lower end shell 5 coincides with the axis of the revolving body of the upper end shell 1, the lower end shell 5 is a warhead shell positioned at the lower end, the lower end shell 5 is positioned at the lower end of the lower cover connecting frame 3, a fifth upper end circular plane of the lower end shell 5 is contacted with a third lower end circular plane of the lower cover connecting frame 3, a fifth outer cylindrical surface of the lower end shell 5 is contacted with a third lower end inner cylindrical surface of the lower cover connecting frame 3, a fifth screw is arranged in a third threaded hole of the lower cover connecting frame 3 and is contacted with a fifth outer cylindrical surface of the lower end shell 5, and the lower cover connecting frame 3 is connected with the lower end shell 5 by the fifth screw;
the number of the fifth screws is 16, the number of the fifth screws is M20, each of the fifth screws has a preload of 100 kn, the coefficient of friction between the fifth screws and the fifth outer cylindrical surface of the lower housing 5 is 0.1, i.e., the maximum friction force that each of the fifth screws and the fifth outer cylindrical surface of the lower housing 5 can generate is 10 kn, the maximum friction force that each of the fifth screws and the fifth outer cylindrical surface of the lower housing 5 can generate is 160 kn, i.e., 160000N, and the mass of the lower housing 5 is about 10 tons, i.e., the gravity of the lower housing 5 is 100000N, and the maximum friction force that each of the 16 fifth screws and the fifth outer cylindrical surface of the lower housing 5 generates is 1.6 times the weight of the lower housing 5, so that the lower cover connecting frame 3 and the lower housing 5 can be reliably connected.
The spring 6 is a sixth spiral revolving body;
the spiral rotation axis of the spring 6 is parallel to the rotation body axis of the upper end shell 1, the spring 6 is positioned in the third circular blind hole of the lower cover connecting frame 3, and the spring 6 is positioned at the lower end of the pin 4;
the ball body 7 is a seventh sphere;
the ball body 7 is positioned in the third spherical hole of the lower cover connecting frame 3, and the uppermost end of the ball body 7 is in contact with the second lower end circular plane of the upper cover connecting frame 2;
the using method and the working principle of the invention are as follows: through upper cover link 2 and 1 mechanical connection's of upper end casing mode, upper cover link 2 is a whole with 1 zonulae occludens of upper end casing, through lower cover link 3 and 5 mechanical connection's of lower extreme casing mode, lower cover link 3 is a whole with 5 zonulae occludens of lower extreme casing, upper cover link 2 and 3 rethread mechanical connection's of lower cover link mode, upper cover link 2 is a whole with 3 zonulae occludens of lower cover link, thereby, upper end casing 1 is a whole with 5 zonulae occludens of lower extreme casing. Thereby ensuring the strength of the connection.
The second circular boss of the upper cover connecting frame 2 is inserted into the third central circular through hole of the lower cover connecting frame 3, so that the coaxiality of the upper cover connecting frame 2 and the lower cover connecting frame 3 is ensured, and further the coaxiality of the upper end shell 1 and the lower end shell 5 is ensured.
The upper cover connecting frame 2 and the lower cover connecting frame 3 are provided with chamfers, so that the chamfers can correct the positions of the upper cover connecting frame 2 and the lower cover connecting frame 3 to be coaxial finally even if the upper cover connecting frame 2 and the lower cover connecting frame 3 are not coaxial at the initial moment of installation.
The ball body 7 jacks up the upper cover connecting frame 2, the upper cover connecting frame 2 can drive the upper end shell 1 to freely rotate at the upper end of the lower cover connecting frame 3, the pin 4 is positioned in the third circular blind hole of the lower cover connecting frame 3 in the rotating process of the upper cover connecting frame 2, until the annular relative position of the upper end shell 1 and the lower end shell 5 is correct, the upper end of the pin 4 just enters the second circular blind hole of the upper cover connecting frame 2, subsequently, the upper end and the lower end of the pin 4 are respectively clamped in the third circular blind hole of the lower cover connecting frame 3 and the second circular blind hole of the upper cover connecting frame 2, the lower cover connecting frame 3 and the upper cover connecting frame 2 are prevented from rotating relatively in the annular direction, and therefore the annular relative position of the upper end shell 1 and the lower end shell 5 is correct.
When the second lower end central circular plane of the upper cover connecting frame 2 is too small in size higher than the third lower end circular plane of the lower cover connecting frame 3, the second lower end central circular plane of the upper cover connecting frame 2 is easily contacted with the lower end shell 5, the friction resistance of the rotation of the lower end shell 5 is increased, when the second lower end central circular plane of the upper cover connecting frame 2 is too large in size higher than the third lower end circular plane of the lower cover connecting frame 3, the second circular boss of the upper cover connecting frame 2 and the third central circular through hole contact surface of the lower cover connecting frame 3 are too small in size, and the coaxiality is not facilitated. Experiments show that the requirements are met when the second lower end central circular plane of the upper cover connecting frame 2 is 2-3 mm higher than the third lower end circular plane of the lower cover connecting frame 3;
in this embodiment, the second lower end center circular plane of the upper cover link 2 is higher than the third lower end circular plane of the lower cover link 3 by 2 mm.
