CN109186341B - Electrical dual-purpose connecting plug-in applied to small-caliber bullet emitter and implementation method thereof - Google Patents

Electrical dual-purpose connecting plug-in applied to small-caliber bullet emitter and implementation method thereof Download PDF

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CN109186341B
CN109186341B CN201811011928.4A CN201811011928A CN109186341B CN 109186341 B CN109186341 B CN 109186341B CN 201811011928 A CN201811011928 A CN 201811011928A CN 109186341 B CN109186341 B CN 109186341B
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low pressure
pressure air
air chamber
hole
electric
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CN109186341A (en
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娄文忠
冯恒振
廖茂浩
丁旭冉
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Beijing Institute of Technology BIT
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Beijing Institute of Technology BIT
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41FAPPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F1/00Launching apparatus for projecting projectiles or missiles from barrels, e.g. cannons; Harpoon guns

Abstract

The invention discloses an electrical dual-purpose connecting plug-in applied to a small-caliber bullet emitter and an implementation method thereof. The invention adopts a three-terminal on-off structure, and comprises a high-low pressure air chamber input end, a high-low pressure air chamber output end and a master control end electric control input end, wherein the master control system is installed to a launcher through a master control end electric interface plug-in unit, the high-low pressure air chamber input end is installed to the high-low pressure air chamber, and the high-low pressure air chamber output end is installed to a launcher ammunition in a launching bin; the power line and the communication bus of the main control system of the transmitter are electrically connected through the main electrical connection through hole and the electrical connection through hole; according to the invention, the respective configuration of the electric signal and the high-temperature high-pressure gas passage generated by gunpowder combustion is realized, the interfaces for realizing electric communication are stably fixed by adopting aviation plugs, a large number of redundant control lines are prevented from being existed around and in the prior art, and the quick installation of the electric connection ports and the stable emission of the transmitter are realized.

Description

Electrical dual-purpose connecting plug-in applied to small-caliber bullet emitter and implementation method thereof
Technical Field
The invention relates to a small-caliber bullet launching technology, in particular to an electric dual-purpose connecting plug-in applied to a small-caliber bullet launcher and an implementation method thereof.
Background
In the process of launching the small-caliber bullet, the powder burns to generate a large amount of energy, and the energy passes through a high-low pressure air chamber of the launcher to provide kinetic energy for launching the small-caliber bullet, thereby realizing the throwing of the small-caliber bullet. However, with the development of small caliber ammunition, the remote control of the master control terminal is used to ensure that the ammunition works stably according to the preset logic time sequence, so that the electromechanical control has become the main body of the small caliber ammunition application. There are two conventional methods of transmission: 1. separate electronic communication interfaces and separate high-low pressure air chambers are reserved in the bin, but as bullet medicines develop towards the miniaturization direction, the firing mode of the bullet is changed from traditional single firing to multiple firing of the small-caliber bullet, so that the target is hit. Meanwhile, a large number of electrical interfaces can increase the weight of the whole emission bin and cause a large number of communication cable redundancies, which is not beneficial to the convenient operation of the battlefield environment; 2. the electronic communication power line and the serial port communication line are arranged on the side wall inside the high-low pressure air chamber and fixed in a special mode, after multiple emission is carried out in the connection mode, the connection mode becomes extremely unstable and cannot be controlled due to sudden changes of the conditions of the temperature, the air pressure and the like inside the high-low pressure air chamber, and finally, the emission and the accurate target hitting are affected. The two interface modes have unstable factors, and long-time stable control in the bullet medicine shooting process can not be realized.
Disclosure of Invention
Based on the problems, the invention provides the electrical dual-purpose connecting plug-in applied to the small-caliber bullet launcher and the implementation method thereof, and the connecting plug-in can reasonably utilize the limited space in the launcher and fundamentally improve the control and signal transmission of real-time high stability of the ammunition in the launching process.
It is an object of the present invention to provide an electrical dual purpose connector insert for use in a small caliber projectile launcher.