When the uppermost end point of the seventh sphere of the ball body 7 is too high than the third upper end circular plane of the lower cover connecting frame 3, the second lower end circular plane of the upper cover connecting frame 2 is easily contacted with the third upper end circular plane of the lower cover connecting frame 3, so that the rotary friction resistance of the upper end shell 1 is too large, and when the uppermost end point of the seventh sphere of the ball body 7 is too high than the third upper end circular plane of the lower cover connecting frame 3, the gap between the upper end shell 1 and the lower end shell 5 is too large, experiments show that the uppermost end point of the seventh sphere of the ball body 7 is 0.7-0.9 mm higher than the third upper end circular plane of the lower cover connecting frame 3, and the requirements are met.
In this embodiment, the uppermost end point of the seventh sphere of the ball body 7 is 0.7mm higher than the third upper end circular plane of the lower cover connecting frame 3;
when the fourth cylinder diameter of the circular blind hole diameter ratio pin 4 of second of upper cover link 2 surpassed the size undersize, pin 4 was difficult to pack into the circular blind hole of second of upper cover link 2, lead to the assembly failure, when the fourth cylinder diameter of the circular blind hole diameter ratio pin 4 of second of cover link 2 surpassed the size oversize, pin 4 packs into behind the circular blind hole of second of upper cover link 2, upper end casing 1 and 5 hoop position precisions of lower extreme casing are too low, through the experiment discovery, when the circular blind hole diameter ratio pin 4's of second of upper cover link 2 fourth cylinder diameter is 0.5mm ~ 0.7mm big, satisfy above-mentioned requirement.
In this embodiment, the diameter of the second round blind hole of the upper cover connecting frame 2 is 0.5mm larger than that of the fourth cylinder of the pin 4;
when the ratio undersize of the axial length of the second chamfer of the upper cover connecting frame 2 and the height of the second circular boss of the upper cover connecting frame 2, the chamfer is undersized, when the upper end shell 1 and the lower end shell 5 are installed, the axial size deviation correction capability is too poor, when the ratio of the axial length of the second chamfer of the upper cover connecting frame 2 and the height of the second circular boss of the upper cover connecting frame 2 is too large, the contact surface size of the second circular boss of the upper cover connecting frame 2 and the third central circular through hole of the lower cover connecting frame 3 is too small, and the coaxiality is not facilitated. Through the experiment, it is found that the ratio of the axial length of the second chamfer of the upper cover connecting frame 2 to the height of the second circular boss of the upper cover connecting frame 2 is 1: and 3-4 hours, the requirements are met.
In this embodiment, the ratio of the axial length of the second chamfer of the upper cover connecting frame 2 to the height of the second circular boss of the upper cover connecting frame 2 is 1: 3.
in a similar way, the ratio of the axial length of the third chamfer of the lower cover connecting frame 3 to the height of the second circular boss of the upper cover connecting frame 2 is 1: and 3-4 hours, the requirements are met. .
In this embodiment, the ratio of the axial length of the third chamfer of the lower cover connecting frame 3 to the height of the second circular boss of the upper cover connecting frame 2 is 1: 3.
the device and the upper end warhead are mechanically connected into a whole, and the device and the lower end warhead are also mechanically connected into a whole, so that the upper end warhead and the lower end warhead are integrated, and even if wind exists or the lower end warhead inclines, as long as the lower end warhead is reliably connected, the upper end warhead and the lower end warhead are kept in a tightly connected state, and the upper end warhead cannot slide off, so that the safety is ensured.
The upper end warhead and the upper cover connecting frame are coaxially connected, the lower end warhead and the lower cover connecting frame are coaxially connected, the second circular boss of the upper cover connecting frame is in clearance fit contact with the third central circular through hole of the lower cover connecting frame, and the upper cover connecting frame is coaxial with the lower cover connecting frame, so that the coaxiality precision of the assembled upper end warhead and the lower end warhead is higher, the axial symmetry of the combined warhead is ensured, the power of the warhead after explosion is ensured, the coaxiality error of the upper end warhead and the lower end warhead in the original scheme is 23-46 mm through experimental comparison, and the coaxiality error of the upper end warhead and the lower end warhead in the invention is not more than 1 mm.
The annular angular position precision is higher after the upper-end warhead part is connected with the upper cover connecting frame, the annular angular position precision is higher after the lower-end warhead part is connected with the lower cover connecting frame, and the annular angular position precision is accurately controlled by the upper-end warhead part and the lower-end warhead part through pins, namely the annular angular position precision of the upper-end warhead part and the lower-end warhead part is higher, so that the functional components on the warhead part can work at a preset angle, and the power of the warhead part after explosion is ensured.
After the upper warhead part is connected with the upper cover connecting frame, even if the upper warhead part is displaced through a crane, the position precision of each adjustment is poor, the upper cover connecting frame and the lower end connecting frame are both provided with large chamfers, when the upper cover connecting frame and the lower end connecting frame are combined, the chamfers automatically correct the position precision, after the upper cover connecting frame and the lower end connecting frame are coaxial, the seventh sphere of the ball body jacks up the upper cover connecting frame, the upper warhead part can freely rotate around an axis until a pin enters a pin hole, the circumferential angle position precision is guaranteed, the process is not repeatedly adjusted, the warhead part is formed by one-step installation, and the time is saved.
Example 2:
as shown in fig. 1, the connecting device for a combined warhead in the embodiment comprises an upper end shell 1 and a lower end shell 5, and is characterized by further comprising an upper cover connecting frame 2, a lower cover connecting frame 3, a pin 4 and a spring 6;
the upper end shell 1 is a first cylinder, the first cylinder of the upper end shell 1 is a revolving body, the lower end surface of the first cylinder of the upper end shell 1 is a first lower end circular plane, and the side surface of the first cylinder of the upper end shell 1 is a first outer cylindrical surface;
the axis of the revolving body of the upper end shell 1 is vertical to the ground, and the upper end shell 1 is a warhead shell positioned at the upper end;
the upper cover connecting frame 2 is a second circular plate, the second circular plate of the upper cover connecting frame 2 is a revolving body, the upper end surface of the second circular plate of the upper cover connecting frame 2 is a second upper end circular plane, the lower end surface of the second circular plate of the upper cover connecting frame 2 is a second lower end circular plane, the middle part of the second upper end circular plane of the upper cover connecting frame 2 is provided with a circle of second annular boss, the inner side surface of the second annular boss of the upper cover connecting frame 2 is a second inner cylindrical surface, the second inner cylindrical surface of the upper cover connecting frame 2 is provided with a circle of second threaded holes, the edge of the second lower end circular plane of the upper cover connecting frame 2 is provided with second circular through holes which are uniformly distributed in the circumferential direction, the middle part of the second lower end circular plane of the upper cover connecting frame 2 is provided with second circular blind holes which are uniformly distributed in the circumferential direction, the center of the second lower end circular plane of the upper cover connecting frame 2 is provided with a second circular boss, the lower end surface of the second circular boss of the upper cover connecting frame 2 is a second lower end central circular plane, the side surface of a second circular boss of the upper cover connecting frame 2 is a second outer cylindrical surface, and a second chamfer is arranged at the joint of a second lower end central circular plane of the upper cover connecting frame 2 and the second outer cylindrical surface;
the revolving body axis of the upper cover connecting frame 2 coincides with the revolving body axis of the upper end shell 1, the upper cover connecting frame 2 is positioned at the lower end of the upper end shell 1, a first lower end circular plane of the upper end shell 1 is contacted with a second upper end circular plane of the upper cover connecting frame 2, a first outer cylindrical surface of the upper end shell 1 is contacted with a second inner cylindrical surface of the upper cover connecting frame 2, a second screw is arranged in a second threaded hole of the upper cover connecting frame 2 and is contacted with a first outer cylindrical surface of the upper end shell 1, and the upper end shell 1 is connected with the upper cover connecting frame 2 through the second screw;
the lower cover connecting frame 3 is a third circular plate, the third circular plate of the lower cover connecting frame 3 is a revolving body, the upper end surface of the third circular plate of the lower cover connecting frame 3 is a third upper end circular plane, the lower end surface of the third circular plate of the lower cover connecting frame 3 is a third lower end circular plane, the center of the third upper end circular plane of the lower cover connecting frame 3 is provided with a third central circular through hole, the inner side surface of the third central circular through hole of the lower cover connecting frame 3 is a third inner cylindrical surface, the joint of the third inner cylindrical surface and the third upper end circular plane of the lower cover connecting frame 3 is provided with a third chamfer, the middle part of the third upper end circular plane of the lower cover connecting frame 3 is provided with third circular blind holes which are uniformly distributed in the circumferential direction, the middle part of the third upper end circular plane of the lower cover connecting frame 3 is provided with third spherical holes which are uniformly distributed in the circumferential direction, the middle part of the third lower end circular plane of the lower cover connecting frame 3 is provided with a third annular boss in the circumferential direction, the inner side surface of a third annular boss of the lower cover connecting frame 3 is a third lower end inner cylindrical surface, and a circle of third threaded hole is formed in the third lower end inner cylindrical surface of the lower cover connecting frame 3;