A multi-ammunition is arranged in the launching bin; the output end of the high-low pressure air chamber is provided with a plurality of pressure dividing hoses; the power line and the communication bus of the main control system of the transmitter are respectively led out through a plurality of adapter joints of the deconcentrator, so that the setting of the detonation information and the setting of the ignition energy information of the system are realized.
The electrical dual-purpose connection plug applied to the small-caliber bullet emitter comprises: the device comprises a three-terminal on-off structure, a master control end electrical interface plug-in, a high-low pressure air chamber end electrical interface plug-in and a transmitting bin end electrical interface plug-in; the three-terminal on-off structure comprises a rigid shell, a high-low pressure air chamber input end, a high-low pressure air chamber output end and a total control end electric control input end, wherein the rigid shell is of a cylinder cavity structure, the high-low pressure air chamber input end and the high-low pressure air chamber output end are respectively arranged at two ends of the cylinder cavity structure, the total control end electric control input end is arranged on the side wall of the cylinder cavity structure, and the axis of the total control end electric control input end is perpendicular to the axis of the cylinder cavity structure; the central through hole of the electric control input end of the main control end is a main electric connection through hole and is communicated with the cylindrical cavity structure of the rigid shell, and the top end of the pipe wall of the electric control input end of the main control end is provided with a mounting groove; the central through hole of the input end of the high-low pressure air chamber is an input ventilation through hole, the pipe wall of the input end of the high-low pressure air chamber is provided with a high-low pressure air chamber electric connection through hole, the axis of the high-low pressure air chamber electric connection through hole is parallel to the axis of the cylinder cavity structure, the high-low pressure air chamber electric connection through hole is communicated with the main electric connection through hole, and the top end of the pipe wall of the input end of the high-low pressure air chamber is also provided with a mounting groove; the central through hole of the output end of the high-low pressure air chamber is an output ventilation through hole, the input ventilation through hole is communicated to the output ventilation through hole through a cylinder cavity structure, the pipe wall of the output end of the high-low pressure air chamber is provided with an electric connection through hole of a transmitting bin, the axis of the electric connection through hole of the transmitting bin is parallel to the axis of the cylinder cavity structure, the electric connection through hole of the transmitting bin is communicated to a main electric connection through hole, and the top end of the pipe wall of the output end of the high-low pressure air chamber is also provided with a mounting groove; the electric interface plug-in of the main control end is annular, the horizontal shape is matched with the port shape of the electric control input end of the main control end, the electric interface plug-in of the main control end corresponds to the electric control input end of the main control end, the central through hole of the electric interface plug-in of the main control end is a main electric connection through hole, and the annular wall of the electric interface plug-in of the main control end is provided with a mounting hole; the electric interface plug-in at the high-low pressure air chamber end is annular, the horizontal shape is matched with the port shape of the input end of the high-low pressure air chamber, the electric interface plug-in corresponds to the input end of the high-low pressure air chamber, the central through hole of the electric interface plug-in at the high-low pressure air chamber end is an input ventilation through hole, and the annular wall of the electric interface plug-in at the high-low pressure air chamber end is provided with an electric connection through hole and a mounting hole; the electric interface plug-in at the transmitting bin end is annular, the horizontal shape of the electric interface plug-in is matched with the shape of the port of the output end of the high-low pressure air chamber, the electric interface plug-in corresponds to the output end of the high-low pressure air chamber, the central through hole of the electric interface plug-in at the transmitting bin end is an output ventilation through hole, and the annular wall of the electric interface plug-in at the transmitting bin end is provided with an electric connection through hole and a mounting hole; the electric control input end of the total control end of the three-end on-off structure is mounted to an adapter of the deconcentrator through the electric interface plug-in of the total control end so as to realize electric connection with a main control system of the transmitter, the input end of the high-low pressure air chamber is mounted to a voltage dividing hose of the output end of the high-low pressure air chamber through the electric interface plug-in of the high-low pressure air chamber, and the output end of the high-low pressure air chamber is mounted to a piece of ammunition in the transmitting bin through the electric interface plug-in of the transmitting bin end; the main control system is divided into two parts by a power line and a communication bus which are respectively led out by the deconcentrator, one part is connected to the power line and the communication line of each sub-ammunition sequentially through a main electric connection through hole and a transmitting bin electric connection through hole, and the other part is connected to the power line and the communication line in a wiring hole on the cavity wall of the high-low pressure air chamber sequentially through the main electric connection through hole and the high-low pressure air chamber electric connection through hole; before the firing, the main control system detects the safety and reliability states of the ammunition through the main control end electrical control input end and carries out detonation information setting; during the shooting, the bullet medicine disconnection and the communication connection of master control system, the bleeder hose of the output of high low pressure air chamber is through the input ventilation through-hole of high low pressure air chamber input with high low pressure air pressure and is carried three terminal break-make structure, carries to a bullet ammunition in the shooting bin through the output ventilation through-hole of high low pressure air chamber output, and high low pressure air pressure converts into initial kinetic energy and launches the bullet ammunition.