the axis of a rotary body of the lower cover connecting frame 3 is coincident with the axis of a rotary body of the upper cover connecting frame 2, the lower cover connecting frame 3 is positioned at the lower end of the upper cover connecting frame 2, a third inner cylindrical surface of the lower cover connecting frame 3 is contacted with a second outer cylindrical surface of the upper cover connecting frame 2, a third screw is arranged in a third circular through hole of the lower cover connecting frame 3, the third screw penetrates through a second circular through hole of the upper cover connecting frame 2, the head part of the third screw is connected with a nut, and the lower cover connecting frame 3 is connected with the upper cover connecting frame 2 through the third screw;
the pin 4 is a fourth cylinder, and the fourth cylinder of the pin 4 is a revolving body;
the axis of the revolving body of the pin 4 is parallel to the axis of the revolving body of the upper end shell 1, the lower end of the pin 4 is positioned in the third circular blind hole of the lower cover connecting frame 3, and the upper end of the pin 4 is positioned in the second circular blind hole of the upper cover connecting frame 2;
the lower end shell 5 is a fifth cylinder, the fifth cylinder of the lower end shell 5 is a revolving body, the upper end surface of the fifth cylinder of the lower end shell 5 is a fifth upper end circular plane, and the side surface of the fifth cylinder of the lower end shell 5 is a fifth outer cylindrical surface;
the axis of the revolving body of the lower end shell 5 coincides with the axis of the revolving body of the upper end shell 1, the lower end shell 5 is a warhead shell positioned at the lower end, the lower end shell 5 is positioned at the lower end of the lower cover connecting frame 3, a fifth upper end circular plane of the lower end shell 5 is contacted with a third lower end circular plane of the lower cover connecting frame 3, a fifth outer cylindrical surface of the lower end shell 5 is contacted with a third lower end inner cylindrical surface of the lower cover connecting frame 3, a fifth screw is arranged in a third threaded hole of the lower cover connecting frame 3 and is contacted with a fifth outer cylindrical surface of the lower end shell 5, and the lower cover connecting frame 3 is connected with the lower end shell 5 by the fifth screw;
the number of the fifth screws is 16, the number of the fifth screws is M20, each of the fifth screws has a preload of 100 kn, the coefficient of friction between the fifth screws and the fifth outer cylindrical surface of the lower housing 5 is 0.1, i.e., the maximum friction force that each of the fifth screws and the fifth outer cylindrical surface of the lower housing 5 can generate is 10 kn, the maximum friction force that each of the fifth screws and the fifth outer cylindrical surface of the lower housing 5 can generate is 160 kn, i.e., 160000N, and the mass of the lower housing 5 is about 10 tons, i.e., the gravity of the lower housing 5 is 100000N, and the maximum friction force that each of the 16 fifth screws and the fifth outer cylindrical surface of the lower housing 5 generates is 1.6 times the weight of the lower housing 5, so that the lower cover connecting frame 3 and the lower housing 5 can be reliably connected.
The spring 6 is a sixth spiral revolving body;
the spiral rotation axis of the spring 6 is parallel to the rotation body axis of the upper end shell 1, the spring 6 is positioned in the third circular blind hole of the lower cover connecting frame 3, and the spring 6 is positioned at the lower end of the pin 4;
the ball body 7 is a seventh sphere;
the ball body 7 is positioned in the third spherical hole of the lower cover connecting frame 3, and the uppermost end of the ball body 7 is in contact with the second lower end circular plane of the upper cover connecting frame 2;
the using method and the working principle of the invention are as follows: through the mode of upper cover link 2 and 1 mechanical connection of upper end casing, upper cover link 2 is a whole with 1 zonulae occludens of upper end casing, through the mode of lower cover link 3 and 5 mechanical connection of lower extreme casing, lower cover link 3 is a whole with 5 zonulae occludens of lower extreme casing, the mode of 3 rethread mechanical connection of upper cover link 2 and lower cover link, upper cover link 2 is a whole with 3 zonulae occludens of lower cover link, thereby, upper end casing 1 is a whole with 5 zonulae occludens of lower extreme casing. Thereby ensuring the strength of the connection.
The second circular boss of the upper cover connecting frame 2 is inserted into the third central circular through hole of the lower cover connecting frame 3, so that the coaxiality of the upper cover connecting frame 2 and the lower cover connecting frame 3 is ensured, and further the coaxiality of the upper end shell 1 and the lower end shell 5 is ensured.
The upper cover connecting frame 2 and the lower cover connecting frame 3 are provided with chamfers, so that the chamfers can correct the positions of the upper cover connecting frame 2 and the lower cover connecting frame 3 to be coaxial finally even if the upper cover connecting frame 2 and the lower cover connecting frame 3 are not coaxial at the initial moment of installation.
The ball body 7 jacks up the upper cover connecting frame 2, the upper cover connecting frame 2 can drive the upper end shell 1 to freely rotate at the upper end of the lower cover connecting frame 3, the pin 4 is positioned in the third circular blind hole of the lower cover connecting frame 3 in the rotating process of the upper cover connecting frame 2, until the annular relative position of the upper end shell 1 and the lower end shell 5 is correct, the upper end of the pin 4 just enters the second circular blind hole of the upper cover connecting frame 2, subsequently, the upper end and the lower end of the pin 4 are respectively clamped in the third circular blind hole of the lower cover connecting frame 3 and the second circular blind hole of the upper cover connecting frame 2, the lower cover connecting frame 3 and the upper cover connecting frame 2 are prevented from rotating relative to each other in the annular direction, and therefore the annular relative position of the upper end shell 1 and the lower end shell 5 is correct.
When the second lower end center circular plane of the upper cover connecting frame 2 is too small in size higher than the third lower end circular plane of the lower cover connecting frame 3, the second lower end center circular plane of the upper cover connecting frame 2 is easily contacted with the lower end shell 5, the friction resistance of the rotation of the lower end shell 5 is increased, when the second lower end center circular plane of the upper cover connecting frame 2 is too large in size higher than the third lower end circular plane of the lower cover connecting frame 3, the second circular boss of the upper cover connecting frame 2 and the third center circular through hole contact surface of the lower cover connecting frame 3 are too small in size, and the coaxiality is not facilitated. Experiments show that the requirements are met when the second lower end central circular plane of the upper cover connecting frame 2 is 2-3 mm higher than the third lower end circular plane of the lower cover connecting frame 3;
in this embodiment, the second lower end center circular plane of the upper cover link 2 is higher than the third lower end circular plane of the lower cover link 3 by 3 mm.
When the uppermost end point of the seventh sphere of the ball body 7 is too high than the third upper end circular plane of the lower cover connecting frame 3, the second lower end circular plane of the upper cover connecting frame 2 is easily contacted with the third upper end circular plane of the lower cover connecting frame 3, so that the rotary friction resistance of the upper end shell 1 is too large, and when the uppermost end point of the seventh sphere of the ball body 7 is too high than the third upper end circular plane of the lower cover connecting frame 3, the gap between the upper end shell 1 and the lower end shell 5 is too large, experiments show that the uppermost end point of the seventh sphere of the ball body 7 is 0.7-0.9 mm higher than the third upper end circular plane of the lower cover connecting frame 3, and the requirements are met.
In this embodiment, the uppermost end point of the seventh sphere of the ball body 7 is 0.9mm higher than the third upper end circular plane of the lower cover connecting frame 3;
when the diameter of the second round blind hole of the upper cover connecting frame 2 exceeds the diameter of the fourth cylinder of the pin 4, the pin 4 is not easy to be installed into the second round blind hole of the upper cover connecting frame 2, which causes assembly failure, when the diameter of the second round blind hole of the upper cover connecting frame 2 exceeds the diameter of the fourth cylinder of the pin 4, the pin 4 is installed into the second round blind hole of the upper cover connecting frame 2, the precision of the annular position of the upper end shell 1 and the lower end shell 5 is too low, the experiment shows that the diameter of the second round blind hole of the upper cover connecting frame 2 is 0.5 mm-0.7 mm larger than the diameter of the fourth cylinder of the pin 4, and the requirements are met.
In this embodiment, the diameter of the second round blind hole of the upper cover connecting frame 2 is 0.7mm larger than that of the fourth cylinder of the pin 4;
when the ratio undersize of the axial length of the second chamfer of the upper cover connecting frame 2 and the height of the second circular boss of the upper cover connecting frame 2, the chamfer is undersized in size, when the upper end shell 1 and the lower end shell 5 are installed, the axial size deviation correction capability is too poor, when the ratio oversize of the axial length of the second chamfer of the upper cover connecting frame 2 and the height of the second circular boss of the upper cover connecting frame 2, the size of the contact surface of the second circular boss of the upper cover connecting frame 2 and the third central circular through hole of the lower cover connecting frame 3 is too small, and the coaxiality is not facilitated. Through the experiment discovery, the axial length of the second chamfer of upper cover link 2 and the circular boss height ratio of second of upper cover link 2 are 1: and 3-4 hours, the requirements are met.
In this embodiment, the ratio of the axial length of the second chamfer of the upper cover connecting frame 2 to the height of the second circular boss of the upper cover connecting frame 2 is 1: 4.
in a similar way, the ratio of the axial length of the third chamfer of the lower cover connecting frame 3 to the height of the second circular boss of the upper cover connecting frame 2 is 1: and 3-4 hours, the requirements are met. .
In this embodiment, the ratio of the axial length of the third chamfer of the lower cover connecting frame 3 to the height of the second circular boss of the upper cover connecting frame 2 is 1: 4.
the device and the upper end warhead are mechanically connected into a whole, and the device and the lower end warhead are also mechanically connected into a whole, so that the upper end warhead and the lower end warhead are integrated, and even if wind exists or the lower end warhead inclines, as long as the lower end warhead is reliably connected, the upper end warhead and the lower end warhead are kept in a tightly connected state, and the upper end warhead cannot slide off, so that the safety is ensured.