The front end of the pipe wall of the electric control input end of the main control end is provided with a plurality of mounting grooves which are distributed in a central symmetry mode.
The pipe wall of the input end of the high-low pressure air chamber is provided with a plurality of high-low pressure air chamber electric connection through holes, the front end of the high-low pressure air chamber is provided with a plurality of mounting grooves, and the plurality of high-low pressure air chamber electric connection through holes are distributed in a central symmetry manner; the plurality of mounting grooves are distributed in a central symmetry mode.
The main control end electrical interface plug-in is fixedly connected with a main control end electrical control input end of the three-terminal on-off structure through a fixing pin; the high-low pressure air chamber end electrical interface plug-in is fixedly connected with the high-low pressure air chamber input end of the three-end on-off structure through a fixing pin; the electric interface plug-in at the transmitting bin end is fixedly connected with the output end of the high-low pressure air chamber of the three-end on-off structure through a fixing pin.
Another object of the present invention is to provide a method for implementing an electrical dual-purpose connection insert for a small-caliber bullet emitter.
The invention discloses a realization method of an electric dual-purpose connection plug-in unit applied to a small-caliber bullet emitter, which comprises the following steps:
1) And (3) electric connection:
a) The main control system of the transmitter is divided into two parts by a power line and a communication bus which are respectively led out by the deconcentrator; one strand is connected to the power line and the communication line of each sub ammunition sequentially through the main electric connection through hole and the electric connection through hole of the launching bin;
b) The other strand is connected to a power line and a communication line in a wiring hole on the cavity wall of the high-low pressure air chamber through a main electric connection through hole and a high-low pressure air chamber electric connection through hole in sequence;
2) And (3) mechanical connection:
a) The total control end electric control input end of the three-end on-off structure is mounted to one adapter of the deconcentrator through the total control end electric interface plug-in unit so as to realize electric connection with a main control system of the transmitter;
b) The input end of the high-low pressure air chamber is mounted to a pressure dividing hose at the output end of the high-low pressure air chamber through an electrical interface plug-in at the end of the high-low pressure air chamber;
c) The output end of the high-low pressure air chamber is mounted to a propellant charge in the launching bin through an electrical interface plug-in at the end of the launching bin;
3) And (5) service treatment before transmission:
after the system is electrified, the main control system detects the safety and reliability states of the sub ammunition through the main control end electrical control input end, and performs function and logic configuration on tasks to be executed by the sub ammunition;
4) Target locking:
after the system locks the striking target, the main control system sets the detonation information of the sub-ammunition;
5) Target striking:
the launcher launches the ammunition, the communication connection of the ammunition disconnection and the master control system, high-temperature high-pressure gas generated by the gunpowder combustion passes through the high-low pressure air chamber in the twinkling of an eye, high-low pressure air is conveyed to the three-terminal on-off structure through the input end of the high-low pressure air chamber, the ammunition enters the launching bin, and the ammunition is pushed by the high-temperature high-pressure gas to obtain initial kinetic energy launching, so that target striking is finally realized.
The invention has the advantages that:
the invention adopts a three-terminal on-off structure, and comprises a high-low pressure air chamber input end, a high-low pressure air chamber output end and a master control end electric control input end, wherein the master control system is installed to a launcher through a master control end electric interface plug-in unit, the high-low pressure air chamber input end is installed to the high-low pressure air chamber, and the high-low pressure air chamber output end is installed to a launcher ammunition in a launching bin; the power line and the communication bus of the main control system of the transmitter are electrically connected through the main electrical connection through hole and the electrical connection through hole; according to the invention, the respective configuration of the electric signal and the high-temperature high-pressure gas passage generated by gunpowder combustion is realized, the interfaces for realizing electric communication are stably fixed by adopting aviation plugs, a large number of redundant control lines are prevented from being existed around and in the prior art, and the quick installation of the electric connection ports and the stable emission of the transmitter are realized.
Drawings
FIG. 1 is an exploded view of one embodiment of an electrical dual purpose connection insert of the present invention applied to a small caliber bullet emitter;
FIG. 2 is a schematic diagram of a three-terminal on-off configuration of one embodiment of an electrical dual-purpose connection insert of the present invention applied to a small caliber bullet emitter;
FIG. 3 is a schematic diagram of a general control side electrical interface package of one embodiment of the present invention applied to a dual electrical connection package for a small caliber bullet launcher;
FIG. 4 is a schematic illustration of a high and low pressure plenum side electrical interface insert of one embodiment of the present invention applied to a small caliber bullet emitter;
FIG. 5 is a schematic view of a launch cartridge-end electrical interface package of one embodiment of the present invention applied to a small caliber bullet launcher;
fig. 6 is an exploded view of the general connection of the electrical dual-purpose connection insert of the present invention applied to a small caliber bullet emitter.
Detailed Description
The invention will be further elucidated by means of specific embodiments in conjunction with the accompanying drawings.
As shown in fig. 1, the electrical dual-purpose connection plug applied to the small-caliber bullet emitter of the present embodiment includes: three-terminal on-off structure, total accuse end electrical interface plug-in components 2, high low pressure air chamber end electrical interface plug-in components 3 and launching bin end electrical interface plug-in components 4. The three-terminal on-off structure is fixedly connected with the main control end electrical interface plug-in unit 2, the high-low pressure air chamber end electrical interface plug-in unit 3 and the transmitting bin end electrical interface plug-in unit 4 through fixing pins 5.
As shown in fig. 1 and 2, the three-terminal on-off structure comprises a rigid shell 11, a high-low pressure air chamber input end 13, a high-low pressure air chamber output end 14 and a total control end electrical control input end 12, wherein the rigid shell 11 is a cylindrical cavity structure, the high-low pressure air chamber input end 13 and the high-low pressure air chamber output end 14 are respectively arranged at two ends of the cylindrical cavity structure, the total control end electrical control input end 12 is arranged on the side wall of the cylindrical cavity structure, and the axis of the total control end electrical control input end 12 is perpendicular to the axis of the cylindrical cavity structure; the central through hole of the main control end electrical control input end 12 is a main electrical connection through hole and is communicated with the cylindrical cavity structure of the rigid shell 11, and the top end of the pipe wall of the main control end electrical control input end 12 is provided with a mounting groove; the central through hole of the high-low pressure air chamber input end 13 is an input ventilation through hole, the pipe wall of the high-low pressure air chamber input end 13 is provided with a high-low pressure air chamber electric connection through hole, the axis of the high-low pressure air chamber electric connection through hole is parallel to the axis of the cylinder cavity structure, the high-low pressure air chamber electric connection through hole is communicated with the main electric connection through hole, and the pipe wall top end of the high-low pressure air chamber input end 13 is also provided with a mounting groove; the central through hole of high-low pressure air chamber output 14 is the output through hole that ventilates, and the input through hole that ventilates communicates to the output through hole that ventilates through cylinder cavity structure, is provided with the electric connection through hole of transmission storehouse at the pipe wall of high-low pressure air chamber output 14, and the axis of transmission storehouse electric connection through hole is on a parallel with the axis of cylinder cavity structure to the electric connection through hole of transmission storehouse communicates to main electric connection through hole, still is provided with the mounting groove on the pipe wall top of high-low pressure air chamber output 14.