The upper end warhead is coaxial after being connected with the upper cover connecting frame, the lower end warhead is coaxial after being connected with the lower cover connecting frame, and the upper cover connecting frame is coaxial with the lower cover connecting frame after the second circular boss of the upper cover connecting frame is in clearance fit contact with the third central circular through hole of the lower cover connecting frame, so that the coaxiality precision of the assembled upper end warhead and the lower end warhead is higher, the axial symmetry of the combined warhead is ensured, the power of the warhead after explosion is ensured, through experimental comparison, the coaxiality error of the upper end warhead and the lower end warhead in the original scheme is 23-46 mm, and the coaxiality error of the upper end warhead and the lower end warhead is not more than 1 mm.
The annular angle position precision is higher after upper end warhead and upper cover link joint, and the annular angle position precision is higher after lower extreme warhead and lower cover link joint, and upper end warhead passes through pin accurate control annular position precision with lower extreme warhead, and upper end warhead and lower extreme warhead annular angle position precision are higher promptly, guarantee that functional part works at predetermined angle on the warhead, have guaranteed the power after the warhead explosion.
After the upper end warhead portion is connected with the upper cover link, although when carrying out the displacement through the crane, the position precision of adjustment at every turn is poor, but upper cover link and lower extreme link all have big chamfer, when upper cover link and lower extreme link make up, chamfer automatic correction position precision, upper cover link and lower extreme link are coaxial after, because the seventh spheroid of ball body jacks up the upper cover link, upper end warhead portion can be around the axis free rotation, until the pin gets into the cotter hole, hoop angular position precision has been guaranteed, this process has not adjusted repeatedly, all be one-time installation shaping, time saving.
Claims (3)
1. A connecting device for a combined warhead comprises an upper end shell (1) and a lower end shell (5), and is characterized by further comprising an upper cover connecting frame (2), a lower cover connecting frame (3), a pin (4) and a spring (6);
the upper end shell (1) is a first cylinder and is a revolving body, and the axis of the first cylinder is vertical to the ground; the lower end surface of the first cylinder is a first lower end circular plane, and the side surface of the first cylinder is a first outer cylindrical surface;
the upper end shell (1) is a warhead shell positioned at the upper end of the upper cover connecting frame (2);
the upper cover connecting frame (2) is a second circular plate and is a revolving body, the upper end surface of the second circular plate is a second upper end circular plane, and the lower end surface of the second circular plate is a second lower end circular plane; the middle part of the second upper end circular plane is provided with a second annular boss, the inner side surface of the second annular boss is a second inner cylindrical surface, and the second inner cylindrical surface is provided with a circle of second threaded holes;
the edge of the second circular plate is provided with second circular through holes which are uniformly distributed in the circumferential direction, the middle part of a second lower end circular plane is provided with second circular blind holes which are uniformly distributed in the circumferential direction, the center of the second lower end circular plane is provided with a second circular boss, the lower end surface of the second circular boss is a second lower end central circular plane, and the side surface of the second circular boss is a second outer cylindrical surface; a second chamfer is arranged at the joint of the second lower end central circular plane and the second outer cylindrical surface;
the axis of a revolving body of the upper cover connecting frame (2) is coincident with the axis of a revolving body of the upper end shell (1), the upper cover connecting frame (2) is positioned at the lower end of the upper end shell (1), a first lower end circular plane of the upper end shell (1) is contacted with a second upper end circular plane of the upper cover connecting frame (2), a first outer cylindrical surface of the upper end shell (1) is contacted with a second inner cylindrical surface of the upper cover connecting frame (2), a second screw is arranged in a second threaded hole of the upper cover connecting frame (2), the second screw is contacted with a first outer cylindrical surface of the upper end shell (1), and the upper end shell (1) is connected with the upper cover connecting frame (2) through the second screw;