As shown in fig. 3, the electrical interface plug-in of the main control end is annular, the horizontal shape is matched with the port shape of the electrical control input end of the main control end, the central through hole of the electrical interface plug-in of the main control end corresponds to the electrical control input end of the main control end, the central through hole of the electrical interface plug-in of the main control end is a main electrical connection through hole 21, and a mounting hole 22 is arranged on the annular wall of the electrical interface plug-in of the main control end.
As shown in fig. 4, the electrical interface plug-in at the high-low pressure air chamber end is annular, the horizontal shape is matched with the port shape of the input end of the high-low pressure air chamber, the central through hole of the electrical interface plug-in at the high-low pressure air chamber end is an input ventilation through hole 31 corresponding to the input end of the high-low pressure air chamber, and the annular wall of the electrical interface plug-in at the high-low pressure air chamber end is provided with an electrical connection through hole 32 and a mounting hole 33.
As shown in fig. 5, the electrical interface plug-in at the transmitting bin end is annular, the horizontal shape is matched with the port shape of the output end of the high-low pressure air chamber, the central through hole of the electrical interface plug-in at the transmitting bin end is an output ventilation through hole 41 corresponding to the output end of the high-low pressure air chamber, and the annular wall of the electrical interface plug-in at the transmitting bin end is provided with an electrical connection through hole 42 and a mounting hole 43.
As shown in fig. 6, the electrical control input end of the total control end of the three-end on-off structure is mounted to an adapter of the deconcentrator through the electrical interface plug-in of the total control end so as to realize electrical connection with a main control system of the transmitter, the input end of the high-low pressure air chamber is mounted to a voltage dividing hose 031 of the output end of the high-low pressure air chamber 03 through the electrical interface plug-in of the high-low pressure air chamber, and the output end of the high-low pressure air chamber is mounted to a ammunition 01 of a transmitter in the transmitting bin 04 through the electrical interface plug-in of the transmitting bin end; the main control system is divided into two parts by a power line and a communication bus which are led out by the deconcentrator respectively, one part is connected to the power line and the communication line of each ammunition through the main electric connection through hole and the electric connection through hole of the launching bin in sequence, and the other part is connected to the power line and the communication line in the wiring hole on the cavity wall of the high-low pressure air chamber through the main electric connection through hole and the electric connection through hole of the high-low pressure air chamber in sequence.
Finally, it should be noted that the examples are disclosed for the purpose of aiding in the further understanding of the present invention, but those skilled in the art will appreciate that: various alternatives and modifications are possible without departing from the spirit and scope of the invention and the appended claims. Therefore, the invention should not be limited to the disclosed embodiments, but rather the scope of the invention is defined by the appended claims.