the lower cover connecting frame (3) is a third circular plate and is a revolving body, the upper end surface of the third circular plate is a third upper end circular plane, and the lower end surface is a third lower end circular plane; a third central circular through hole is formed in the center of the third upper end circular plane, the inner side face of the third central circular through hole is a third inner cylindrical surface, and a third chamfer is formed at the joint of the third inner cylindrical surface and the third upper end circular plane; the middle part of the third upper end circular plane is provided with a third circular blind hole and a third spherical hole which are uniformly distributed in the circumferential direction; the edge of the third circular plate is provided with third circular through holes which are uniformly distributed in the circumferential direction, the middle part of a third lower end circular plane is provided with a circle of third annular boss, the inner side surface of the third annular boss is a third lower end inner cylindrical surface, and a circle of third threaded holes are formed in the third lower end inner cylindrical surface;
the axis of a rotary body of the lower cover connecting frame (3) is superposed with the axis of a rotary body of the upper cover connecting frame (2), the lower cover connecting frame (3) is positioned at the lower end of the upper cover connecting frame (2), a third inner cylindrical surface of the lower cover connecting frame (3) is contacted with a second outer cylindrical surface of the upper cover connecting frame (2), a third screw is installed in a third circular through hole of the lower cover connecting frame (3), the third screw penetrates through the second circular through hole of the upper cover connecting frame (2), the head of the third screw is connected with a nut, and the lower cover connecting frame (3) is connected with the upper cover connecting frame (2) by the third screw;
the pin (4) is a fourth cylinder and is a revolving body; the axis of the fourth cylinder is parallel to the axis of the first cylinder, the lower end of the pin (4) is positioned in a third circular blind hole of the lower cover connecting frame (3), and the upper end of the pin (4) is positioned in a second circular blind hole of the upper cover connecting frame (2);
the lower end shell (5) is a fifth cylinder and is a revolving body, the upper end surface of the fifth cylinder is a fifth upper end circular plane, and the side surface is a fifth outer cylindrical surface;
the lower end shell (5) is a warhead shell positioned at the lower end;
the fifth cylindrical axis coincides with the first cylindrical axis, the lower end shell (5) is positioned at the lower end of the lower cover connecting frame (3), a fifth upper end circular plane is contacted with a third lower end circular plane of the lower cover connecting frame (3), a fifth outer cylindrical surface is contacted with a third lower end inner cylindrical surface of the lower cover connecting frame (3), a fifth screw is installed in a third threaded hole of the lower cover connecting frame (3), the fifth screw is contacted with a fifth outer cylindrical surface of the lower end shell (5), and the lower cover connecting frame (3) is connected with the lower end shell (5) by the fifth screw;
the spring (6) is a sixth spiral revolving body;
the axis of the sixth spiral rotary body is parallel to the axis of the first cylindrical body, and the spring (6) is positioned in a third circular blind hole of the lower cover connecting frame (3) and positioned at the lower end of the pin (4);
the ball body (7) is a seventh sphere;
the seventh sphere is positioned in the third sphere hole of the lower cover connecting frame (3), and the uppermost end of the ball body (7) is in contact with the second lower end circular plane of the upper cover connecting frame (2);
the second lower end central circular plane of the upper cover connecting frame (2) is 2 mm-3 mm shorter than the third lower end circular plane of the lower cover connecting frame (3);
the uppermost end point of the seventh sphere is 0.7-0.9 mm higher than the third upper end circular plane of the lower cover connecting frame (3);
the diameter of a second round blind hole of the upper cover connecting frame (2) is 0.5-0.7 mm larger than that of a fourth cylinder of the pin (4);
the ratio of the axial length of the second chamfer of the upper cover connecting frame (2) to the height of the second circular boss of the upper cover connecting frame (2) is 1: 3-4;
the ratio of the axial length of the third chamfer of the lower cover connecting frame (3) to the height of the second circular boss of the upper cover connecting frame (2) is 1: 3 to 4.
2. The coupling device for a built-up warhead according to claim 1, wherein the second lower end center circular plane of the upper cover link (2) is shorter than the third lower end circular plane of the lower cover link (3) by 2 mm;
the uppermost end point of the seventh sphere of the ball body (7) is 0.7mm higher than the third upper end circular plane of the lower cover connecting frame (3);
the diameter of a second round blind hole of the upper cover connecting frame (2) is 0.5mm larger than that of a fourth cylinder of the pin (4);
the ratio of the axial length of the second chamfer of the upper cover connecting frame (2) to the height of the second circular boss of the upper cover connecting frame (2) is 1: 3;
the ratio of the axial length of the third chamfer of the lower cover connecting frame (3) to the height of the second circular boss of the upper cover connecting frame (2) is 1: 3.
3. the coupling device for a built-up warhead according to claim 1, wherein the second lower end center circular plane of the upper cover link (2) is shorter than the third lower end circular plane of the lower cover link (3) by 3 mm;
the uppermost end point of the seventh sphere of the ball body (7) is 0.9mm higher than the third upper end circular plane of the lower cover connecting frame (3);
the diameter of a second round blind hole of the upper cover connecting frame (2) is 0.7mm larger than that of a fourth cylinder of the pin (4);
the ratio of the axial length of the second chamfer of the upper cover connecting frame (2) to the height of the second circular boss of the upper cover connecting frame (2) is 1: 4;
the ratio of the axial length of the third chamfer of the lower cover connecting frame (3) to the height of the second circular boss of the upper cover connecting frame (2) is 1: 4.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202010863325.8A CN111981918B (en) | 2020-08-25 | 2020-08-25 | Connecting device for combined warhead |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202010863325.8A CN111981918B (en) | 2020-08-25 | 2020-08-25 | Connecting device for combined warhead |
Publications (2)
Publication Number | Publication Date |
---|---|
CN111981918A CN111981918A (en) | 2020-11-24 |
CN111981918B true CN111981918B (en) | 2022-08-19 |
Family
ID=73443155
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202010863325.8A Active CN111981918B (en) | 2020-08-25 | 2020-08-25 | Connecting device for combined warhead |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN111981918B (en) |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105115368A (en) * | 2015-06-04 | 2015-12-02 | 西安近代化学研究所 | Payload for cannon and missile weapon platform |
CN204902689U (en) * | 2014-12-23 | 2015-12-23 | 西安航天化学动力厂 | Cladding mould of formed part |
CN206246401U (en) * | 2016-12-05 | 2017-06-13 | 高邮长河泵业有限公司 | A kind of upper and lower shaft coupling connection level of axial-flow pump, proper alignment positioning apparatus |
CN106871740A (en) * | 2017-03-30 | 2017-06-20 | 西安天鹰防务科技有限公司 | The application of barrel assemblies, shell carry frame and shell carry frame on unmanned plane |
CN206535025U (en) * | 2016-06-23 | 2017-10-03 | 中国人民解放军军械工程学院 | The airborne water mists fire-fighting bomb for forest system of the formula that is rigidly connected |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6912943B2 (en) * | 2003-08-04 | 2005-07-05 | Mehdi Bolhassani | Bullet sizing and lubricating device |
-
2020
- 2020-08-25 CN CN202010863325.8A patent/CN111981918B/en active Active
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN204902689U (en) * | 2014-12-23 | 2015-12-23 | 西安航天化学动力厂 | Cladding mould of formed part |
CN105115368A (en) * | 2015-06-04 | 2015-12-02 | 西安近代化学研究所 | Payload for cannon and missile weapon platform |
CN206535025U (en) * | 2016-06-23 | 2017-10-03 | 中国人民解放军军械工程学院 | The airborne water mists fire-fighting bomb for forest system of the formula that is rigidly connected |
CN206246401U (en) * | 2016-12-05 | 2017-06-13 | 高邮长河泵业有限公司 | A kind of upper and lower shaft coupling connection level of axial-flow pump, proper alignment positioning apparatus |
CN106871740A (en) * | 2017-03-30 | 2017-06-20 | 西安天鹰防务科技有限公司 | The application of barrel assemblies, shell carry frame and shell carry frame on unmanned plane |
Also Published As
Publication number | Publication date |
---|---|
CN111981918A (en) | 2020-11-24 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN105466289B (en) | Renewable type sliding block flame-proof mechanism | |
US7143679B2 (en) | Cannelured frangible cartridge and method of canneluring a frangible projectible | |
CN205940308U (en) | A prefabricated angle of attack device for high -speed penetration test of body | |
CN111981918B (en) | Connecting device for combined warhead | |
CN105043172B (en) | A kind of liquid phase charge warhead internal stresses release device | |
CN113246059B (en) | Radial seal circle does not have assembly guiding device of cuting | |
CN113607005B (en) | Can form gradient activation activity and invade shaped charge structure of exploding body of rod | |
US20140299012A1 (en) | Fragmentation-beam tank projectile | |
CN112082438A (en) | Forming device based on laser range finder improves precision | |
CN112879566A (en) | Radial sealing device for compensating insufficient elasticity of material by improving resilience capability of structure | |
US4782198A (en) | Suspension insulators | |
CN205790636U (en) | The semi-rigid SMA bent type radio frequency coaxial connector that a kind of low leakage is highly reliable | |
CN114111460B (en) | Vertical rotor explosion-proof mechanism of rotary bullet fuze for ensuring explosive treatment safety | |
CN113686213B (en) | Micro fuse chemical power supply quick activation mechanism and method thereof | |
KR101782492B1 (en) | Rotating ammunition fuze | |
CN211174992U (en) | Special-shaped full-load four-point contact ball slewing support bearing | |
CN112033236B (en) | Mechanical connecting device capable of automatically correcting precision of axial and circumferential positions of warhead | |
CN110174653A (en) | A kind of millimeter wave test table that portable revolving speed is remote-controlled | |
CN112081803B (en) | Device for improving coaxiality based on laser range finder | |
CN113390303B (en) | Warhead is with body of bullet parameter adjustment device | |
CN216482555U (en) | Ring-shaped energy-gathering charge device | |
CN112066788A (en) | High-safety and high-reliability mechanical firing mechanism | |
US4047485A (en) | Compact electrical fuze | |
CN112879565B (en) | Corrosion-resistant radial cylindrical surface sealing device | |
US3366059A (en) | Fuze for spin stabilized projectiles |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
GR01 | Patent grant | ||
GR01 | Patent grant |