Claims (5)

1. An electrical dual-purpose connecting plug-in applied to a small-caliber bullet launcher is provided with multiple ammunition in a launching bin; the output end of the high-low pressure air chamber is provided with a plurality of pressure dividing hoses; the power line and the communication bus of the main control system of the transmitter are led out respectively through a plurality of adapter of the deconcentrator, and the electric dual-purpose connecting plug-in unit comprises: the device comprises a three-terminal on-off structure, a master control end electrical interface plug-in, a high-low pressure air chamber end electrical interface plug-in and a transmitting bin end electrical interface plug-in; the three-terminal on-off structure comprises a rigid shell, a high-low pressure air chamber input end, a high-low pressure air chamber output end and a total control end electric control input end, wherein the rigid shell is of a cylinder cavity structure, the high-low pressure air chamber input end and the high-low pressure air chamber output end are respectively arranged at two ends of the cylinder cavity structure, the total control end electric control input end is arranged on the side wall of the cylinder cavity structure, and the axis of the total control end electric control input end is perpendicular to the axis of the cylinder cavity structure; the central through hole of the electric control input end of the main control end is a main electric connection through hole and is communicated with the cylindrical cavity structure of the rigid shell, and the top end of the pipe wall of the electric control input end of the main control end is provided with a mounting groove; the central through hole of the input end of the high-low pressure air chamber is an input ventilation through hole, the pipe wall of the input end of the high-low pressure air chamber is provided with a high-low pressure air chamber electric connection through hole, the axis of the high-low pressure air chamber electric connection through hole is parallel to the axis of the cylinder cavity structure, the high-low pressure air chamber electric connection through hole is communicated with the main electric connection through hole, and the top end of the pipe wall of the input end of the high-low pressure air chamber is also provided with a mounting groove; the central through hole of the output end of the high-low pressure air chamber is an output ventilation through hole, the input ventilation through hole is communicated to the output ventilation through hole through a cylinder cavity structure, the pipe wall of the output end of the high-low pressure air chamber is provided with an emission bin electric connection through hole, the axis of the emission bin electric connection through hole is parallel to the axis of the cylinder cavity structure, the emission bin electric connection through hole is communicated to a main electric connection through hole, and the top end of the pipe wall of the output end of the high-low pressure air chamber is also provided with a mounting groove; the main control end electrical interface plug-in is annular, the horizontal shape of the main control end electrical interface plug-in is matched with the shape of a port of the main control end electrical control input end, the main control end electrical interface plug-in corresponds to the main control end electrical control input end, the central through hole of the main control end electrical interface plug-in is a main electrical connection through hole, and the annular wall of the main control end electrical interface plug-in is provided with a mounting hole; the electric interface plug-in unit at the end of the high-low pressure air chamber is annular, the horizontal shape is matched with the shape of the port of the input end of the high-low pressure air chamber, the electric interface plug-in unit corresponds to the input end of the high-low pressure air chamber, the central through hole of the electric interface plug-in unit at the end of the high-low pressure air chamber is an input ventilation through hole, and the annular wall of the electric interface plug-in unit at the end of the high-low pressure air chamber is provided with an electric connection through hole and a mounting hole; the electric interface plug-in at the transmitting bin end is annular, the horizontal shape of the electric interface plug-in is matched with the shape of the port of the output end of the high-low pressure air chamber, the electric interface plug-in corresponds to the output end of the high-low pressure air chamber, the central through hole of the electric interface plug-in at the transmitting bin end is an output ventilation through hole, and the annular wall of the electric interface plug-in at the transmitting bin end is provided with an electric connection through hole and a mounting hole; the electric control input end of the main control end of the three-end on-off structure is mounted to an adapter of the deconcentrator through the electric interface plug-in of the main control end so as to realize electric connection with a main control system of the transmitter, the input end of the high-low pressure air chamber is mounted to a voltage dividing hose of the output end of the high-low pressure air chamber through the electric interface plug-in of the high-low pressure air chamber, and the output end of the high-low pressure air chamber is mounted to a piece of ammunition in the transmitting bin through the electric interface plug-in of the transmitting bin end; the main control system is divided into two parts by a power line and a communication bus which are respectively led out by the deconcentrator, one part is connected to the power line and the communication line of each ammunition sequentially through a main electric connection through hole and a transmitting bin electric connection through hole, and the other part is connected to the power line and the communication line in a wiring hole on the cavity wall of the high-low pressure air chamber sequentially through the main electric connection through hole and the high-low pressure air chamber electric connection through hole; before the firing, the main control system detects the safety and reliability states of the ammunition through the main control end electrical control input end and carries out detonation information setting; during the shooting, the bullet medicine disconnection and the communication connection of master control system, the bleeder hose of the output of high low pressure air chamber is through the input ventilation through-hole of high low pressure air chamber input with high low pressure air pressure and is carried three terminal break-make structure, carries to a bullet ammunition in the shooting bin through the output ventilation through-hole of high low pressure air chamber output, and high low pressure air pressure converts into initial kinetic energy and launches the bullet ammunition.
2. The electrical dual-purpose connection plug-in as claimed in claim 1, wherein the front end of the pipe wall of the general control end electrical control input end is provided with a plurality of mounting grooves which are distributed in a central symmetry manner.
3. The electrical dual-purpose connecting plug-in unit as claimed in claim 1, wherein the pipe wall of the input end of the high-low pressure air chamber is provided with a plurality of high-low pressure air chamber electrical connecting through holes, the front end is provided with a plurality of mounting grooves, and the plurality of high-low pressure air chamber electrical connecting through holes are distributed in a central symmetry manner; the plurality of mounting grooves are distributed in a central symmetry mode.
4. The electrical dual-purpose connection plug-in as claimed in claim 1, wherein the general control end electrical interface plug-in is fixedly connected with a general control end electrical control input end of the three-terminal on-off structure through a fixing pin; the high-low pressure air chamber end electrical interface plug-in is fixedly connected with the high-low pressure air chamber input end of the three-end on-off structure through a fixing pin; the electric interface plug-in at the transmitting bin end is fixedly connected with the output end of the high-low pressure air chamber of the three-end on-off structure through a fixing pin.
5. A method of implementing an electrical dual-purpose connection insert for a small caliber bullet emitter according to claim 1, comprising the steps of:
1) And (3) electric connection:
a) The main control system of the transmitter is divided into two parts by a power line and a communication bus which are respectively led out by the deconcentrator; one strand is connected to the power line and the communication line of each sub ammunition sequentially through the main electric connection through hole and the electric connection through hole of the launching bin;
b) The other strand is connected to a power line and a communication line in a wiring hole on the cavity wall of the high-low pressure air chamber through a main electric connection through hole and a high-low pressure air chamber electric connection through hole in sequence;
2) And (3) mechanical connection:
a) The total control end electric control input end of the three-end on-off structure is mounted to one adapter of the deconcentrator through the total control end electric interface plug-in unit so as to realize electric connection with a main control system of the transmitter;
b) The input end of the high-low pressure air chamber is mounted to a pressure dividing hose at the output end of the high-low pressure air chamber through an electrical interface plug-in at the end of the high-low pressure air chamber;
c) The output end of the high-low pressure air chamber is mounted to a propellant charge in the launching bin through an electrical interface plug-in at the end of the launching bin;
3) And (5) service treatment before transmission:
after the system is electrified, the main control system detects the safety and reliability states of the sub ammunition through the main control end electrical control input end, and performs function and logic configuration on tasks to be executed by the sub ammunition;
4) Target locking:
after the system locks the striking target, the main control system sets the detonation information of the sub-ammunition;
5) Target striking:
the launcher launches the ammunition, the communication connection of the ammunition disconnection and the master control system, high-temperature high-pressure gas generated by the gunpowder combustion passes through the high-low pressure air chamber in the twinkling of an eye, high-low pressure air is conveyed to the three-terminal on-off structure through the input end of the high-low pressure air chamber, the ammunition enters the launching bin, and the ammunition is pushed by the high-temperature high-pressure gas to obtain initial kinetic energy launching, so that target striking is finally realized.
CN201811011928.4A 2018-08-31 2018-08-31 Electrical dual-purpose connecting plug-in applied to small-caliber bullet emitter and implementation method thereof Active CN109186341B (en)

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CN208833086U (en) * 2018-08-31 2019-05-07 北京理工大学 A kind of electric and gas dual purpose connection plug-in unit applied to Small cartridge transmitter

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